Welcome to the Family

Transcription

1 Aerospace Gulfstream 280 Welcome to the Family This Honeywell Operator Handbook is designed to introduce you to the Honeywell systems on your Gulfstream aircraft and provide you with basic knowledge to support your daily operations. In addition to valuable product overviews and operational guidelines, we have included information on our service and support programs that will help you to maximize your experience with this equipment. Support Network Aerospace Technical Support Portal Training Pilot Pilot Gateway Engine APU Systems Maintenance & Flight Services Optional Equipments & Upgrades Global Customer Committee Resources Quick Start Guide

2 Aerospace Business Aviation Quick Start Guide This Quick Start Guide contains essential information for getting started with Honeywell products and services on your new aircraft. Go back to the main page to browse complete information. This guide links to external websites so you have to be connected to the internet. AOG Customer Portal Registration Aerospace Technical Support Important Information Aircraft on Ground. Our dedicated Support Service Teams are poised to assist you 24 hours a day, 7 days a week Worldwide. Important Information To access any of the services online at myaerospace.com you need to Sign in to get your Honeywell ID. Important Information Our 24/7/365 technical operations center is at your service for immediate resolution of technical issues. Training Technical Publications Aftermarket Services Important Information New aircraft receive Free of Charge training entitlement slots per product/system good for 2 years from date of delivery. Important Information New aircraft receive tech pubs entitlement for 12 months of no charge publications. Important Information Protect your equipment, lower the cost of ownership, and increase the value and efficiency of your aircraft with Honeywell Aftermarket Services. Direct Access Pilot Gateway Business Aviation on the Go Important Information Honeywell support Network Mobile App. Your Honeywell Business Aviation customer support network now travels with you. Important Information The Honeywell Pilot Gateway is your one stop shop for key aircraft information. Important Information View Honeywell Aerospace products for various business aviation aircraft platforms and models. Back to Menu

3 Direct Access Your Honeywell Business Aviation Customer Support Network Now Travels With You

4 Your Honeywell Business Aviation Customer Support Network Now Travels With You Quickly connect with Aircraft On Ground (AOG) desks, easily locate and contact your nearest avionics dealer and mechanical service center; sales managers; access the Aerospace Technical Support Network for immediate technical support of your aircraft anywhere in the world and receive the latest news from Honeywell. True to its name, the app utilizes GPS data to provide direct access to Honeywell s aircraft on ground support, nearest tech support staff, dealers, service centers, and other vital Honeywell customer resources. Direct Access makes it easier than ever for customers to reach out and find someone who can help them, with just a few touches on their smart phone or tablet. It gives Honeywell the ability to respond to our customers needs and solve their problems quicker and more efficiently. The new mobile app is designed with extensive input from our Global Customer Committee who acted as beta testers at every step in the process to ensure that the app meets the real needs of our customers. The Direct Access App is published and available as follows: Honeywell Aerospace hosting page: Honeywell App Store: BlackBerry/Windows Phones and Desktops (access through device browser):

5 Worldwide Reach Worldwide Support Together Delivering Solutions To The Global Business Aviation Market Global Technical Operations Honeywell Aerospace 1944 East Sky Harbor Circle Phoenix, AZ aerospace.honeywell.com C / Honeywell International Inc. Back Home C Global Tech Ops.indd 1-2 4/10/16 10:25 AM

6 Connecting to Aerospace Technical Support Global Technical Operations By Phone: By Web: (US/Canada) MyAerospace.com (International) Honeywell Aerospace s Global Technical Operations provide comprehensive and responsive technical support through an extensive network of experts around the globe. Press #1 for Avionics or #2 for Mechanical By AeroTechSupport@Honeywell.com By App: (For Business & General Aviation Customers) Launch the Honeywell Mobile Application from Tablets or SmartPhones running Android, Apple, and Blackberry OS Aircraft On Ground - We are Here to Help Aerospace Technical Support By Phone: Honeywell s enhanced Aerospace Technical Support network is your single (US/Canada) point-of-entry for technical assistance 24 hours a day. Our global team of (International) highly skilled field service, product support and technical support engineers Option #4 is dedicated to resolving your technical issues... on the spot. Non-technical Issues Combining state-of-the-art communications technology, streamlined Part Quotes, Ordering, Repair or Warranty processes and a fully staffed network of avionics and mechanical experts ensures that you get immediate technical guidance and troubleshooting solutions for all your Honeywell Aerospace products. Dedicated Technical Support Our global team provides engineering support to maintenance personnel through telephone consultation or at the customer s facility. Engineering Performance Solutions A team of product support engineers provide timely technical responses Honeywell Aerospace hosting page: aerospace.honeywell.com/mobileapp Honeywell App Store: appstore.honeyewell.com Blackberry/Windows Phones & Browsers access through device browser: honeywellaero.force.com/bgadir By Phone: (US/Canada) (International) Option #1 Spares Option #2 Global Data Center, NavDB, MSP, HAPP Option #3 Repair & Overhaul Option #6 Technical Publications to complex field issues and analysis of reliability data to guide product improvements. Team members leverage advanced analytics of fleet performance and OEM alignment to identify opportunities for high-impact investigations and near-term solutions for customer technical issues. The team serves as the primary source for improving the long-term performance of Honeywell Aerospace products, and they help drive down the total cost of ownership. Back Home C Global Tech Ops.indd 3-4 4/10/16 10:25 AM

7 Connecting to Aerospace Technical Support By Phone: By Web: (US/Canada) MyAerospace.com (International) Press #1 for Avionics or #2 for Mechanical By By App: (For Business & General Aviation Customers) Launch the Honeywell Mobile Application from Tablets or SmartPhones running Android, Apple, and Blackberry OS Aircraft On Ground - We are Here to Help By Phone: (US/Canada) (International) Option #4 Non-technical Issues Part Quotes, Ordering, Repair or Warranty Honeywell Aerospace hosting page: aerospace.honeywell.com/mobileapp By Phone: Worldwide Reach Worldwide Support (US/Canada) (International) Honeywell App Store: appstore.honeyewell.com Option #1 Spares Option #2 Global Data Center, NavDB, MSP, HAPP Blackberry/Windows Phones & Browsers access through device browser: Option #3 Repair & Overhaul Option #6 Technical Publications Together Delivering Solutions To The Global Business Aviation Market honeywellaero.force.com/bgadir Global Technical Operations Honeywell Aerospace 1944 East Sky Harbor Circle Phoenix, AZ aerospace.honeywell.com C / Honeywell International Inc. Back Home C Global Tech Ops.indd 1-2 4/10/16 10:25 AM

8 THE BEST SUPPORT NUMBER YOU CAN FLY. ONE-CALL YOU VE GOT QUESTIONS. WE VE GOT ANSWERS. AND YOU VE GOT OUR NUMBER. ANYTIME At Honeywell Aerospace, the quest for perfection isn t just about the products we design and make. It s also about the way we support those products, and the people who use them. Your success depends on keeping the aircraft flying, solving problems quickly, and knowing immediate technical support is available always. In fact, when we asked customers what is the single most important service we can provide, the overwhelming answer was 24 X 7 phone support from technical experts to ensure dispatchability. So - that s exactly what Honeywell Aerospace now offers you. ANYWHERE One-Call Technical Assistance. 24/ 7 ANYTIME. FROM ANYWHERE. HONEYWELL AVIATION INTRODUCES ONE-CALL TECHNICAL ASSISTANCE. KEEPING YOU FLYING. 24/ 7 When everything is on the line, so are we. Aerospace Electronic Systems Air Transport Systems Honeywell International Inc North 19th Avenue Phoenix, AZ Tel: Fax: May Honeywell International Inc. Ver1 Back Home

9 We've rebuilt Honeywell Technical Support to fit you. Our one goal in creating the new Honeywell technical support systems was to put you no more than one call away from the person with answers no matter what the question. To do that, we completely refigured our technical support structure. Now, Honeywell Technical Operations Center staff, Field Service Engineers (FSE,) and Product Service Engineers (PSE) work together as a cohesive Global Technical Operations unit. It's a fully staffed network of avionics and mechanical experts that makes sure you get immediate technical guidance and troubleshooting solutions to keep you flying This design brings you a tremendous depth of knowledge beyond what any single FSE could provide it gives you experience and expertise in every possible dispatch related area of concern. In fact, prior to implementing this new system, the people taking your calls at Honeywell had an average of 8 years experience. Today, you ll talk to 20-year veterans. Make the call that connects you to the network, and you re matched with an experienced support professional assigned to quickly resolve your question and get you safely flying again. In reorganizing our customer service structure, we created a dedicated Entry Into Service (EIS) support team. The team s sole function is to provide the trouble shooting, operational guidance, training, and unforeseen factors support that can come with taking delivery of a new platform. The more we help you, the smarter we get. One number lines you up with it all. Here s another advantage the new integrated system has over the old way of doing things: now, we can collect and share frequently asked questions and their solutions. So one customer s successful interaction with a Honeywell technical expert has the potential to benefit a world of flight. Technical support 24/7, experienced full-time product and support staff, consistent support for all airlines, and one-number convenience working together to increase first-call resolution. Another thing we think you ll appreciate about the system: instead of just a select few Honeywell customers having access to experts, we re bringing everyone closer to help. And, the same experts you ll talk with when you call also happen to be located throughout every customer region. So when you need on-site support, Honeywell is there. Those technical experts work in partnership with AOG teams to resolve AOGs in the most efficient way available, whether that means technical support or parts access. A couple more features to win an airline s heart. The conversations we ve had with airline customers made it clear when it comes to product fixes, they don t want to play the role of middle-man. Instead, they want Honeywell to work directly with OEMs to solve problems, and to hold off on releasing fixes until both sides agree it s the right solution. We think you re going to like what happens when you call. ACCURACY IMMEDIACY 24/7 SUPPORT Fair enough. So based on the service calls we collect through our new service system, we ll identify potential problem trends, contact the appropriate OEM, and get to work on a solution. Back Home

10 MyAerospace.com Users Guide MyAerospace.com Registration Process

11 Table of Contents Getting Your Honeywell ID... p. 3 Verify and Password... p. 4 Setting up your MyAerospace Account... p. 5 Associate to a Company Automatically... p. 5 Associate to a Company by providing additional information... p. 6 Register your Company... p. 7 Requesting Access to Online Tools... p. 8 Entering Personal/Additional Information... p. 9 Entering your Aircraft Information... p. 9 Summary and Request Status... p. 10

12 Honeywell MyAerospace.com About this Guide This guide provides step-by-step instructions on the enhanced registration features and user interface available in the MyAerospace portal. Getting Your Honeywell ID Your Honeywell ID is the key to managing the various online tools available on the MyAerospace portal and other Honeywell websites. Access to the online tools is available to authorized customers and Honeywell employees, its subsidiaries and operating divisions, to conduct business with Honeywell. 1 To register go to At the sign in box, select [Register] to start the registration process. 2 A new window will pop-up, requiring you to enter your personal and contact information. Using a company address (john.doe@mycompany.com) will assist in accessing the correct account. 3 Enter the requested information and click the [Register] button

13 Getting Your Honeywell ID (cont.) 4 Read the Privacy Statement and select [I Agree] to continue or [I Do Not Agree] to cancel the process. 5 A message has been delivered to the address entered in your profile, select [Finish]. Check your inbox for a message from HoneywellIDAdministrator@honeywell.com Verify and Password 6 The link embedded in the message will direct you to a login screen. 7 Enter your password and select [Continue].

14 Setting up your MyAerospace Account. 8 If your password is correct, a "Welcome Aboard!" screen will appear. Select [Let's Get Started>] to continue. Associate to a Company Automatically If the address provided during the registration process matches an existing registered company, your account will be linked to the company. If your company is not listed, select [Add an additional company site] and continue steps in page 7 [Register your company] 9a Select all options that apply, and select [Continue >]. At this point your association is completed continue at page number 8 [Requesting Access for Online Tools]

15 Associate to a Company by providing additional information. If your address is not recognized by an existing registered company, you will be asked additional information to locate the correct account. 9b Select [Yes], if your company has conducted business with Honeywell or [No] to proceed to registering as a new company. In order to obtain your company information, you must provide an invoice number from a previous order placed with Honeywell. Locate the Sold-To Code and the Invoice Number. 9c Select [Yes] if you have this information. 9d Enter the Sold-To Code and Invoice Number, then select [Continue >] If the information is located, you will be presented with your company accounts, similar to the screen on page 5.

16 Associate to a Company by providing additional information (cont.) If the information is not located, you will be directed to a previous screen to select [Yes] to enter the data again, or select [No] for other options. Select [I need help...] to display a contact form. Enter detailed information about your case, and any other information to locate your company account, then select the [Submit>] button. Or select [Do not associate me...] to continue to step [Requesting Access to Online Tools] for limited guest access until you are associated to a company account. Registering your Company To register your company or continue as an individual user, select one of the following: If you select [Register Your Company], additional information such as purchasing information, billing and shipping address, trade type/dba, bank information, trade references, legal and financial information and tax documentation. Approval must be granted to users after required data has been entered. An notification will be delivered upon the completion of registration verification and approval.

17 Requesting Access to Online Tools Select the online tools you want to access. Tool availability varies for each user based on associated company or individual pre-established profile. 10 Select the [Request] button on the tools you want to access. 11 Select [Continue] to continue.

18 Entering Personal and Additional Information This section contains your personal information, some of the fields will auto-populate with information from your Honeywell ID profile. Create a Passphrase for additional security when authentication is required over the phone. 12 Enter your primary address. If more than one address is available based on your input during the registration process (page 5), choose one, then select [Continue >]. Additional information may be required depending on which tools you requested access for, some tools will require some extra information for you to work with them, or even to rely on the approval or denial of said access. Entering your Aircraft Information Depending on tool access selection, this information may be required For multiple aircraft, select [Add Aircraft] to enter additional aircraft information. Select [Finalize>] to complete the registration process.

19 Summary and Requests Status A summary of online tool requests and their status is displayed. Some auto-approved tools will be available for immediate use. Notifications will be distributed on tool requests requiring further action.

20 Courses: Honeywell offers system and component maintenance courses to supplement the offerings of the aviation training industry. A complete list, description and schedule of Honeywell Aerospace offerings are available on the Honeywell Aerospace web site at Honeywell can also provide quotes for customized training packages not listed in the catalog. About us: Headquartered in Phoenix, Arizona, Honeywell s Training Solutions provides customized training and support for the aviation industry. Count on Honeywell Training Solutions for the technical expertise, knowledge base and decades of field experience that will help you maximize operational value and performance of your aircraft. Aerospace Training Solutions For course reservations, visit us at Serving customers worldwide: Air transport Business aviation Regional General aviation Cargo Helicopters For additional information: Please contact Customer Training Solutions. training.solutions@honeywell.com Telephone: Fax: Authorized service centers Aviation training Military OEMs Providing customized training support to the aviation industry Honeywell Aerospace Customer Training Solutions and Flight Operations Support North 19th Ave. Phoenix, AZ Tel: Toll Free: International: Fax: C March Honeywell International Inc.

21 Count on Honeywell Training Solutions for the technical expertise, knowledge base and decades of field experience that will help you maximize operational value and performance of your aircraft. When you train, you want the real thing. Flight simulator and training device manufacturers turn to Honeywell for the hardware, source data and software, and engineering expertise that assure timely revisions and the highest fidelity available. Training providers rely on Honeywell for the courseware, training tools, delivery systems and fresh content that help keep pilots and maintenance personnel current. Our solutions enable delivery of the most accurate and realistic experience outside the cockpit. Training levels Familiarization Intermediate Line maintenance Special request Training courses Avionics Auxiliary Power Units (APU) Propulsion Environmental Control Systems (ECS) From PC-based individual training packages to complex systems engineering for full flight simulators, Honeywell Training Solutions offers a comprehensive slate of products and services. On-line and interactive multimedia training packages Real aircraft code running on a PC or laptop Custom course design and content development Pilot guides and maintenance manuals Factory-based maintenance courses Systems engineering and technical support Data and software licensing Hardware components With content from Honeywell s cadre of technical pilots and experienced engineers, pilot guides and maintenance manuals, as well as interactive computer-based training such as Honeywell s PC-FMS or PC-CMC, our training courseware development services provide you with content you can rely on for all your classroom training needs. Classroom training Held at Honeywell facilities Available at customer sites Training device hardware maintenance service and support Virtual classroom offers many benefits: Live, interactive, instructor-led distance learning online Up-to-date curriculum; new courses added continuously Internet broadcast courses No travel required Two-hour classes conveniently scheduled for students Global reach For more information, training.solutions@honeywell.com Honeywell backs its robust, flexible systems with the technical support, user documentation and instructor training only available from the source.

22 Honeywell Flight Technical Services Honeywell Aerospace 1944 East Sky Harbor Circle Phoenix, AZ aerospace.honeywell.com C / Honeywell International Inc. Back Home C Pilot Services.indd 1-2 4/10/16 1:08 PM

23 Honeywell Flight Technical Services Direct-To FMS Newsletter Experienced ATP-rated pilots provide instructor-led familiarization for flight operations and customer training personnel to increase pilot knowledge and safety, and ensure the successful launch of new products. Our highly-trained staff holds specialty seminars and provides web-accessible information (such as CBT and video) on Honeywell s innovative products and services to customers around the globe. Examples include: Publication designed to provide insight on technical issues affecting the Honeywell FMS community. Data link operations Navigation database technical updates and loading procedures NextGen and Performance Based Navigation updates FMS Upgrades and functionality Discussion of Operational procedures Aircraft database and SmartPerf learning Go-DirectTM RNP AR and Data Link Approval Consultancy Services Honeywell Flight Technical Services provides services to aid the operator in obtaining LOA and Ops Specs for RNP AR and FANS/ATN data link operations. FAA designated RNP AR Consultants provide the following: Entry-into-Service (EIS) Support For operators that have purchased new aircraft or new Honeywell equipment within the last 2 years. Navigation Database Validation RNP Monitoring Program FTS Program Pilots and training specialists also provide operational input to Includes software or hardware upgrades like Field Service Engineers and the Aero Cert Hotel, EASy II, CDS/R, or Primus Elite. Technical Support team in regard to An FTS program pilot can provide RNP AR support services Field Support for Operational Issues and questions Train the Trainer Support Audit and assist in curriculum development for training providers, air carriers, etc. operational issues. Provide support for corporate aviation departments to develop pilot familiarization training free of charge to the operator. This familiarization training may be conducted on site at the operator s location or via live webcasts. Pilot Familiarization Services at Operator s Location Operators requesting additional familiarization training on any Honeywell avionics products (FMS, Weather Radar, training programs Informational Webinars Web-based presentations on products, Honeywell Pilot Gateway - pilots.honeywell.com mandates and other operational issues that The Pilot Gateway is an easy to use interface that provides users with free are important to the operator are regularly access to many of Honeywell s BGA technical publications, videos and broadcast by a FTS Program Pilot or Training other resources tailored to pilots and easily allows them to ask operational Specialist. questions and provide feedback. Included in the Gateway are: Webinars cover various subjects and are free Alerts and updates for pilots - Service Information Letters of charge. Documents and Resources Pilots Guides, Familiarization Videos, Recordings of all presented webinars are GDC Services, Online learning VNAV, EGPWS, RAAS, Autopilot, etc.) outside made and available to operators on the the EIS 2 year period. Go-Direct Newsletters website. This site does not Calendar of upcoming events require a log in. Direct access to My GDC All familiarization materials are provided digitally, free of charge. Printed material is available at a charge to the operator. For a listing of available familiarization Current News and Updates Honeywell Operator s Conferences Contact Us Link to submit general questions, technical issues Flight Technical services provides breakout questions or leave feedback services, please contact the Flight Technical sessions for pilots that focus on products Services group at FTS@honeywell.com. and issues that are important to flight You can contact the Flight Technical Services group either through the operations. Operator conferences are held at Pilot Gateway link pilots.honeywell.com or by at FTS@honeywell.com various locations throughout the year. Back Home C Pilot Services.indd 3-4 4/10/16 1:08 PM

24 Honeywell Flight Technical Services Direct-To FMS Newsletter Experienced ATP-rated pilots provide instructor-led familiarization for flight operations and customer training personnel to increase pilot knowledge and safety, and ensure the successful launch of new products. Our highly-trained staff holds specialty seminars and provides web-accessible information (such as CBT and video) on Honeywell s innovative products and services to customers around the globe. Examples include: Publication designed to provide insight on technical issues affecting the Honeywell FMS community. Data link operations Navigation database technical updates and loading procedures NextGen and Performance Based Navigation updates FMS Upgrades and functionality Discussion of Operational procedures Aircraft database and SmartPerf learning Go-DirectTM RNP AR and Data Link Approval Consultancy Services Honeywell Flight Technical Services provides services to aid the operator in obtaining LOA and Ops Specs for RNP AR and FANS/ATN data link operations. FAA designated RNP AR Consultants provide the following: Entry-into-Service (EIS) Support For operators that have purchased new aircraft or new Honeywell equipment within the last 2 years. Field Support for Operational Issues and questions also provide operational input to Field Service Engineers and the Aero Cert Hotel, EASy II, CDS/R, or Primus Elite. Technical Support team in regard to operational issues. familiarization training free of charge to the operator. This familiarization training may be conducted on site at the operator s location or via live webcasts. Pilot Familiarization Services at Operator s Location Operators requesting additional familiarization training on any Honeywell avionics products (FMS, Weather Radar, Navigation Database Validation RNP Monitoring Program FTS Program Pilots and training specialists Includes software or hardware upgrades like An FTS program pilot can provide RNP AR support services Informational Webinars Web-based presentations on products, mandates and other operational issues that Train the Trainer Support Audit and assist in curriculum development for training providers, air carriers, etc. Provide support for corporate aviation departments to develop pilot training programs Honeywell Pilot Gateway - pilots.honeywell.com The Pilot Gateway is an easy to use interface that provides users with free are important to the operator are regularly access to many of Honeywell s BGA technical publications, videos and broadcast by a FTS Program Pilot or Training other resources tailored to pilots and easily allows them to ask operational Specialist. questions and provide feedback. Included in the Gateway are: Webinars cover various subjects and are free of charge. Recordings of all presented webinars are Alerts and updates for pilots - Service Information Letters Documents and Resources Pilots Guides, Familiarization Videos, GDC Services, Online learning VNAV, EGPWS, RAAS, Autopilot, etc.) outside made and available to operators on the the EIS 2 year period. Go-Direct Newsletters website. This site does not Calendar of upcoming events require a log in. Direct access to My GDC All familiarization materials are provided digitally, free of charge. Printed material is available at a charge to the operator. For a listing of available familiarization Honeywell Operator s Conferences Flight Technical services provides breakout Current News and Updates Contact Us Link to submit general questions, technical issues questions or leave feedback services, please contact the Flight Technical sessions for pilots that focus on products Services group at FTS@honeywell.com. and issues that are important to flight You can contact the Flight Technical Services group either through the operations. Operator conferences are held at Pilot Gateway link pilots.honeywell.com or by at FTS@honeywell.com various locations throughout the year. Back Home C Pilot Services.indd 3-4 4/10/16 1:08 PM

25 Honeywell Flight Technical Services Honeywell Aerospace 1944 East Sky Harbor Circle Phoenix, AZ aerospace.honeywell.com C / Honeywell International Inc. Back Home C Pilot Services.indd 1-2 4/10/16 1:08 PM

26 HTF7250G Turbofan Engine HIGH PERFORMANCE. INCREASED RELIABILITY. LOWER COST OF OWNERSHIP. The Latest in Business Jet Engine Innovation

27 Delivering enhanced customer value through design innovation, the HTF7250G engine demonstrates Honeywell s commitment to propulsion system engineering and technological development for business class aircraft. Advanced performance with a lower The Honeywell HTF7250G turbofan engine delivers an optimal balance of performance and value that maximizes propulsion efficiency with lower maintenance costs and highly reliable operation for today s business jet operators. Customer Focused Design Incorporating a breadth of customer input from operators, service center engineers and aircraft manufacturers, the HTF7250G delivers the power with significantly lower parts count and up to 30 percent lower cost of ownership. Combining ISA+15C flat rating with best-in-class fuel efficiency is accomplished by a wide cord damperless fan, SLE compressor airfoil technology, a low-emissions effusioncooled combustor, transpiration cooled HPT blades, and a dual-channel FADEC. The HTF7250G is available with a full nacelle and thrust reverser. Enhanced Maintainability The HTF7250G incorporates many timeand cost-saving maintenance features. Individual LRUs can be replaced on average in 20 minutes or less with no shimming, rigging or adjusting using standard hand tools with nothing more than an idle power leak check. QEC engine changes can be accomplished in three hours with two technicians. Using MSG-3 protocol and 39 strategically placed borescope ports for 360-degree visibility to all gas path components, the HTF7250G is a true on-condition engine.

28 Key HTF7250G Engine Benefits Increased Customer Value Improved Fuel Efficiency Lower Cost of Maintenance Reduced Noise Signature World-Class Reliability Excellent Durability cost of ownership. Key Honeywell Advantages World-Class Customer Service and Support Honeywell s global support network includes over 22 service centers trained to maintain the HTF7250G. Available MSP programs provide predictable engine maintenance costs for either on-condition or fixed-interval maintenance plans. On-line service resources for parts, warranty, technical publications, Authorized Service Center Network, Spotlight (TM) troubleshooting tool, and much more available through web portal. HTF7250G Engine Specifications Thrust: Flat Rating: Fan Diameter: Dry Weight: Bypass ratio: lbf (pounds force) ISA + 15 C (86 F) 34.2 in kg (1364 lbs) Development Capability We apply our 50 years of propulsion systems experience and industryleading engine integration expertise to the ongoing development of new engine systems, technology upgrades and product enhancements. Dedicated Resources Focused organization that understands the propulsion needs and requirements of aircraft operators with over 65,000 fielded propulsion engines and more than 241 million service hours. Operational Performance With our Six Sigma methodology and ongoing technological investments, Honeywell delivers optimal value and peak performance. Advanced Technologies We use the newest processes, materials and concepts to create propulsion system solutions with high reliability, improved performance, and cost-effective operation. Global Network Worldwide resources that span the Americas, Europe, Middle East, Africa, Asia and the South Pacific, providing 24/7/365 support with a full range of maintenance, repair, overhaul and customer service capabilities.

29 Honeywell Aerospace Honeywell is a leading global provider of integrated avionics, engines, wheels and brakes systems and service solutions for aircraft manufacturers, airlines, business and general aviation, military, space and airport operations. For more information on Honeywell Aerospace, visit us online at www. honeywell.com/aero Engines, Systems & Services Honeywell P.O. Box Phoenix, Arizona Domestic: International: A September Honeywell International Inc.

30 Honeywell.com EEI Software, Setup, Download and Basic Review e EEI V Document control number Honeywell Proprietary

31 Honeywell.com Benefits of the EEI Program EEI program is a common engine interface program developed for the HTF7000/HTF7250G series and the TFE731 engine models EEI program allows ECU downloads of multiple engines at the same time Provides detailed fault isolation information (MCID s) Provides trend and engine exceedance data Version has been qualified on: WIN95, 98, 2000, NT, ME and XP (has not been qualified for use on VISTA or Windows 7) Note: The following presentation is presented primarily for HTF7250G Operators. Functional and Program Use Differences Exist for other HTF7000/HTF7250G and TFE731 Operators 2 Document control number Honeywell Proprietary

32 Honeywell.com HTF7250G EEI Interface Kit HTF Kit p/n XX Kit includes: FADEC Interface Cable (grey) - P/N Manufactured by Honeywell USB interface device Manufactured by Edgeport EEI Software CD (also available on-line) Carrying Case Supplied at delivery free of charge Replacement parts/kits available through Honeywell For Additional Information contact Honeywell Tech Ops Center (800) Document control number Honeywell Proprietary

33 Honeywell.com EEI Software Now Available On e-engine 4 Document control number Honeywell Proprietary

34 Honeywell.com EEI Software Download Select HTF7000 Software 5 Document control number Honeywell Proprietary

35 Honeywell.com EEI Software Download Look for EEI Document control number Honeywell Proprietary

36 Honeywell.com EEI Software Download 1. Select EEI V 2.09 File, choose Open, then double click Setup.exe 2. After install above, select EEI Update File, choose Save, then save in EEI Folder for later use EEI Download is a 2 part process 7 Document control number Honeywell Proprietary

37 Honeywell.com EEI e-engine Interface. 8 Document control number Honeywell Proprietary

38 Honeywell.com Initial Start Up Create an Operator Name and User Name EEI allows multiple users on the same P.C. and maintains the settings based on the user name. This Log In is not a password type of log in. No need to create a password. The Operator and User name created will also appear in the Download comments after Download. 9 Document control number Honeywell Proprietary

39 Honeywell.com Initial Start Up There are 2 Modes of EEI Operation: BASIC mode and Full UP mode Check Basic mode for normal Download and Review Uncheck Basic mode for Full Up mode (Use Full Up Mode to Add/Delete or Change ECU and Aircraft information) 10 Document control number Honeywell Proprietary

40 Honeywell.com Initial Start Up / EEI Update After initial download and start up, select File, EEI Update and select EEI Update zip file that was downloaded from e-engine earlier. 11 Document control number Honeywell Proprietary

41 Honeywell.com Change unit selections 12 Document control number Honeywell Proprietary

42 Honeywell.com Select Aircraft 13 Document control number Honeywell Proprietary

43 Honeywell.com Quatech Card Com Port Set Up HTF7XXX COM Through Quatech QSP-200/300BA-G (PCMCIA ). If not previously installed carefully follow Supplied CD Installation Instructions. 14 Document control number Honeywell Proprietary

44 Honeywell.com Edgeport USB Set Up HTF7XXX COM Through Edgeport USB Converter. If not previously installed carefully follow Supplied CD Installation Instructions. 15 Document control number Honeywell Proprietary

45 Honeywell.com Com Port Set Up Quatech/Edgeport Select Configure, then Com Port Configuration HTF7XXX Uses Four Com Ports Note: Ports Must be Consecutive i.e. 1-4 based on PC Resources Assigned Through the Quatech PCMCIA Card or Edgeport USB Converter 16 Document control number Honeywell Proprietary

46 Honeywell.com Quatech Com Port Set Up Setup Can be Confirmed Through Device Manager Start Com Port for EEI Will Be Com Document control number Honeywell Proprietary

47 Honeywell.com Edgeport Com Port Set Up Setup Can be Confirmed Through Setup Device Manager Start Com Port for EEI Will Be Com Document control number Honeywell Proprietary

48 Honeywell.com Edgeport Configuration Select Run c:\windows\system32\edgeport.exe Select the Ports Flag. Use the drop downs to select Industrial Settings to RS422 No Terminating Resistor. Select Update and Save Config 19 Document control number Honeywell Proprietary

49 Honeywell.com Enter Starting Com Port Select Starting Com Port. Remaining Com Ports Will Auto Fill With Consecutive Numbers 20 Document control number Honeywell Proprietary

50 Honeywell.com Quatech Cable Set UP Sl Select OPTIONS then Display Connection Diagram 21 Document control number Honeywell Proprietary

51 Honeywell.com Edgeport Cable Set UP Sl Select OPTIONS then Display Connection Diagram 22 Document control number Honeywell Proprietary

52 Honeywell.com Edgeport USB Converter Sl Select OPTIONS then Display Connection Diagram 23 Document control number Honeywell Proprietary

53 Honeywell.com Cable Set UP 24 Document control number Honeywell Proprietary

54 Honeywell.com Download 25 Document control number Honeywell Proprietary

55 Honeywell.com Download Cable Connection Status Download Selectable Single Engine or Select All Engines 26 Document control number Honeywell Proprietary

56 Honeywell.com Download Results Page 27 Document control number Honeywell Proprietary

57 Honeywell.com Review 28 Document control number Honeywell Proprietary

58 Honeywell.com Review 29 Document control number Honeywell Proprietary

59 Honeywell.com Review Summary Page Engine Maint. Data Will be Green if Clear, Red if Activity. Select Corresponding Tab to View Activity/Troubleshoot. 30 Document control number Honeywell Proprietary

60 Honeywell.com Review e Maintenance a Conditions o 4 Digit Code Tied Directly to LMM Troubleshooting. MCID XXXX Syntax Very Effective For LMM Search for Fault Isolation i.e. MCID 1505 Tabular Data Provided for First and Last Occurrence of the MCID 31 Document control number Honeywell Proprietary

61 Honeywell.com Review Trend Data 32 Document control number Honeywell Proprietary

62 Honeywell.com Review Event Data Event Data Presented in Tabular and Graphical Format. Graphs are Scalable Using Corner Anchors. Event Data Recorded is 2 Minutes Prior to the Event Occurrence and 1 Minute After Event tpoint. Data is Combined Slow Scan (Black) and Fast Scan (Red) Data 33 Document control number Honeywell Proprietary

63 Honeywell.com Review Chronology 34 Document control number Honeywell Proprietary

64 Honeywell.com Realtime 35 Document control number Honeywell Proprietary

65 Honeywell.com Realtime Realtime Function displays and saves Realtime variables stored in ECU RAM. Realtime Function is intended d to give you the ability to view and record engine parameters under operational conditions Realtime Function Features Strip Chart, Analog and Discrete Display 36 Document control number Honeywell Proprietary

66 Honeywell.com MC Monitor Allows for Review of MCID s Residing in NVRAM that Have not Yet Met Conditions to Move Into Write Buffers and Display as MCID 37 Document control number Honeywell Proprietary

67 Honeywell.com ing downloads to Jet-Care Copy files to Stored C:\EEI\Download Memory jogger CEEIDOWNLOAD downloads to care.com com 38 Document control number Honeywell Proprietary

68 Powerplant Warranty The HTF7350 Warranty is designed to ensure maximum in service operation for your propulsion system. The Warranty is in effect for five years and includes the following powerplant coverage. For more warranty information, contact Honeywell at U.S , International , or visit IPPS Component Fixed Structural Nacelle Components Moveable Structural Nacelle Components Non-Structural Nacelle Components Term 5 years or 3,000 hours 5 years or 3,000 hours 5 years or 3,000 hours Engine Components 5 years or 3,000 hours See next page for detailed component coverage descriptions

69 Powerplant Warranty IPPS Component Fixed Structural Nacelle Components Moveable Structural Nacelle Components Non-Structural Nacelle Components Descritpion Such as inlet, attachment flange, inner and outer skins and bulkhead, and thrust reverser (Not including: thermal anti-ice provisions, brackets, hinges, latches, door lands, seals, attachment features and fasteners). Such as access doors, hinges, latches, fan cowl doors (upper and lower), tie rods, and pins. Such as pneumatic ducts, electrical, hydraulic, fire detection, fuel, and air turbine starter duct. (all other items not specifically noted in other categories).

70 HTF7250G Thrust Reverser System Description HONEYWELL CONFIDENTIAL: This copyrighted work and all information are the property of Honeywell International Inc., contain trade secrets and may not, in whole or in part, be used, duplicated, or disclosed for any purpose without prior written permission of Honeywell International Inc. All rights reserved. ECCN 9E991 - The technical data in this document is under the jurisdiction of the Export Administration Regulations (EAR). "Diversion contrary to U.S. law is prohibited" Page 0 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

71 Agenda Thrust reverser system description General description System components Page 1 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

72 General Description Physical characteristics Length - 44 inches Upper Door Forward diameter inches Upper - Outer Skin Exhaust diameter inches Systems Removed Panel Margined weight pounds Forward fixed structure Composite fire wall Composite forward barrel Aluminum machined beams Composite beam outer skins Doors Aluminum machined doors Aluminum outer skins Forward systems panels Provide external loft transition to circular Forward Firewall cross section Circular cross section aft from leading edge of doors Clocking achieved by Removing systems panels Rotating thrust reverser ±5 or ±10 degrees Reinstalling systems panels without rotation Lower Systems Panel Side Beams Lower Doors Page 2 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

73 General Description Page 3 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

74 System Components Aircraft mounted WOW and WSU relays Throttle quadrant assembly (TQA) Maintenance Enable switch Isolation control unit (ICU) Powerplant mounted Directional control unit (DCU) Pivot door actuators (PDAs) Hydraulic primary lock (HPL) Electro-hydraulic primary lock (EHPL) Stow switches Deploy switches Multiplexer Ground test switch Primary lock assembly Electronic control units (ECUs) Page 4 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

75 System Components WOW and WSU relays Inboard WSU relay Provides 28VDC to LH ICU and DCU Provides 28VDC to RH EHPL and Rev Balk Inner WOW relay Provides 28VDC to LH ICU and DCU Provides 28VDC to RH EHPL and Rev Balk Outboard WSU relay Provides 28VDC to RH ICU and DCU Provides 28VDC to LH EHPL and Rev Balk Outer WOW relay Provides 28VDC to RH ICU and DCU Provides 28VDC to LH EHPL and Rev Balk Page 5 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

76 System Components Page 6 Throttle quadrant assembly (TQA) Reverse balk solenoid Prevents throttle movement beyond reverse idle until the thrust reverser is fully deployed Includes economizer circuit to reduce electrical current demand, prevents ECUs from sensing actual solenoid faults TR request switches Provide 28VDC high side power to the TR solenoids when the throttle lever is at or below the reverse idle position 2 switches per throttle lever (4 total) Rotary variable differential transformer (RVDT) Transmits throttle lever angle (TLA) to engine FADEC Take-off region: TLA > 46 Climb region: 40 < TLA < 46 Cruise region: 2 < TLA < 40 Forward idle region: -7 < TLA < 2 Typical location of TR request switches: -15 Reverse idle region: -34 < TLA < -31 Reverse region: -105 < TLA < -34 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

77 System Components Throttle quadrant assembly (TQA) Page 7 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

78 System Components Maintenance Enable switch Used during ground maintenance procedures Suppresses logging of MCIDs Used during inhibition procedures Page 8 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

79 System Components Maintenance Enable switch Page 9 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

80 System Components Page 10 Isolation control unit (ICU) Solenoid operated isolation valve Controls the flow of hydraulic pressure to the TR system components Pressure switch Provides an indication to the FADEC when hydraulic pressure is present downstream of the isolation valve Dual redundant switches, one per ECU channel Normally closed, open = pressure Inhibit lever Mechanically prevents isolation valve from opening Activates inhibit switch G250 specific labels: OPEN = un-inhibited, CLOSE = inhibited Inhibit switch Provides an indication to the FADEC when the inhibit lever is in the inhibited position Dual redundant switches, one per ECU channel Normally closed, open = inhibited Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

81 System Components Isolation Control Unit (ICU) Page 11 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

82 System Components Directional Control Unit (DCU) Solenoid operated directional control valve Ports fluid to the PDAs, HPL, and EHPL to control door movement and locking Time delay circuit Ensures that the PDAs have moved to the overstow position prior to S- hook release and provide adequate time for EHPL balk retraction. Page 12 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

83 System Components Directional Control Unit (DCU) Page 13 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

84 System Components Pivot door actuator (PDA) 2 PDAs per TR assembly, upper and lower Open or close pivot doors based on hydraulic pressure commands from the DCU Contain an integral locking mechanism to prevent un- commanded extension Manual lock/unlock mechanism for inspection/test Page 14 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

85 System Components Pivot door actuator (PDA) Page 15 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

86 System Components Hydraulic primary lock (HPL) Hydraulic actuator Pressurize to retract Rotates the left hand (aft looking forward) s-hook to the unlocked position when retracted Ports hydraulic pressure to the EHPL when retracted Page 16 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

87 System Components Hydraulic primary lock (HPL) Page 17 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

88 System Components Electro-Hydraulic primary lock (EHPL) Solenoid operated balking device Prevents hydraulic actuator from retracting when de-energized energized Balk switch Provides balk device position indication to the FADEC. Dual redundant switches, one per ECU channel Normally closed, open = un-balked Hydraulic actuator Pressurize to retract Rotates the right hand (aft looking forward) s-hook to the unlocked position when retracted Ports hydraulic pressure back to the DCU when retracted Page 18 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

89 System Components Electro-hydraulic primary lock (EHPL) Page 19 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

90 System Components Stow switches 4 switches per TR assembly Upper door, left hand switch Upper door, right hand switch Lower door, left hand switch Lower door, right hand switch Dual redundant switch contacts One per ECU channel Normally closed, open = not stowed Actuated by striker plate on door Page 20 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

91 System Components Stow switches Page 21 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

92 System Components Deploy switches 2 switches per TR assembly One for upper door One for lower door Dual redundant switch contacts One per ECU channel Normally closed, open = deployed Actuated by knob on inner blister panel Page 22 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

93 System Components Deploy switches Page 23 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

94 System Components Multiplexer Combines left hand upper and lower stow switch signals into a single resistance signal Combines right hand upper and lower stow switch signals into a single resistance signal Combines upper and lower deploy switch signals into a single resistance signal Page 24 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

95 System Components Multiplexer Page 25 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

96 System Components Ground test switch Used to deploy/stow thrust reverser during ground maintenance Single switch contact shared by both ECU channels Normally open, closed = ground test active Page 26 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

97 System Components Ground test switch Page 27 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

98 System Components Primary lock assembly Consists of s-hook, door hooks, lever, link, spring Released by application of retract pressure Doors must be in overstow position Actuator t piston pulls link, rotates t lever, rotates t s-hook Returns to locked position with removal of pressure Return spring moves mechanism and actuator piston to locked position Engage when door hooks approach stow position S-hook ratchets t as door hooks pass to overstow position Link, lever, and actuator held by spring Page 28 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

99 System Components Primary lock assembly Actuator Fork Door Hook Link Lever Return Spring S-Hook Door Hook Page 29 Use or disclosure of information contained on this page is subject to the restrictions on the cover. HONEYWELL CONFIDENTIAL

100 Publication No. SE Revision 5-21 MAY 2014 TECHNICAL MANUAL INSTALLATION INSTRUCTIONS ELECTRONIC ENGINE INTERFACE (EEI) SOFTWARE VERSION / FOR MODEL TFE731 AND HTF7000 ENGINES PART NUMBER SW /-1002 THIS MANUAL SUPERSEDES PUBLICATION NO. SE , DATED 17 MAY 2012 This document and all information and expression contained herein are the property of Honeywell International, Inc., are loaned in confidence, and may not, in whole or in part, be used, duplicated, or disclosed for any purpose without prior written permission of Honeywell International, Inc. All rights reserved. This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991, NLR Eligible. HONEYWELL Ground Support Solutions 3520 Westmoor St. South Bend, IN

101 SE Electronic Engine Interface (EEI) Version / TFE731 and HTF7000 Software Installation Instructions Please follow these instructions to install your new copy of the EEI software Version EEI or EEI EEI - Operating system Requirements EEI Version EEI compatible with Windows 95, Windows 98, Windows ME, Windows NT, Windows 2000 and Windows XP. It is not compatible with Windows Vista or Windows 7 and should not be used with these operating systems. EEI Version EEI compatible with Windows 7 32-bit Enterprise and Windows 7 64-bit Professional edition. It is not compatible with versions of Windows lower than Windows 7 and should not be used with these operating systems. Applicable TFE731/HTF7000 EEI/ECTM Kit PNs L G-100 (Astra SPX) F50EX F900EX TFE Classic TFE All (Service Center Kit) L45 w/ RE HS900XP HTF X EEI installation package EEI is available in a single Installation CD or as EEI installation zip file in Honeywell MyAerospace Portal website (Software & Data). This Installation CD will run automatically when the autorun feature has been enabled on the target PC. The steps outlined in Appendix A will guide the user through the EEI installation steps on the target PC. NOTE: EEI does not provide drivers that are needed for a chosen back-up device. Appendix B details Honeywell MyAerospace Portal site login and locating the EEI installer. Appendix C details the EEI Update Feature and download from Honeywell MyAerospace Portal. Honeywell International Inc. Do not copy without express permission of Honeywell. 1

102 SE Appendix A Detailed Installation Sequence Displays Step by step installation sequence for EEI. 1. Insert the EEI Software Distribution CD in your Laptop s CD Drive OR unzip the installation zip file downloaded from Honeywell MyAerospace Portal website. The part number for EEI are: a. EEI Version EEI : PN SW b. EEI Version EEI : PN SW If the CD does not auto-start the installation procedure, then run the setup.exe file on the CD (by double-clicking this file name shown in Figure A-1). If EEI installer is downloaded from Honeywell MyAerospace Portal website, double click on setup.exe from the extracted folder in above step. Figure A-1. Distribution Disk Contents and Location of Setup.exe 3. Follow the instructions as the software installs. Honeywell recommends accepting all defaults (images below may differ for EEI ). Honeywell International Inc. Do not copy without express permission of Honeywell. A1

103 SE Figure A-2. Initial EEI Installation Display Figure A-3. Accepting EEI Application License Terms Honeywell International Inc. Do not copy without express permission of Honeywell. A2

104 SE Figure A-4. Selecting the EEI Destination Folder (available only in EEI ) Figure A-5. Installation Progress Display Honeywell International Inc. Do not copy without express permission of Honeywell. A3

105 SE Figure A-6. Prompt to Optionally View the Readme File Figure A-7. Displaying the Readme File Honeywell International Inc. Do not copy without express permission of Honeywell. A4

106 SE Figure A-8. Installation Completion Message 4. Once the installation is complete, start the EEI Application using either the desktop icon (Figure A-9) or All Programs => e-engine Interface => Launce EEI (Figure A-10). NOTE: If installing EEI , perform EEI Update immediately after successful installation. Figure A-9. EEI Desktop Icon Honeywell International Inc. Do not copy without express permission of Honeywell. A5

107 SE Figure A-10. EEI Programs Start Sequence Honeywell International Inc. Do not copy without express permission of Honeywell. A6

108 SE Appendix B Honeywell s MyAerospace Portal Website - EEI Software Installer NOTE: If you are registered with the Honeywell s MyAerospace portal website ( you are encouraged to download the EEI software from that location (Figure B-3) - as this website always has the most current version of the software. Login to the portal website ( Then under the SOFTWARE & DATA tab, select the Engine and APU Software Downloads menu item as shown in Figure B-1 to access the EEI Software Downloads Page (hereafter referred to as download page ) as shown in Figure B-2. Figure B-1. Navigate to EEI Software Download Page After Login to MyAerospace Honeywell International Inc. Do not copy without express permission of Honeywell. B1

109 SE Figure B-2. EEI Software Downloads Page To download the EEI software select either HTF7000 Software or TFE731 Software in the Engine Software Downloads listbox in the download page shown in Figure B-2. Then follow the steps shown in the following screens. Select the button Download Software Files in Select listbox as shown in Figure B-3 or Figure B-4. Note that the appropriate Download Software Files item in the listbox under the desired EEI software version header should be selected - the latest version which is or for the previous version. B2 Honeywell International Inc. Do not copy without express permission of Honeywell. Back Back Home Home

110 SE Figure B-3. EEI Software Download Instructions Through HTF7000 Follow instructions shown in the download page. You can view this document by selecting the View Download Installation Instructions item in the Select listbox. Honeywell International Inc. Do not copy without express permission of Honeywell. B3

111 SE When downloading through TFE731, make sure to first select the Tools all TFE731 Installation item in the Select listbox in the download page. Then select the Download Software item on the third listbox displayed on the download page. Figure B-4. EEI Software Download Instructions through TFE731 Honeywell International Inc. Do not copy without express permission of Honeywell. B4

112 SE Appendix C EEI Update Feature EEI Update contains updates to the Aircraft Fleet database along with other configurable parameters that are released after a baseline release of EEI software. This file is used to update the EEI local database to the latest fleet information supported by Honeywell Engines. EEI Update is a zip file containing information about the latest fleet supported by EEI. Download the EEI Update.zip file and import in to EEI using the EEI Update function from File menu. The EEI Update file is available under the Software Downloads Page in the MyAerospace portal website. Refer to Figure C-1. The EEI Update file is currently only available and compatible for the EEI software version but in the future EEI Update files may also become available as necessary for the EEI software version. Figure C-1. EEI Update in MyAerospace Portal Website Honeywell International Inc. Do not copy without express permission of Honeywell. C1

113 36-150[IAI]-2 Auxiliary Power Unit The Auxiliary Power Unit offers world-class reliability and enhanced mission performance in a compact design. The APU is certified for in-flight operation and provides a matched bleed air source to the environmental control system for cabin comfort in temperature extremes. Electrical power is available to power cockpit and galley systems. The APU electrical generation system provides electrical power for main engine starting; therefore, reducing the burden of the main engine. The advanced operational capabilities of overall allow for lower operational costs with enhanced convenience, comfort and efficiency. G280 Operators Handbook

114 Commercial Warranty for the Gulfstream G [IAI-2] APU Administrative Overview Warranty claims for the Honeywell [IAI-2] APU may be submitted on an Honeywell Engines, Systems and Services Warranty Claim form, by claim entry into the Honeywell Engines, Systems and Services CHAMPS system, or customer invoice/purchase order providing all required information listed below. Warranty claims will be honored for work accomplished at Honeywell Authorized Service Facilities or within the guidelines of the Honeywell warranty policy. All warranty claims are authorized by Honeywell, at Honeywell's discretion. All hardware valued at greater than $500 must be returned with a warranty claim form for warranty consideration. Honeywell will replace or repair at its option any manufactured non-conforming hardware during the effective warranty period set forth below. Warranty replacement with new hardware is at the discretion of Honeywell. The following information is required to process an APU warranty: Date of purchase / Date of delivery Date of installation and removal APU Part Number and component or LRU Part Number, if applicable, including dash numbers Corresponding APU and component or LRU Serial Numbers Aircraft number and date of entry into service (or date of spare part installation) Total flight hours (TSN) accrued on item or component Description of claimed non-conformance and circumstances Date of claimed non-conformance Itemized account of labor hours directly expended in performing repair, if applicable Itemized account of material furnished by Owner directly incorporated in the repair, if applicable Purchase Order Warranty coverage includes: Parts and labor to repair the APU or APU component Shipping of the APU or APU component within the continental United States, when warranty is accepted.

115 Warranty coverage does not include: Handling fees APU or LRU removal and / or reinstallation New replacement parts except at Honeywell discretion Rental of APU's Component exchange fees Scheduled and routine maintenance (HSI, inspections, etc.) Warranty Program Details - Definitions The following words or phrases have the noted meanings: 1. "Seller" means Honeywell Engines, Systems and Services and its affiliates, and business units of Honeywell Inc. 2. "Owner" means the legal or registered owner of the APU. 3. "APU" means a new [IAI-2] Auxiliary Power Unit, Part Number X delivered for commercial use. 4. "Parts" means components or Line Replaceable Units (LRU's) of the APU which may be repaired or replaced by Seller or its Authorized Facility. 5. "APU Operating Hours" means the Total Since New (TSN) accumulated on the APU or its Parts, as recorded by the APU hour-meter. 6. "Installation" means the date the APU or Part is originally installed on the aircraft. 7. "Failure", "Malfunction", or "Non-Conformance" in an APU or Part means breakage or improper function. 8. "Normal Wear and Tear" means the gradual and expected deterioration of an APU or Part, the need for regular overhaul and periodic maintenance and consumable hardware, and does not constitute a failure or malfunction under this warranty. Warranty Coverage Seller warrants to the Owner that each APU sold for installation as original equipment on new aircraft and new spare APU's will as set forth below comply with applicable Seller drawings and specifications and be free from defects in material and workmanship. These warranties shall run to the original purchaser, its successors, assigns and customers when they are the Owner.

116 Duration of Warranty ORIGINAL EQUIPMENT APU's Duration will be sixty (60) months from date of delivery to Owner, or two thousand five hundred (2,500) APU operating hours, whichever first occurs. NEW SPARE APU's Duration will be sixty (60) months from date of shipment to the Owner, or two thousand five hundred (2,500) APU operating hours, whichever first occurs. Warranty claim determination will be based on the data supplied to Seller by the Owner, its successors and customers when they are the Owner, substantiated by inspection, testing, failure analysis, and information from Seller's representatives. Seller will have the sole right to determine whether the failure qualifies under the terms and conditions of this warranty. NEW SPARE PART WARRANTY Duration will be twelve (12) months from date of shipment or six (6) months from date of installation of the new spare Part on the APU, whichever first occurs. Seller warrants to the Owner that each new spare part sold for installation on an APU will, at the time of shipment or installation as identified above, conform to the applicable Seller drawings and specifications, and be free from defects in material and workmanship. REPAIR AND OVERHAUL (after original equipment/spare warranty expiration) Duration will be one hundred eighty (180) days from date of shipment from Seller or ninety (90) days from date of installation of the repaired or overhauled Part on the APU, whichever first occurs. Repair and overhaul warranty is applied at the expiry of the original equipment, new spare APU and new spare part warranties, and does not in any way extend the original warranty periods. RESPONSIBILITY OF SELLER If an APU or Part is returned to Seller or a Honeywell Authorized Service Center and is found by Seller, in its sole discretion, to have failed as a result of a failure in material or workmanship covered by this warranty, Seller will at no cost to the Owner: 1. Repair or replace, at Seller s sole option, the failed APU or Part. Any APU or Part which is replaced or exchanged will become the property of Seller. 2. Assume round trip shipping costs for failed or non-conforming APU's or Parts within the continental United States; however if Seller's inspection discloses the returned APU or Part does not require repair or replacement under warranty, Seller's usual inspection charges will apply. 3. The correction of any failure or malfunction will in no way extend the period of this warranty. 4. Seller reserves the right to make changes in its products without incurring any obligation to incorporate the same on previously delivered APU s or Parts.

117 RESPONSIBILITY OF OWNER The following conditions govern the application of this warranty: 1. All Owners must send in a Warranty Registration Card form within thirty (30) days of becoming an Owner. Warranty registration cards are in the Engine Log book or may be obtained from Seller by writing to: HONEYWELL P.O. Box 29003, Mail-stop Phoenix, Arizona ATTENTION: WARRANTY DEPARTMENT 2. Owner will assure that records are maintained which will accurately reflect APU operating hours and when maintenance was performed. At Seller s request, such records will be provided to substantiate warranty claims. 3. Owner will be responsible for costs of removal and reinstallation. 4. Scheduled routine maintenance and inspection, including, but not limited to: disassembly, assembly, cleaning, inspection, replacement of consumable hardware such as gaskets, filters, packings, igniter plugs, nuts, bolts, etc., minor repairs for cracks, nicks, dents, and all repair effort required as a result of Normal Wear and Tear are the responsibility of the Owner and are specifically excluded from this warranty. 5. Owner shall submit a warranty claim within the warranty period and the affected APU or Part must be returned to Seller, accompanied by a Honeywell Standard Claim form, within thirty (30) days after discovery of such defect or nonconformity. 6. APU's and LRU's returned without the required warranty data are subject to return and/or repair charges. EXCLUSIONS The provisions of this warranty will not apply if the APU or Part has been subjected to: a. Any maintenance, repair, installation, storage, operation, use, handling or environmental condition which is improper or not in accordance with Seller manuals, Bulletins, or other written instructions; or b. Any alteration, modification or repair by anyone other than Seller or its authorized representatives which adversely affects the normal operation and performance of the APU; or c. Any accident, misuse, neglect, or negligence after delivery by Seller; or d. Ingestion of foreign material or foreign object damage; or e. Lack of incorporation of Service Bulletins related to the cause of failure.

118 This warranty will not apply to: LIMITATIONS a. Any APU or Part to the extent that the defect or nonconformity is attributable to a Part not supplied by Seller; or b. Malfunction or failure due to accident, non-conformance, or noncompliance with Seller's operating, scheduled maintenance or other pertinent instructions. THIS WARRANTY IS EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER WRITTEN OR ORAL, EXPRESS, IMPLIED OR STATUTORY, INCLUDING, BUT NOT LIMITED TO, ANY IMPLIED WARRANTIES OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE OR USE AND WARRANTIES ARISING FROM COURSE OF PERFORMANCE, DEALING, USAGE OR TRADE, WHICH ARE HEREBY EXPRESSLY DISCLAIMED. IN NO EVENT SHALL SELLER BE LIABLE FOR INCIDENTAL OR CONSEQUENTIAL DAMAGES. THE EXCLUSION OF INCIDENTAL AND CONSEQUENTIAL DAMAGES AS SET FORTH IN THIS WARRANTY STATEMENT SHALL BE DEEMED INDEPENDENT OF, AND SHALL SURVIVE, ANY FAILURE OF THE ESSENTIAL PURPOSE OF ANY LIMITED REMEDY UNDER THE TERMS OF THIS AGREEMENT. NO EXTENSION OR EXPANSION OF THIS WARRANTY SHALL BE BINDING UPON SELLER UNLESS SET FORTH IN WRITING AND SIGNED BY SELLER'S AUTHORIZED REPRESENTATIVE.

119 36-150[IAI]-2 Auxiliary Power Unit P/N

120 Overview The [IAI]-2 Auxiliary Power Unit (APU) is a single shaft, constant speed gas turbine engine that provides electrical and pneumatic power to the aircraft. The APU is comprised of three major sections: Power section (reference Figure 1) Gearbox assembly (reference Figure 2) Controls and accessories The power section compressor provides a source of compressed air for combustion and bleed air for general aircraft use. Air enters the compressor inlet, compressed in a centrifugal impeller, then discharged through a diffuser into the turbine plenum. The turbine section consists of: Turbine wheel assembly Turbine plenum Combustion chamber assembly The plenum serves as a receiver for combustion discharge air and as an enclosure for the combustion chamber. Compressed air is received by the turbine plenum and directed through the combustion chamber, where fuel is introduced and burned. The hot gases then flow into the turbine. The single-stage turbine consists of a radial fixed-area nozzle and a radial inflow turbine wheel that drives the compressor and gearbox. After passing through the turbine wheel, the gas discharges axially through a short diffusing section. The gearbox assembly houses the reduction gear train required for use in driving APU accessories and aircraft power takeoff (PTO) requirements. A mounting pad is provided to mount a customer-furnished accessory, such as a starter-generator. The gearbox also contains provisions for mounting an optional Honeywell-designed direct current (dc) starter motor. Additionally, the gearbox serves as an oil sump for the APU selfcontained lubrication system. Controls and accessories include those required for APU operation (i.e., electronic control unit, fuel system, lubrication system, ignition system, and optional electric starter). The APU is equipped with a fully automatic control system that properly sequences control of fuel and ignition during starting and operation. APU speed is regulated by the full-authority electronic control unit (ECU) that directs delivery of the correct amount of fuel regardless of ambient conditions and load requirements. APU overspeed protection is provided by the ECU, which will automatically terminate APU operation within safe limits (110 percent rotor speed). The purpose of the gearbox section is to house the reduction gear train needed to rotate the APU accessories. The gear train supplies rotation to the power section during startup. The gearbox has a high strength; thin wall aluminum housing that contains the reduction gear train and other internal components.

121 Additionally, the gearbox section: supplies the oil system for the APU and APU generator, is the oil sump for the APU self-contained oil system, oil jets are sized to give the required flow to limit the maximum oil temperature rise across highspeed bearings to 50 F (27.7 C), turns the APU generator at 12,000 RPM clockwise. The gearbox section has mounts for the following: starter/generator, magnetic drain plug, oil fill cap, rotary oil pump assembly/fuel control assembly, low oil pressure switch, high oil temperature sensor, motional pickup transducer, time totalizing meter (hourmeter). In addition, the APU has a start counter and an inlet temperature bulb (sensor) mounted on the compressor inlet duct. The electrical installation system supplies electrical power through the APU wiring harness to operate the APU units/components. It is also the path for the ECU to communicate with the electrical, sensing and operational components of the APU. The ECU is connected through aircraft wiring to the APU/aircraft interface connection on the left side of the APU enclosure. Power is supplied to the APU electrical system from the aircraft dc bus. The electrical installation system includes the APU wiring harness.

122 Figure 1: Power Section

123 Figure 2: Accessory Drive Gearbox Assembly

124 Engine Operation The APU is a gas turbine engine. The part of a gas turbine engine that produces power is the power section. The operation of the power section occurs in three phases: compression of ambient air, combustion of the compressed air after it is mixed with fuel, conversion of the thermal/kinetic energy of the burned fuel/air mixture into mechanical (rotary) energy (shaft energy). The power section's three subsections that work together to operate the gas generator are the: compression section, combustion section, turbine (conversion) section. Power Section The compressor rotor turns at high speed and pulls in a large quantity of ambient air through the compressor inlet duct and compressor inlet (protective cylinder with holes which permit airflow but prevents foreign object ingestion). The compressor rotor then compresses this air. The compressed air has a large quantity of oxygen, which causes a very hot flame during combustion. When the compressor rotor compresses the air, it also gives the air a high velocity. To prevent flameout and permit the air to correctly mix with fuel, the vanes of the compressor diffuser decrease the velocity of the air and increase its pressure before it goes into the combustion chamber. The positions of the remotely located Load Control Valve (LCV) and APU mounted Surge Control Valve (SCV) control the quantity of air that flows into the aircraft bleed system, and the Electronic Control Unit (ECU) controls the positions of the valves. If the two valves are closed, all airflow goes into the combustor. When either valve is open, some of the compressed air flows through either or both open valves. The remaining compressed air goes through the compressor deswirl and then into the combustion section. The deswirl is the bridge between the compression and combustion sections. The vanes of the deswirl cause airflow to become straight as it goes into the combustion section. This airflow is known as compressor discharge air. The compressor discharge air flows into the combustion chamber between the inside of the turbine housing and outside of combustion chamber. Approximately 30% of compressor discharge air mixes with fuel for combustion, and is known as combustion air. The combustion air comes into the combustion chamber through a row of orifices and mixes with fuel in a space known as the primary zone. The airflow in the primary zone has a circular flow pattern, which causes the spray of fuel to mix fully with combustion air. During APU startup, sparks from the igniter plug cause the fuel/air mixture to ignite and burn in the primary zone. After combustion, the hot combustion gas moves in the direction of the outer transition liner. Most of the compressor discharge air (that is not used as combustion air) that remains is known as secondary air. Secondary air comes into the combustion chamber (through larger orifices) downstream of the primary zone, in the space known as the dilution zone. The secondary air mixes with hot combustion gas in the dilution zone and causes smoother airflow. It also keeps the temperature in the combustion chamber at a safe

125 level and decreases the temperature of the liner walls. The liner turns the combustion gas to move it through the turbine nozzle. The turbine nozzle vanes increase the velocity of the combustion gas and give it the correct angle to hit the blades of the turbine rotor. This causes the turbine rotor to turn. The turbine rotor and compressor rotor are attached on a common shaft, thus the turbine rotor rotation, turns the compressor rotor which brings in more air. After the combustion gas flows through the blades of the turbine rotor, it flows out the exhaust duct and overboard. Accessory Drive Gearbox Reduction Gearing System The mechanically driven accessories, APU generator/adapter gearbox, fuel control unit, and starter motor, are connected to the power section through the gear reduction system. The reduction gears of the gearbox decreases the high speed, low torque power of the power section rotating group into the low speed, high torque power that is necessary to drive the accessories. Operation with Bleed Air Loads The engine can be bleed-loaded at speeds above 95% plus 94 seconds. Operating Time and Engine Starts An externally mounted APU hourmeter provides a record of cumulative APU operating time. An externally mounted APU start counter provides a record of cumulative APU starts. When necessary for the APU to supply bleed air to the aircraft, the ECU will send a signal to open the LCV. When part of the compressor air is taken to supply bleed air, the ECU must make allowances for the loss of that quantity of air (which is normally available for combustion and cooling as well as to help drive the turbine). To make allowance for the loss of pneumatic energy, much more fuel is necessary (as compared for shaft loads) to supply sufficient thermal energy to increase RPM and keep it at 100%. Bleed air loads cause a much more significant increase in exhaust gas temperature (EGT) than do shaft loads due to the reduced airflow through the turbine rotor and exhaust. The EGT Immersion Thermocouple (sensor) continuously provides exhaust gas temperature data to the ECU. When the ECU detects a rise in EGT toward unacceptable operational parameters, it signals the LCV to modulate toward closed. The result is that more airflow is directed through the power section, which reduces EGT and fuel flow.

126 APU Typical Functions The APU provides pneumatic power for ECS, and shaft power to drive a customer furnished starter/generator. The APU can be shaft and bleed loaded at 95% rpm plus four seconds. In the ECS mode, the APU supplies air to the air conditioning packs. Air conditioning is done through flight deck signals that open both APU LCV and pack flow valves. Bleed air to the aircraft systems is regulated by the APU pneumatic control system based on aircraft pneumatic demands. During bleed operation (ECS), the APU compares actual EGT with a predetermined temperature schedule within the electronic control box (ECB). When EGT exceeds the preset limit, the ECB automatically modulates the APU LCV to a more closed position to lower the load and keep EGT within acceptable levels. When bleed loading is completed, the APU returns to IDLE rpm in preparation for the next mode. During operation, the ECB monitors engine speed, temperature, oil pressure and overcurrent in its components. The APU shuts down if any limits are exceeded. Operating time is recorded by an hourmeter. The hourmeter starts to operate at 95% rpm. Pressing the APU STOP switch shuts down the APU. There is no shutdown cooldown period.

127 Figure 3: Typical APU Function The purpose of the APU is to provide the aircraft with (Reference Figure 3): DC generator output for the aircraft electrical system Pneumatic output for the ECS In normal operation, APU generator and pneumatic air (APU bleed) loading are requested from the flight deck to the APU ECU. The ECU automatically controls loading and unloading of the APU. The ECU utilizes and monitors several inputs to perform automatic control: Inlet air temperature (T 2 ) Engine speed Exhaust gas temperature (EGT) Oil pressure Oil temperature Utilizing these inputs, the ECU automatically controls: Engine speed Bleed flow EGT limits during bleed-load operation

128 The APU will automatically shutdown if a prescribed protective shutdown condition is present. To facilitate use of extracted pneumatic power, the APU bleed air valve (BAV) is connected between the APU and the aircraft s pneumatic system. It is signaled by the ECU to allow air to flow from the APU to the aircraft. The APU pneumatic control system regulates the APU pneumatic output power by sensing the APU exhaust temperature (EGT) and inlet temperature. When the EGT exceeds a preset limit, the ECU closes the BAV to a half open position, preventing an APU overtemperature condition. The ECU will continue to monitor EGT and automatically opens the BAV when EGT falls below a preset limit. When ECS operation is not required, the APU BAV is signaled to close and the APU returns to idle.

129 APU Starting (Power Management) The APU starts automatically after selecting the APU Master switch followed by pressing the APU Start switch. The ECU will control ignition and fuel automatically as required for ambient conditions. During the ECU pre-start Built-In-Test-Equipment (BITE), if a failure is detected that would critically effect mission success, the ECU inhibits starting of the APU until the failure is resolved. The failure is stored in the ECU. The APU speed sensor signal provides switch-points for automatic fuel and ignition initiation, starter relay dropout, arming, and ignition termination. At full rated speed, the ECU controls engine speed at 58,737 rpm ±1.0%. The ECU regulates the APU pneumatic output by sensing the APU EGT and comparing this to a predetermined schedule within the ECU. Bleed extraction will be controlled to prevent an overtemperature condition. Exhaust gas temperature and engine speed are continuously monitored by the ECU. The ECU will shut down the APU if engine speed exceeds 108% or EGT exceeds overtemperature scheduled limits. The ECU has the authority to shut down the APU when BITE indicates that continued APU operation might cause damage. The ECU also has the authority to inhibit starting of the APU when BITE indicates APU operation may cause damage. Upon request, the ECU will report all APU fault data over ARINC 429 to the multi-function display (MFD). This enables an analysis of APU fault data for troubleshooting. The ECU provides for automatic control and sequencing from start to 100% rpm. At 10% APU speed, the ECU powers the ignition unit, and the fuel solenoid valve, allowing fuel flow to the three primary fuel nozzles. A timed-acceleration-control feature schedules fuel during APU starts. At 10%, the ECU also powers the surge control valve. At 50% speed the generator control unit de-energizes the starter/generator. If the GCU system fails, the ECU will deenergize the starter contact relay automatically. At 95% speed the hourmeter is energized. At 95% speed plus 4 seconds, the ECU switches to on-speed operation. The following activities occur: The ready-to-load signal is activated The bleed air valve arms The generator is armed At 99% speed the ignition unit is de-energized At 100%, a closed-loop speed feedback circuit in the ECU assumes control and maintains power section rotor speed constant within ±1.0%. If the APU speed drops below 96% for any reason, the ignition unit will be re-energized, unless the APU is in the protective or normal shutdown modes. The APU may be loaded once it reaches on-speed operation. NOTE: It is recommended that the APU should not be loaded for at least 60 seconds after reaching on-speed operation.

130 APU Protective Shutdowns The ECU has the authority to shut down the APU when BITE indicates that continued APU operation might cause damage. Once a protective shutdown has been initiated, BITE will be inhibited from detecting any further shutdown or LRU faults during the APU roll down. The ECU has the authority to inhibit starting of the APU when BITE indicates APU operation may cause damage. Shutdown history information is also stored in the ECU NVM. During APU operation, protective shutdowns occur if any of the following conditions occur: Parameter Overspeed Low Oil Pressure Over temperature (High Exhaust Gas Temperature (EGT)) Loss of EGT detection High Oil Temperature (HOT) Loss of speed detection Electronic Control Unit (ECU) failure No light off during start Reverse flow Loss of DC Power Automatic Shutdown Features Specification 108 percent maximum (63,460 rpm) Less than 31 psig ( kpa) for more than 10 seconds above 95 percent governed speed 1325ºF (718ºC) for more than 10 seconds Open thermocouple unit 325ºF (163ºC) for more than 10 seconds Open motional pickup transducer circuit Internal failure of the ECU EGT does not increase to 400ºF (204ºC) in 17 seconds from percent speed Inlet temperature more than 275ºF (135ºC) for 5 seconds ECU primary input voltage is less than 10 vdc NOTE: The APU is considered Catagory 2 (non-essential), and all protective shutdowns are active in-flight or on the ground.

131 Leading Particulars Parameter Specification Weight (52.2 kg) (approximately) Dimensions Height 21.5 in (54.6 cm) Length 32.3 in (82.0 cm) Width 19.1 in (48.5 cm) Engine Ratings (Corrected to 113ºF (45ºC) standard sea level condition at a turbine discharge temperature of 1230ºF (665ºC) maximum Pneumatic Power Output Only Bleed-air Flow Bleed-air Pressure Bleed-air Temperature Combined Pneumatic and Shaft Power Output Shaft Power Bleed-air Flow Bleed-air Pressure Bleed-air Temperature Electrical System ECU P/N Lubricating System Fill Capacity 62.8 lb (28.5 kg)/minute minimum 46.7 psia (321 kpa) minimum 470ºF (243.3ºC) 22.0hp minimum 58.0 lb (26.3 kg)/minute minimum 48.6 psia ( kpa) minimum 471ºF (243.9ºC) 16 to 36 vdc 2.0 US quarts approx (1900 cm 3 ) Parameter Fuel Inlet Pressure Normal Minimum Fuel Specification Maximum Fuel System Specification 20 to 40 psig ( to kpag) 5 psig (34.47kPag), above the true vapor pressure of the fuel being used 60 psig ( kpag) MIL-DTD-5624, Grades JP-4 and JP-5 ASTM D1655, Grade Jet A

132 Operating Limits Observation Condition Limit Requirements CAUTION: Shutdown if indicated values are more than or continue at these limits. Pressure Oil Governed Speed 45± 10 psig (310 ± kpa) Speed Steady-state Rotor Full-load governed speed (nominal) (100 percent speed operation). Full-load governed speed (nominal) (100 percent speed operation). ± 2 psig (±13.7 kpa max fluctuation) 58,737 rpm (100 percent) 58,150 to 59,324 rpm ( percent) Temperature Inlet Air Oil Allowable variation at steady state operation ± 588 rpm (± 1.0 percent) 57ºC (135ºF) maximum 163ºC (325ºF) maximum

133 Cabin Pressure Control Systems Since aircraft pressurization was introduced in 1941, Honeywell cabin pressure control systems, built on wellrespected names such as Garrett and AiResearch, have become a leader in the aerospace industry. Thousands of aircraft worldwide, logging millions of hours each year, operate comfortably and safely with Honeywell systems. Through the use of modular design, Honeywell offers an array of all-electric and electro-pneumatic configurations that are customized to meet your cabin pressure needs. The Honeywell team is dedicated to creating innovative solutions that deliver exceptional passenger comfort and safety.

134 Innovative solutions for passenger safety and comfort Thrust Recovery System: An all-electric out-flow valve cabin pressure system, the Thrust Recovery System maximizes aircraft range and minimizes fuel penalty by directing overboard air in the aft direction to recover thrust. Dual and Single Auto Channel Smart Valve System: Fully electric out-flow valve, the Smart Valve system leads the next generation of cabin pressure controls, with a design for use with integrated avionic systems that combines control and monitoring functions into a compact package. Honeywell can work with you to meet your cabin pressure needs by offering: Full-line of product solutions Custom design capability Extensive system and component test facilities Advanced analytical capabilities Full support service facilities Validated material technology and process capability Integration Monitor and warning functions Data bus interface Consolidated valve and electronics Minimum weight Dispatch Reliability Proven reliability Redundancy management Flow Distribution Enhanced passenger comfort Optimum air flow Thrust Recovery Skin mounted Custom contour Honeywell customers include: Aero Commander Aero Vodochody Avro/BAe Boeing Bombardier Cessna Dassault DeHavilland EADS CASA EADS Socata Fairchild Fokker Gulfstream IAI IPTN Lockheed Martin Northrop/Grumman Piaggio Pilatus Raytheon Rockwell SAAB Electro-Pneumatic System: A long time tradition at Honeywell and in the aerospace industry, the Electro- Pneumatic system has led the industry by providing customers with high quality pneumatic solutions. Engines, Systems & Services Engines, Systems & Accessories Honeywell International Inc N. Oracle Road Tucson, AZ Tel: N May Honeywell International Inc.

135 G280 CABIN PRESSURE CONTROL SYSTEM Overview The Cabin Pressure Control System (CPCS) is a fully automatic system that provides the following aircraft functions: Cabin pressure rate control Cabin altitude limiting Cabin-to-ambient differential pressure control The CPCS is comprised of three Line-Replaceable Units (LRUs) certified as part of the airplane type certificate: Controller Outflow Valve Safety Valve The controller consists of a single package with two independent channels a control channel and a backup monitor channel. The outflow valve utilizes a dual-channel actuator with dissimilar motors to control the amount of air exiting the cabin. One channel of the actuator utilizes a brushless DC motor and is driven by commands from the control channel of the controller. The other channel of the actuator utilizes a brush DC motor and is utilized for manual and altitude-limit operation. The safety valve is independent of the outflow valve and controller. Its purpose is to relieve excess positive pressure in the event of a failure condition. The CPCS requires DC electrical power to operate, and a source of cabin air inflow to pressurize the cabin. Cabin air inflow is provided by one of the following mechanisms, depending on the airplane mode of operation: APU bleed air ground operation Main engine bleed air normal flight Ram air negative pressure relief The controller automatically controls the cabin pressure to a predetermined schedule to ensure optimum passenger comfort. Selected operational parameters are monitored and if limits are exceeded, the controller will automatically switch to manual mode, where the crew may manually adjust the cabin pressure.

136 Operating Specifications The physical and operational characteristics of the CPCS are listed below. Aircraft Parameters - approximately: Ceiling: Pressurized Volume (net): ECS Airflow: Temperature Range: ft 1200 cu ft 25 lb/min (normal) Cabin -15 to +70ºC Ambient -55 to +70ºC CPCS Parameters - approximately: Cabin Altitude at Aircraft Ceiling: 7024 ft Cabin Climb Rate (automatic mode): 500 slfpm Cabin Descent Rate (automatic mode): 300 slfpm Landing Altitude Accuracy: ±200 ft Cabin Altitude Limiting (electronic): ±400 ft Oxygen Mask Drop Limits: High-Cabin Altitude ft Non-High Cabin Altitude ft Differential Pressure Limits: Ground Mode Positive (electronic) (electronic) 0.75 psid Positive (pneumatic) psid maximum ±0.043 psid Negative 9.45 ±0.10 psid

137 Physical Description G280 CPCS Outflow Valve G280 CPCS Controller G280 CPCS Safety Valve

138 CPCS Functions The schematic below describes the relationship between the CPCS LRUs and the aircraft interface: In normal ground operation, the outflow valve is maintained in the full-open position to minimize the differential pressure between cabin and ambient. When the main engine throttles are advanced, the CPCS begins to pre-pressurize the cabin in anticipation of takeoff. By increasing the pressure in the cabin prior to rotation, pressure transients are minimized during rotation. During aircraft climb, cabin pressure is controlled to an internal climb schedule computed to minimize the cabin rate-of-change. During climb, the cabin rate of change is limited to 500 sea-level feet per minute for passenger comfort. If necessary to limit differential pressure, the cabin rate of change is automatically increased to prevent an overpressure condition. During aircraft cruise, cabin pressure is maintained at the scheduled pressure. As the aircraft begins to descent, the system switches to either a descent schedule or the selected landing altitude and begins controlling the cabin pressure to this schedule. Finally, when the aircraft lands, the outflow valve is driven open to completely depressurize the cabin.

139 Cabin Pressure Controller The primary purpose of the cabin pressure controller (CPC) is to automatically control aircraft pressurization. To do this, the CPC transmits open and close speed commands to the outflow valve (OFV) to regulate the amount of airflow out of the aircraft. The amount of airflow is regulated so that the actual cabin pressure matches the software pressurization schedule in the CPC for each phase of aircraft operation. Other purposes of the CPC include these: - Allow manual control of the OFV and cabin pressure by the flightcrew - Self-test of the system - Fault annunciation for the flightcrew - System status to the EICAS. In order to sense the mode of operation (automatic or manual) and to control pressurization, the CPC receives discrete, digital, and continuous signals from switches, sensors, and the OFV. The CPC includes a monitor channel which monitors the operation of the automatic channel. If the automatic channel fails, the monitor channel allows the flightcrew to operate the CPCS in the manual mode. In the manual mode, the monitor channel supplies feedback to the flightcrew about the manual mode inputs. The CPC includes two pressure ports to sense the cabin pressure. One port is used by the automatic channel and the other port is used by the monitor channel. Outflow Valve The purpose of the outflow valve (OFV) is to control the rate of airflow out of the aircraft cabin. The OFV is usually controlled automatically by the CPC, but can be controlled manually by the flightcrew with switches in the cockpit. The 0FV includes the primary components as follows: - Electromechanical actuator - Two DC motors - Feedback potentiometer - Limit switches - Tubular outflow duct with butterfly plate - Connectors J1 and J2. The electromechanical actuator contains the electrical and electronic circuitry that receives the position commands from the CPC or from switches in the cockpit. The circuitry also supplies actuator position (automatic mode) and status back to the CPC. The actuator includes the necessary gears to move the butterfly plate shaft.

140 Two DC motors are included in the OFV to move the butterfly plate. One motor is used in the automatic mode and the other motor is used when the CPCS is in the manual mode. The motors operate independently and only one motor is operated at a time. A feedback potentiometer is used to transmit the position of the butterfly plate back to the CPC. This feedback signal from the OFV to the CPC is used for BIT testing. Limit switches are used in the OFV to stop the electromechanical actuator when the butterfly plate reaches the limits of travel. The tubular outflow duct and variable-position butterfly plate supply the actual path for airflow discharge from the aircraft. The butterfly plate is attached to a shaft which is moved by the electromechanical actuator. Pressure Relief Valve The pressure relief valve (PRV) is used to prevent over-pressurization of the aircraft that can occur because of an increase in cabin pressure or a decrease in atmospheric pressure. The PRV is a pneumatically-operated poppet-type control valve that is used to give positive pressure relief. It is a passive, non-electronic valve that has no interface or physical connection with the other CPCS components. When the cabin pressure is in limits, the PRV monitors the cabin pressure, but does not operate. It is only used to give pressure relief when the cabin pressure is greater than the CPCS electronic differential pressure limits. The metering section of the PRV includes a port to cabin pressure, a port to atmospheric pressure, and a metering valve. The metering valve has a diaphragm assembly and a spring-loaded, adjustable metering pin. The metering section monitors the difference between cabin pressure and atmospheric pressure and, if the difference reaches the pneumatic ΔP limit, the metering valve will open. The open metering valve will cause a change in pressure inside the control chamber, which will open the main valve poppet. The main valve poppet is used to let cabin air flow out from the cabin and give positive pressure relief.

141 G280 ENVIRONMENTAL CONTROL SYSTEM COMPONENTS Overview The G280 Environmental Control System (ECS) receives high temperature bleed air from the two main engines or the Auxiliary Power Unit (APU) to provide conditioned air to the cockpit and cabin for pressurization, heating and cooling. The ECS creates a supply of cool, de-humidified air to maintain selected temperatures and ventilation rates within the cockpit zone and cabin zone. The conditioned air also provides aircraft pressurization and cooling air for the avionics. The ECS introduces cabin air inflow into the cabin while the Cabin Pressure Control System (CPCS) controls the amount of air that is exhausted from the cabin. The ECS is comprised of the Line-Replaceable Units (LRUs) listed in the table below. The LRUs are certified as part of the airplane type certificate. Items denoted CFE (Customer Furnished Equipment) are not supplied by Honeywell but are necessary elements of the overall ECS. The ECS components may be categorized into three functional groupings- bleed air control; wing anti-ice control; and air conditioning and distribution. Bleed Air Control LIST OF ECS LINE REPLACEABLE UNITS (LRUs) Item No. Part Number Component High Stage Valve LP Valve, Check Manifold Pressure Regulating and Shutoff Valve Sensor, Precooler Inlet Temp Precooler, Left Hand Precooler, Right Hand Valve, Fan Air Sensor, Manifold Pressure Sensor, Precooler Outlet Temp Valve, Check, APU & Ground Connection Service Pressure Regulator Air Management System Controller Valve, Manifold Isolation Wing Anti-Ice Control Valve, Wing Anti-Ice Sensor, Wing Anti-Ice Temp Switch, Wing Anti-Ice Overtemp Switch, Wing Anti-Ice Undertemp/ Overtemp

142 Air Conditioning and Distribution LIST OF ECS LINE REPLACEABLE UNITS (LRUs) (Cont d) Environmental Control Unit 3-1A Heat Exchanger, Primary 3-1A Heat Exchanger, Secondary 3-1B Valve, Check 3-1C Air Cycle Machine 3-1D Sensor, Compressor Outlet Temp 3-1E Reheater/ Condenser 3-1F Water Extractor 3-1G Valve, Turbine Inlet Temp Control 3-1H Valve, Low Limit Temp Control Duct Temperature Limiter Nozzle, Water Spray Venturi Sensor, Delta P Sensor, Pack Inlet Temp Sensor, Temperature (35 o F) Sensor, Zone/Duct Temp Temperature Selector Temperature Sensor Fan Valve, Check, Cabin Air Valve, Check, Emergency Air Valve, Check, Emergency Ram Air Valve, Check, Flight Deck Air Valve, Check, Gasper Valve, Check, Pack Supply Valve, Pack Inlet Valve, Trim Air 3-19 CFE Valve, Cockpit Defog 3-20 CFE Valve, Emergency Air Shutoff 3-21 CFE Converter, Ozone 3-22 CFE Heat Exchanger, Emergency Air 3-23 CFE Manual/ Auto Switches The bleed-air control subsystem of the ECS controls the pressure and temperature of air bled from the engine or APU before it is introduced into the wing anti-ice control subsystem and the air conditioning and distribution subsystem. The wing anti-ice control subsystem takes bleed air and modulates the flow of bleed air to the left and right wing anti-ice ducting. The air conditioning and distribution subsystem controls the temperature of the flight deck and cabin environments.

143 Environmental Control Unit (ECU) The heart of the ECS is the Environmental Control Unit (ECU), commonly referred to as the refrigeration pack. The ECU includes a three wheel air cycle machine (ACM), a high pressure water extractor, primary and secondary heat exchangers, a reheater/condenser heat exchanger, a low limit valve, a turbine inlet temperature control valve, a compressor bypass check valve and a compressor outlet temperature sensor. ECU Operation G280 Environmental Control Unit Cooling is done by two methods; heat transfer within the primary and secondary heat exchangers, and compression with rapid expansion through the ACM. During ECS operation, regulated bleed air enters the ECU where it passes through the bleed air inlet of the primary heat exchanger (see ECU schematic on following page). Induced air or ram air is ducted through the ram air inlet of the heat exchanger, cooling the bleed air. The cooled bleed air then enters the compressor section of the ACM, where the air is compressed to approximately 1.5 times the inlet pressure. If the compressor discharge pressure is less than the inlet pressure, the air will bypass the compressor section through the compressor bypass check valve and go directly into the secondary heat exchanger. The temperature of the air flowing into the inlet of the secondary heat exchanger is sensed by the compressor outlet temperature sensor and a signal is sent to the air management system controller. Some of the compressor discharge air will be bypassed into the turbine inlet by the turbine inlet temperature control valve to hold turbine inlet temperature above a preset level. Most of the compressor discharge air is ducted through the secondary heat exchanger where additional heat is removed by induced air or ram air. The induced air or ram air is then ducted overboard through the fan air plenum and fan plenum check valve. The induced airflow is supplied by the fan on the ACM during ground operation. In the flight mode, most of the ram air bypasses the fan through the fan plenum check valve.

144 G280 Environmental Control Unit Schematic The cooled compressed air exiting the secondary heat exchanger then enters the reheater portion of the reheater/condenser where it is cooled by air flowing out of the water extractor. The air then flows through the condenser portion where it is cooled further by turbine discharge air. The cold air then flows into the water extractor where entrained moisture is centrifugally removed. Air pressure forces the condensed moisture out of the water extractor, through a drain strainer and out of the pack. The air then passes through the reheater again, gaining temperature to vaporize any remaining moisture. The air then flows into the turbine section of the ACM where it is permitted to expand, decreasing its temperature. As the air moves across the turbine wheel, it generates power to drive the compressor and fan wheels of the ACM, which share a common shaft. The energy removed by forcing the turbine airflow to do work causes a substantial decrease in temperature, and can result in turbine discharge air temperatures well below freezing. The low limit valve adds some hot bleed air to the cold turbine discharge air to prevent ice formation in the condenser. The mixed air flows through the condenser portion of the reheater/condenser again. The conditioned air exiting the condenser is then mixed with warm air to achieve the desired cockpit and cabin temperature.

145 Air and Thermal Systems Efficient and cost-effective integrated air management and control solutions

146 Proven to deliver highly reliable and efficient operation with lower total costs of ownership for aircraft operators. Cost-effectively optimizing pas Honeywell designs and manufactures a broad range of integrated Air and Thermal System (A&TS) that provide efficient cabin air conditioning and temperature control, aircraft pressure control, and fuel tank inerting for commercial aircraft. Featuring advanced functionality for optimal system performance, our electric and pneumatic systems improve passenger comfort and safety while minimizing operator cost of ownership. Cabin Air Management Systems Our lightweight and highly efficient air and thermal management solutions monitor and control cabin temperature and air flow in the cockpit, passenger, and cargo areas and provide cooling for avionics. They also manage the aircraft s engine bleed air and provide ice protection for flight control surfaces. Air Source Systems engine bleed and non-bleed architectures that precondition air temperature, pressure and quality coming into the aircraft s air conditioning system. Air Conditioning Systems air and vapor cycle solutions that control cabin temperature, remove humidity, and optimize fresh and recirculated air flow rates for an improved cabin environment. Anti-Ice Systems prevents ice build-up on engine cowl and flight control surfaces for improved flight safety. Cabin Pressure Control Systems As a pioneer in cabin pressure control system development, Honeywell leads the industry in highly reliable solutions that monitor and maintain aircraft cabin pressure to required levels for enhanced passenger comfort and safety while providing lower aircraft operating costs. Thrust Recovery System maximizes aircraft range and minimizes fuel penalty by using an all-electric out-flow valve to direct overboard air in the aft direction to recover thrust. Dual and Single Auto Channel Smart Valve System advanced design for use with integrated avionic systems that combines control and monitoring functions into a compact, fully electric out-flow valve package. Electro-Pneumatic System high quality, and reliable pneumatic valve solution for controlling aircraft cabin pressure. Air Conditioning Pack Flow Control Valve

147 senger comfort and safety Gas Processing Systems Our integrated on-board solutions improve flight safety through highly reliable and efficient gas processing technologies. On-Board Inert Gas Generating Systems (OBIGGS) FAA approved system that improves aircraft safety by reducing the risk of fuel tank explosions. Extended Mechanical Systems Perimeters Honeywell provides integrated, multi-ata chapter solutions that include these Air and Thermal Systems along with Auxiliary Power Systems and Primary and Secondary Electric Power Systems. These extended perimeter solutions create additional aircraft-level value through increased system performance and reduced weight. Airframe Components From fans and controllers to power units and heat exchangers, Honeywell delivers a complete range of A&TS components that increase the functionality of integrated systems, reduce weight, and improve overall system performance for safer, more efficient and reliable aircraft operation. Fans and Blowers Compressors and Pumps Air Cycle Machines Heat Exchangers and Water Separators High Power Motors and Controllers Ozone Converters and Hydrocarbon Burners Actuators Airframe Valves Pressure, Temperature and Flow Sensors Key Benefits Proven A&TS design and development capability Innovative technologies increase system efficiency and performance Solutions designed to reduce operating costs and improve reliability Comprehensive offering of integrated and federated systems in electric and electro-pneumatic configurations Leading developer and integrator of More Electric Aircraft A&TS architectures Global repair service, logistics and customer support network OBIGGS Thermal Control Unit Heat Exchanger

148 Honeywell Aerospace Honeywell is a leading global provider of integrated avionics, engines, wheels and brakes systems and service solutions for aircraft manufacturers, airlines, business and general aviation, military, space and airport operations. For more information on Honeywell Aerospace, visit us online at Global Network of Support Services Honeywell s resources span the Americas, Europe, Middle East, Africa, Asia and the South Pacific to deliver dedicated 24/7 service support. As a world leader in aviation aftermarket services, our global repair centers, logistics network and field services engineering teams are able to quickly repair, supply, and warranty equipment whenever and wherever it is needed. Honeywell Aerospace Honeywell 1944 East Sky Harbor Circle Phoenix, Arizona North America: International: C November Honeywell International Inc.

149 G280 Lighting Shipset A comprehensive exterior lighting solution for the G280.

150 Marquee technology for a marquee jet The Best of Both Worlds Gulfstream has long been one of the premier names in business aviation, as Honeywell has for aircraft lights. Befitting that of Gulfstream s newest airplane the G280 Honeywell has provided a full exterior lighting suite, leveraging our full expertise in BGA lighting technology. Astreon : Solid-State Position Lighting Utilizing solid-state lighting technology, Honeywell s Astreon position lights are changing the game in business aviation. While traditional light sources provide business jet operators with about 300 hours of operation before maintenance is needed, Astreon products have an estimated FAR-compliant life of 3,000 hours with an estimated total life of 20,000 hours. Astreon LED lighting is designed to deliver outstanding reliability and provide lower total cost of ownership by reducing replacements and decreasing downtime associated with replacing and re-potting incandescent or halogen lighting and lenses. Product Overview n Wingtips, Navigation, and Strobe Lights - Recognition Light ( ) - Left Hand Forward Position Light ( ) - Right Hand Forward Position Light ( ) - Left Hand Wing Anti-Collision Light ( ) - Left Hand White Tail Light Lens ( ) - Right Hand Wing Anti-Collision Light ( ) - Right Hand White Tail Light Lens ( ) - Power Supply ( ) - Aft Position Light & Anti-Collision Light ( ) n Landing, Taxi, and Flood Lights - Left Hand Ice Inspection Light ( ) - Right Hand Ice Inspection Light ( ) - Left Hand Logo ( ) - Right Hand Logo ( ) - Taxi Light (B4150B ) - Landing Light (B5325A-4-24) n Emergency and Utility Lights - Baggage Light ( ) - Left Hand Door Emergency Exit ( & ) - Right Hand Over Wing Emergency Exit ( & ) - Right Hand Ground Emergency Exit ( & ) - Refuel Door (A-6850C7) Honeywell Aerospace Honeywell 1944 E. Sky Harbor Circle Phoenix, AZ Domestic International A December Honeywell International Inc.

151 Laseref VI Micro Inertial Reference System Reduce operating costs with RNP precision guidance

152 Laserf VI:Layout 1 3/16/2009 9:02 AM Page 2 Laseref VI Simplify crew workload and reduce maintenance and operational costs Honeywell s Laseref VI micro inertial reference system (IRS) has been designed to simplify pilot workload while dramatically reducing installation time, weight, size, power, and cost. This revolutionary design is based on flawless service from more than 50,000 commercial inertial reference systems in service around the world and is compliant with new ADS-B requirements. Altitude 0.1 degree Heading 0.4 degree Position (inertial) 2 NMPH Position (hybrid) 12 Meters Hybrid position coasting performance > NM Velocity (inertial) 8 knots Velocity (hybrid) 0.25 knots Software certification DO-178B Level A Hardware certification DO- 160E Technical standard order (TSO) C4c, C5e, C6d, C129a Reduces operational costs through a 50% reduction in box size and over a 30% reduction in both weight and power consumption compared to similar systems In-service reliability >50,000 MTBF Interfaces ARINC-429 I/O Mounting tray 0.5 lbs Reduces installation costs and increases accuracy with electronic mounting tray alignment Size 6.5 x 6.4 x 6.4 Weight 9.1 lbs Reduces pilot workload through automatic mode control logic and automatic initialization Power (typical) 20 watts Cooling Passive Accelerometer sensor technology Quartz Gyro sensor technology Digital ring laser Benefits I I I I Eliminates delays with automatic IRS alignment I Reduces crew workload with in-motion inertial alignment and automatic realignment between flights made possible through GPS integration I CHARACTERISTICS Reduces weight and operating costs by implementing passive cooling technology Find Out More For more information on Honeywell s Laseref VI micro inertial reference system, visit Accuracy two sigma or 95% HIGH Integrity Applications To provide 100% availability of RNP 0.1 navigation performance and immunity to GPS outages, an optional Honeywell Inertial GPS Hybrid (HIGH) upgrade is available. HIGH combines raw measurement from each satellite in view from the MMR with a Kalman filter to provide a highly calibrated solution ensuring operators of their exact position. This capability is available for retrofit and forward-fit applications to maximize airline and route efficiencies. I ARJ-21 I Boeing 787 I Bombardier (CL-605, CRJ, C-Series) I Dassault (F7X, F50EX, F900EX, I Embraer (170, 175, 190, 195) I Gulfstream (100, 150, 200, 250, 350, F2000EX) 450, 500, 500, 650, CAEW) I Pilatus Trainers (PC7, 9, 21) I Raytheon (Hawker 4000, Trainers) I Sukhoi SSJ-100 I Hundreds of retrofit installations Honeywell Aerospace 1944 E Sky Harbor Circle Phoenix, AZ Domestic: International: A March Honeywell International Inc. Back Home Back Home

153 Web Flight Planning ACCURATE FLIGHT PLANS. DESIGNED FOR CORPORATE AVIATION. Online Flight Planning and Support Services for Business Aviation

154 Web Flight Planning The Honeywell Global Data Center (GDC) presents the next generation of online flight support services with our advanced Web Flight Planning system. Featuring user-friendly point-and-click menus combined with robust routing capabilities, GDC s Web Flight Planning system enables business aircraft operators to create and file flight plans from any personal computer connected to the internet. Simplifying Pilot Workload Our intuitive Web Flight Planning system is configurable with operator preferences, meaning that pilots only need to enter information that is unique to a particular flight. Flight plans are based upon current wind and temperature information and use aircraft performance data provided by the aircraft s manufacturer. Among other innovative features, pilots may optimize flight plans for best fuel efficiency or shortest flight time and upto-date weather reports for departure, destination or alternate airports can be Find out more For further information on how Web Flight Planning can enhance your flight operations, contact our Service Support team at (888) or us at gfo@mygdc.com. Additional information is also available online at quickly obtained while flight planning without changing pages. Oceanic contingency planning has never been easier. Our new system uses the most current wind information to automatically calculate drift-down performance and Equal Time Points between diversionary airports, simplifying decision making in the event of a loss of cabin pressurization or an engine-out emergency while flying in oceanic areas. The system calculates optimum performance recommendations for such events based on accurate performance data provided by the aircraft manufacturer. Expanded Functionality Honeywell s advanced web-based system provides accurate routing, precise performance calculations, and increased flexibility with features designed specifically for corporate aircraft operators. These value-added features include expanded drift-down reports, multiple wind models (including historical winds), precise aircraft performance data, and updated route selections such as National Route Program (NRP) routes, Pacific Tracks, Polar Tracks, and time saving FAA Coded Departure Routes (CDR). Comprehensive Solution The new Web Flight Planning system will enable business aircraft to operate more efficiently while saving time and money. Easy, secure access is provided via the internet and GDC s cost-effective subscription plans provide access to a variety of other value-added flight support features designed especially for business aviation. These services include textual and graphic-based weather products, passenger weather briefings, and worldwide flight following. No matter your flight support needs, Honeywell s GDC delivers innovative and real-time solutions to help your flight crews make the right decisions on the ground and during flight. Why Honeywell? Over 20 years of corporate aviation flight planning experience Industry leader in flight support services Experienced staff available 24-hours per day Cost-effective subscription plans Fleet discounts available Worldwide VHF and satellite datalink communications Web Flight Planning Advantages Powerful and flexible online flight planning system Quickly generate and file flight plans for destinations worldwide Intuitive point-and-click menus Advanced route selection tools OEM aircraft performance data Honeywell Aerospace NE 36th Street Redmond, WA Toll Free: International: A Feburary Honeywell International Inc.

155 Flight Sentinel SAVE TIME AND REDUCE DELAYS Always by your side

156 Your extra teammate - looking ahead to avoid problems and delays With busy schedules to keep, executives expect to arrive safely, refreshed, and on-time every time! Flight Sentinel s personalized flight planning and dispatch service is specifically designed to expedite your flight planning, increase situational awareness while enroute, and eliminate delays. Your Global Flight Sentinel service has once again proven to be invaluable to us. On a high priority charter flight from Southern California to the East Coast, where a winter storm had slowed or stopped most traffic, your service got us off the ground on time and saved us an hour of ATC Delays on departure. Our passengers had been concerned about the weather and your continual updates on enroute conditions and destination weather and expected delays gave them a great deal of comfort. The information on expected holding at the destination was spot-on and made a very favorable impression on the passengers. For More Information: visit us online at or Honeywell Aerospace Honeywell Flight Support Services NE 36 Street Redmond, WA North America Toll Free: Outside North America: Your Virtual Cockpit Member Starting the night before your flight, our staff checks and double checks NOTAMs, TMU advisories, weather, Digital ATIS, airport arrival quotas, ground delay programs, play book and coded departure routes, and much more. On the day of departure Flight Sentinel manages your flight plan filing to ensure an on-time departure, and if an Airspace Flow Program is in effect for your flight, we ll call you with your EDCT (estimated departure clearance time). A October Honeywell International Inc. Your IN-COCKPIT TEAM MEMBER Flight Sentinel includes Contract Pilot Services to provide complete team member support. 1 Contracted Pilot Trip per Year (max 5 days); all travel expenses are covered by Honeywell.* ATP-rated pilots that are left/right seat current & qualified Current 1st class medical certifi cates PRNAV & International Ops Certifi ed * Additional trips are provided to subscribers at 10% discount. Daily Contract Pilot Rates Available for: Gulfstream G-V Gulfstream 350/450/550 Bombardier Global Express/XRS/5000 Cessna Sovereign Citation X Citation XLS Hawker 4000 Pilatus PC-12 NG Embraer Lineage Embraer Legacy Dassault Falcon 2000EX EASy

157 Pre-Arranged Fuel LOWER FUEL COSTS AT THE READY Worldwide Fuel Service

158 Put your trust in the world s largest jet fuel re-seller locations worldwide With Honeywell s solution, you are assured the highest quality fuel and best service in the industry. Through our arrangement with the world s largest jet fuel re-seller, Honeywell s fuel desk can offer you the peace of mind knowing that your fuel will be waiting for you at over 1500 locations worldwide. Instant Credit Approval Is Available for GDC Subscribers As a further convenience, credit services are available with a simple application process. Why wait? Global Data Center (GDC) is ready to serve you globally, 24 hours, 365 days a year. ARRANGING FUEL HAS NEVER BEEN EASIER! It s as simple as 1, 2, Visit us online at or dial or ( outside US and Canada) Check latest fuel prices and or der online. Your fuel will be waiting for you at the pre-arranged price! Fuel where you need it, when you need it. Whatever your fuel needs may be across the globe, GDC can help you lower your fuel costs and fly more efficiency. For a no-risk fuel quote or to sign-up today, please contact Alastair Brownlee , or fuel@mygdc.com For More Information: visit us online at or Honeywell Aerospace 1944 E. Sky Harbor Circle Phoenix, AZ Domestic: International: A October Honeywell International Inc.

159 Flight Support Services YOUR PARTNER FOR FLIGHT OPERATIONS SERVICES Flight Operations Support Solutions to meet your Needs Today and Tomorrow

160 Honeywell Global Data Center (GD Honeywell is at your service with solutions designed for your specific needs. Flight Deck Datalink Communications (VHF, Inmarsat, Iridium) l Graphical Weather l Flight Sentinel l GDC - Flight Support Services l Pre-Flight & In-Flight: Worldwide Flight Planning, Text and Graphical Weather, Runway Performance Data, RAIM Prediction l Flight Following Solutions Designed For Your Specific Needs Honeywell s Global Data Center provides solutions that increase productivity and improve efficiency. With aviation experts and 24x7 availability, our services help maximize efficiency and minimize delays, so we can help get you to your destination safely. Charter and Fractional Solutions: Services that expand operational control to increase trip bookings and reduce delays, maximizing aircraft availability while keeping your clients happy and your fleet productive. Corporate Operator Solutions: Proactive services designed to help you avoid delays and maximize productivity for passengers and pilots avoiding hours of delays, no matter where in the world you travel. Owner/Operator Solutions: Best In Class Tools with integrated services, notifications and rich user interfaces. A natural, work flow process allows you to access relevant information to decrease flight planning and preparation time. Honeywell s Global Data Center (GDC) For 25 years Honeywell s Global Data Center (GDC) has provided flight support services to corporate, fractional, charter, private, government and military aircraft worldwide. Our services include 24-hour telephone support from experienced aviation professionals and access to the web application at The GDC staffs FAA-licensed flight dispatchers (Part 121 and Part 135), airline transport pilots, instructor pilots, and military pilots to provide flight support services as an extension of your flight department 24 hours a day, 7 days a week. Our expert flight data specialists utilize tools and flight operations know-how to provide a wide range of support services such as: Flight Support Services Flight Sentinel Flight Deck Communications Graphical Weather Customers can access Global Data Center Services by telephone, mobile device or datalink communications from the cockpit. The Global Data Center works the way you do. Using a simplified workflow approach that is continuously enhanced with features and improved with customer feedback. Flight Planning Services World Wide Flight Planning and Filing Flight plan delivery via facsimile or Multiple route options including: Wind optimized, ATC Preferred, Pilot defined, North Atlantic (NAT) Track routes and other ATC oceanic routes Advanced Passenger Information System (APIS) Receiver Autonomous Integrity Monitoring (RAIM) prediction Runway analysis Pre-arranged fuel Storage of flight plans from third party vendors

161 C). Services for your Operation. Air Traffic Services Digital Automatic Terminal Information Service (D-ATIS) reports Terminal Weather Information for Pilots (TWIP) Standard and special event airport reservations Pre-Departure Clearances Oceanic Clearances East and West bound oceanic clearances Weather Services Text weather including METAR, TAF, PIREP, SIGMET and NOTAM Area forecasts and route weather Passenger weather briefings Winds and temperatures aloft Uplink Graphical weather Graphical Weather Services (Web) Over 800 aviation weather charts Aviation hazards, hurricane tracking and significant weather products National and regional radar summary Winds and temperatures aloft Worldwide satellite imagery Flight Support Services A leader in datalink communications for over 25 years, Honeywell s Global Data Center (GDC) is your 24-hour source for dependable flight deck communication services. Crews stay in contact with two way datalink messaging. Linked to the outside world, the GDC system provides the sophistication and flexibility that enables you to communicate with your home base, Fixed Based Operators (FBO), Customs and Immigration, , fax machines, other aircraft, mobile handhelds and much more. All of your mission-critical air-ground, ground-air communications receive priority handling from the GDC, and our staff is available 24 hours per day to assist your aircraft with message delivery anywhere in the world. Providing unsurpassed dependability, each of the GDC s redundant communications systems are engineered for high reliability. When it counts, you can rely on the GDC to deliver. Datalink (ACARS) Communications Service to all datalink avionics Worldwide VHF Inmarsat Iridium Datalink service solutions Air traffic services Air-Ground, Ground-Air and Air-Air Message Delivery Flight plan uplink Graphical weather Message forwarding to telephone, pagers, , facsimile, and ACARS/AFTN addresses Text weather Graphical Weather Honeywell provides datalink graphical weather information through its WINN (Weather Information Network) for Honeywell Plane View cockpits, electronic flight bags and Proline 21 equipped cockpits. WINN Graphical Weather Service Features Features Datalink, VHF and Satellite XM Satellite Graphically displays NEXRAD, winds aloft and satellite cloud height, Clear Air Turbulence, Convective Weather, Lightning Benefits Enhanced safety and situational awareness User interface designed for quick, easy access 24/7 Honeywell customer service and support Real time graphical weather solution at a cost effective price

162 Flight Sentinel With busy schedules to keep, executives expect to arrive safely, and on-time every time. Flight Sentinel s personalized flight planning and dispatch service is specifically designed to expedite your flight planning, increase situational awareness while enroute, and eliminate delays. Utilizing the Collaborative Decision Making* (CDM) tools, Honeywell provides proactive flight coordination with air traffic control and crews. Collaborative Decision Making (CDM) is a joint government/industry initiative aimed at improving air traffic management through increased information exchange among the various parties in the aviation community. For more information: visit us online at or The GDC is uniquely qualified and equipped to deliver our Flight Sentinel Service, a proactive service designed to minimize or eliminate delays. GDC Flight Sentinel Specialists can route your flight plans in pre-flight and in-flight using the FAA s CDM tool* to proactively watch for (and help you avoid) delays due to traffic, weather, ATC hazards, etc. Our team, who are members of FAA s Collaborative Decision Making program, communicate directly with the FAA National Air Traffic Control Command Center, regional centers, towers, and other ATC facilities to identify traffic and weather bottlenecks. The night before your flight, our staff begins to check and monitors NOTAMs, TMU advisories, weather, Digital Automatic Terminal Information Service, airport arrival quotas, ground delay programs, playbook and coded departure routes, and more. Experts continually monitors and factors all the latest information right into your flight plan. On your departure day, Flight Sentinel manages your flight plan filing to ensure an on-time departure and provides true point to point flight following with airborne advisories as needed. Expanding the support we bring your flight operation beyond virtual, Flight Sentinel now brings the resources of Honeywell s experienced pilot training crews, to fill in gaps in crew staffing when the need occurs. Flight Sentinel is the only dispatching and flight operations support service in the industry that provides an experienced pilot to keep flight departments always mission ready. Each new Flight Sentinel subscription now includes the use of pilot staffing services once per year at no additional fee. Honeywell Aerospace NE 36 Street Redmond, WA North America Toll Free: Outside North America: A October Honeywell International Inc.

163 Integrated Flight Planning and Scheduling ENHANCING YOUR FLIGHT SUPPORT SERVICES Flight Planning and Scheduling Just Became Easier

164 Integrated Flight Planning and Scheduling Flight planning and scheduling just became easier. If you use CTA-FOS for scheduling and Honeywell GDC for flight support services, you re in for a significantly improved customer experience. As a leader in providing the business jet flight departments and charter operators with professional, efficient and unique, flight planning and dispatching services, Honeywell s Global Data Center introduces the industry s only truly integrated software solution that connects pilots and schedulers. The value of this service is realized by seamlessly connecting flight plans entered into mygdc.com with the CTA-FOS scheduling software creating truly integrated communications link between crews and schedulers making flight operations more efficient and working in complete harmony. By connecting scheduling software to the flight plan in mygdc.com, For more information: visit us online at or there are no entry duplications, flight planning and scheduling information is always up to date which makes the complex coordination with all departments much easier and more accurate. For more efficiency on the road, mobile connectivity to flight planning software and other services offered through mygdc.com can be also be performed using a smart phone, Iphone, Android and Blackberry through mymobilegdc.com. Flight plan changes, aircraft weight and balance, runway analysis all work together to offer a complete package for more efficient flight planning coordination. Included as part of a premium flight plan subscription through the Global Data Center, this is the industry s only flight planning service that closes the loop between scheduling departments and crews for large flight departments, charter operations, or single aircraft operators Benefits Easy and Flexible Flights scheduled using CTA-FOS application by schedulers is immediately available on mygdc.com for pilots to flight plan and file OR Users can plan their trip from CTA-FOS application which can be viewed simply by opening up a browser from FOS, without re-entry into the GDC system. Reduced work communication between the dispatcher and pilot maximizes productivity by limiting the amount of unnecessary re-work. Peace of Mind Users can compute the flight plans from GDC for the trips planned in CTA-FOS and the corresponding flight plan can be viewed from CTA- FOS application, ensuring that the scheduling department and pilots are on the same page at all times. Features View and File Flight Plans for Scheduled Trips at MyGDC.com No data entry duplication - sharing of data is seamless Access the GDC application while in the CTA FOS software View from both CTA FOS and GDC is harmonious Honeywell Aerospace NE 36 Street Redmond, WA North America Toll Free: Outside North America: A October Honeywell International Inc.

165 Real Time, Reliable Communications Datalink communications

166 Real Time, Reliable Communications Overview: For over 25 years, the GDC has provided VHF and satellite datalink communications to any datalink-equipped aircraft worldwide. GDC s robust two-way ACARS (Aircraft Communications Addressing and Reporting System) data communications is compatible with a variety of VHF and satellite networks across the globe. With enterprise level connections to communications networks worldwide, GDC can relay messages almost anywhere. We also offer subscribers a wide choice of data link services to choose from. Datalink services include free text messaging, Pre-Departure Clearances (PDC), Oceanic Clearances, Transcribed Weather Information for Pilots (TWIP), and many others. GDC also offers expert service & support for a variety of datalink avionics. The Global Data Center offers service to the aviation industry s wide selection of airborne data link communications hardware, providing this service seven days a week, twenty four hours a day, three hundred and sixty five days a year. We offer reliable service solutions for AFIS, Primus Epic, TeleLink, and UniLink equipped aircraft - as well as all of the commercial air transport Communications Management Unit (CMU) systems. Services can be accessed via telephone, Internet, or your aircraft s flight management system. Our experienced staff of Flight Data Specialists (FDS) is always available to assist you with a variety of tasks including flight planning, message forwarding, and troubleshooting. The FDS staff has been specially selected for their real life aviation experience and professional certifications. Incoming calls are answered quickly to provide the fastest response to busy flight crews on the road. We offer multiple service plans to meet the needs of large and small flight departments, with flexible package pricing. GDC customers in the commercial air transport, corporate, government and military aviation segments depend on our unsurpassed reliability, and our relentless customer focus as critical to their success. For more information on how the Global Data Center can enhance your flight operations, please call us at: ext. 4, or To visit us on the web, go to or

167 Datalink Services Service to all datalink avionics Uplink flight plans to Flight Management Computers (FMC) Terminal Weather and SIGMETs Winds and temperatures aloft Digital ATIS (D-ATIS) and TWIP reports Pre-Departure Clearances (PDC) and Datalink Oceanic Clearances North Atlantic (NAT) Track routes and other ATC oceanic routes Air-to-ground/ground-to-air/ air-to-air messages , voice, pager or facsimile messages Assisted message delivery Datalink Networks Supported VHF Networks: SITA ARINC Other regional networks Satellite Constellations: Inmarsat Aero C, H, H+, I Iridium Datalink Graphical Weather* Includes But Not Limited To: Worldwide significant weather charts U.S. Categorical METAR (CATMET) charts U.S. National and Regional Radar (NEXRAD) charts Worldwide winds and temperatures aloft charts Worldwide clear air turbulence charts Worldwide convective charts Satellite (cloud height) charts * Availability dependent upon aircraft avionics configuration and software levels Key Benefits Reduced pilot workload Worldwide datalink communications over any network Customized plans to meet any budget or flight schedule. For more information on how the Global Data Center can enhance your flight operations, please call us at: ext. 4, or For More Information: visit us online at or

168 Honeywell Aerospace NE 36 Street Redmond, WA North America Toll Free: Outside North America: A October Honeywell International Inc.

169 MAINTENANCE SERVICE PLAN (MSP) Business aviation s most comprehensive maintenance program

170 Business Aviation s Most Comprehensive Maintenance Program Your aircraft is a big investment...an investment worth protecting. Designed specifically for your Honeywell engines and Auxiliary Power Units (APUs), MSP is an efficient and cost-effective program offering a practical alternative for managing future maintenance expenses. Aircraft owner/operators have learned to rely on MSP to protect them from the unexpected. So avoid unplanned maintenance costs. Avoid downtime. Avoid unnecessary stress. After all, when it comes to your aircraft, time is money. AVOID UNPLANNED MAINTENANCE COSTS AVOID DOWNTIME AVOID UNNECESSARY STRESS Backed by Product Experts Designed and supported exclusively by Honeywell, the experts behind your engines and APUs, MSP delivers peace of mind in knowing you re covered by the best. Predictable Engine and APU Maintenance Costs Increases accuracy of aviation department s annual budgeting Provides predictable long range financial planning Eliminates cost impact of unscheduled repairs Covers replacement costs of cycle life-limited hardware Annual rate adjustments are limited by U.S. Government economic indices Increase the Value of Your Aircraft Enroll in MSP and enhance the resale value of your aircraft. MSP is officially recognized and rated for its aircraft appreciation in the Aircraft Bluebook Price Digest. Continuous Financial Coverage for Service and Repair Scheduled major maintenance Unscheduled maintenance Service Bulletin incorporation for guaranteed state-of-the-art configuration Rental engine during Compressor Zone Inspections and extended unscheduled maintenance

171 MSP Coverage Options Engine MSP Gold Gold NRL APU MSP Gold Gold On Condition Maintenance CAMP Engine Trend Monitoring S.O.A.P. Kit and Analysis Routine Inspection Parts 1 NLS Routine Inspection Labor Major Periodic Inspection (MPI) / Compressor Zone Inspection (CZI) / Hot Section Periodic Inspections (HSI) Inspection Labor Consumable Parts 1 Component Repair Labor (If Required) Other Required Parts Rental Engine During CZI (From Honeywell Engine Bank) Life Limited Parts Engine Removal and Reinstallation and/or Access Time 2 Transportation of Engine 2 Troubleshooting Labor Allowance 3 Consumable Parts 1 Other Required Parts Component Repair Labor (If Required) Rental Engine (From Honeywell Engine Bank) Exchange Engine/Module/Line Replaceable Unit (LRU) Engine and LRU Removal and Reinstallation and/or Access Time 2 Logistical Support for Road Trips (Engine AOG Only) 2 FOD Gap Coverage 5 Transportation of Unserviceable Engine or LRU Service Bulletins: Category 1, 2, and 3 4 Engine Conversion / Upgrade at Reduced Cost Increases Aircraft Resale / Trade-In Value Program Transferable at Time of Sale New Aircraft APU MSP at No Cost for 5 Years if Propulsion Engines on MSP Routine Inspection MPI / CZI / HSI Unscheduled Maintenance Additional Benefits 1 Fluids (oil, fuel etc.) are not covered 2 Per MSP standard business practices 3 MSP up to 10 hours. MSP Gold up to 20 hours (more than 10 hours requires approval and/or justification). Warranty up to 10 hours (more than 10 requires approval and/or justification). 4 Labor will be covered by MSP when bulletins are incorporated in conjunction with other covered maintenance activities providing convenient access to the applicable engine area; otherwise, labor expenses will be the operator s responsibility. 5 Applicable only to FOD events occurring January 1, 2015 or later. Does not apply to CFE738. NOTE: Service bulletins identified as Category 1, 2, and 3 will be incorporated into MSP engines according to the Compliance Section of the bulletin. All coverage is detailed in executed contract with owner/operator. Examples of items not covered by MSP or MSP GOLD: Items not contained in IPC such as airframe parts and fluids (oil, fuel, etc.); overtime; expedite fees; transportation of components other than engines/apu s and LRU s; labor for ECU downloading; Service Center administration fees for logbook review, material control, freight for internal work orders, etc.; or any service not provided by a Honeywell Authorized Service Center. MSP Gold is not available for TPE331.

172 Find Out More For more information about MSP or to obtain an enrollment quote, please contact any Honeywell Authorized Service Center or one of the MSP Sales Administration offices listed below. We look forward to discussing MSP enrollment benefits with you. Call us at: Or visit us online at: Honeywell Aerospace 1944 East Sky Harbor Circle Phoenix, AZ aerospace.honeywell.com N I 05/ Honeywell International Inc.

173 Flight Support Services CABIN SERVICES THAT KEEP YOU CONNECTED WHETHER YOU'RE ON THE GROUND OR IN THE AIR Honeywell Flight Support Services powered by Satcom Direct.

174 As a premier provider of flight support services for business aviation, Honeywell is focused on making your flight operations as effective as possible, through our comprehensive flight planning, cabin communications and database services. From flight routing, weather information and database updates to satellite communications, in-flight television news services, and data connectivity. With these technologies, we have the right mix of flight support solutions and subscription services to meet your unique operational requirements and aircraft needs. Honeywell and Satcom Direct now offer aircraft operators increased flexibility in choosing services to meet their specific business requirements. Operators can now purchase flight support and cabin communications services as a comprehensive package that saves time and the cost of managing multiple contracts and suppliers. In addition to a complete solution, aircraft operators are still able to purchase and utilize specific services separately from both Honeywell and Satcom Direct. Find out more For further information, contact our Service Support team at (888) or us at gfo@mygdc.com. Additional information is also available online at or at (321) , sales@satcomdirect.com, Features Reliable Voice High-speed data Data communications connectivity Satellite television availability Iridium Inmarsat Swift 64 SwiftBroadband Global One Number Plane Simple website access Aero X data compression Benefits Flexible services Comprehensive packages Simplified billing Comprehensive solution for services One number for Inmarsat, Iridium and Magnastar services Fast and friendly customer service Simple activation and configuration management Real-time S64 network congestion monitoring Invoices available online VOIP calling capability Honeywell Aerospace N. Deer Valley Phoenix, AZ Toll Free: International: A October Honeywell International Inc.

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176 Honeywell Aerospace Honeywell is a leading global provider of integrated avionics, engines, systems and service solutions for aircraft manufacturers, airlines, business and general aviation, military, space and airport operations. For more information on Honeywell Aerospace, visit us online at Go Direct Services Find Out More Visit us online at Honeywell Aerospace 1944 East Sky Harbor Circle Phoenix, AZ U.S. Toll Free: International Tel: EMEAI Toll Free: EMEAI Direct Dial: A November Honeywell International Inc. Unlock your aircraft capabilities for Required Navigation Performance (RNP) operations

177 As a FAA approved consultant, Honeywell helps simplify the Required Navigation Performance Special Aircraft and Aircrew Authorization Required (RNP SAAAR) approval process with Go Direct Services. As a key component of the FAA s nextgeneration performance-based navigation system, RNP SAAAR procedures allow aircraft to fly more precise approaches and departures, increasing operational efficiency while reducing operating costs, noise and emissions. To help gain FAA approvals for RNP SAAAR, Honeywell provides a full range of consulting services, including operational approvals, navigation data validation, and monitoring program to quickly guide operators through the FAA operational approval process and maintain compliance with all regulations. RNP Approaches For decades, modern aviation has relied on ground-based navigation aids, but recent industry developments are driving the adoption of RNP techniques using global positioning system (GPS) as a method of increasing capacity and improving traffic flow. RNP enables aircraft to fly more precise approaches, providing benefits for lower minima operations, more favorable routing in congested or terrainchallenged and special use airspace, noise abatement compliance, improved safety, and lower operating cost. A combination of onboard navigation technology, precise sensors and the GPS satellite network keep aircraft within a tightly specified airspace corridor. Aircraft can precisely fly a wide variety of desired flight paths including curved paths to avoid terrain and obstacles, thereby overcoming limitations of conventional instrument procedures. Operational Approvals RNP SAAAR Approach Procedure Sun Valley Idaho Hailey Airport (KSUN) RNAV (RNP) Runway 31 Lowest approach minimums give highest availability to Sun Valley (2% improvement over the GPS RNAV approach) Per FAA Advisory Circular , operators are required to obtain approvals from the FAA to fly RNP approach procedures. Operators would need to show compliance by meeting the specific requirements for equipment, flight operations, and navigation database integrity. Additionally, aircraft must be equipped with FMS, IRS, GPS, EGPWS with terrain and obstacle alerting, and flight management system software to meet the minimum aircraft requirements needed to conduct flight operations with RNP levels <0.3 nm. Go Direct Services Go Direct provides a full line of services to not only help ease the burden of the FAA approval process, but also to simplify the implementation of RNP SAAAR into your flight operations. Aircraft operators that obtain full operational approval will be able to fly all the FAA created public RNP SAAAR approaches. Consultancy technical expertise and guidance to assist with the RNP SAAAR approval process for compliance with AC regulations, providing the most timely and efficient integration of requirements into current flight operations. RNP SAAAR Required Equipment Enhanced Ground Proximity Warning System (EGPWS) Navigation Database Validation comprehensive validation process that is synchronized with the Navigation Data production process to ensure that RNP SAAAR procedures are validated in-cycle for each new navigation database update. Monitoring Program provides record keeping of operators RNP SAAAR operations per AC requirements. Aircraft Equipment Honeywell offers both hardware and software upgrades to meet all the RNP SAAAR requirements in accordance with AC for your specific aircraft. Operator Benefits Better access to terrainchallenged airports, and special use airspace Enables parallel runway, converging and adjacent airport operations Improved access to business airports in proximity to high traffic airports Lower Minima resulting in fewer weather-related delays, and diversions Better access for environmental concerns Reduced flight time due to optimized routing Smaller environmental footprint due to reduced noise and fuel use Enables early, guided turns on missed approach More reliable, repeatable flight paths Improved flight path aligns closer to runway (5 deg versus 14 deg for the GPS RNAV approach) RNP 0.3 guided missed approach path provides low minimums with added safety Inertial Reference System (IRS) Flight Management System (FMS) Global Positioning System (GPS)

178 Honeywell Go Direct Services Due to the complexity of RNP SAAAR operations and certification challenges, the FAA has emphasized that a high level of oversight is required. As a result, the FAA has solicited a call for RNP consultants. Honeywell received FAA designation as a Consultant for RNP SAAAR operational approvals in November In order to meet the needs of operators and aircraft manufacturers to implement this technology, Honeywell is offering a suite of services and tools related to RNP SAAAR. Overview of Honeywell Go Direct Services to Operators: The FAA RNP Consultant designation positions Honeywell to effectively assist operators with the RNP SAAAR operational approval process. Further, Honeywell is offering customers a full line of RNP related services including: Navigation database validation, RNP monitoring, RNP prediction services. These added services will enhance efficiency of RNP SAAAR operations for corporate operators. Go Direct services includes the following services to help operators develop and implement a robust RNP SAAAR program in full compliance with AC , resulting in timely FAA operational approval: 1. RNP SAAAR Consultancy to assist operators with the RNP SAAAR approval process to comply with the AC The consultancy team will assist operators with the following: Technical expertise and guidance for every operational requirement in the AC Established relationships with FAA Dedicated team of consultants RNP SAAAR gap analysis of operator s current processes and documentation Standardized application package and FAA approval recommendation Reduced timeline for approval 2. Navigation Database Validation to comply with the requirements of Appendix 3 of AC The DB validation process will be synchronized with the Navigation Data production process to ensure that the procedures are validated in-cycle for each new database. The DB validation process includes, A Visual comparison of the source database to the FAA 8260 Flyability validation through use of Honeywell FMS simulators Evaluation of nuisance EGPWS warnings Provide letter to operator that lists all validated RNP procedures in compliance of AC RNP Monitoring Program that provides record keeping of all operator s RNP operations. As per AC requirements every 30 days a written report will be sent to the FAA with details of all operations and a technical review of results. The operator will be provided Blackberry and web-based templates to facilitate the record keeping. 4. RNP SAAAR Training: Honeywell is working with Training providers to develop RNP SAAAR training programs that comply with the AC RNP Prediction Tool that provides a detailed assessment of RNP availability for the entire route of flight. This tool is expected to be available in Overview of Honeywell RNP SAAAR Services to Aircraft Manufacturer: Honeywell will offer the following services to the Aircraft manufacturer to enable aircraft certification for RNP SAAAR in accordance with Appendix 2 of AC Regulatory expertise to interpret Appendix 2 of AC Compliance matrix for Appendix 2 Recommendations for detailed Operational consideration (Appendix 4) material Recommendations for revisions to maintenance manual and minimum equipment list Performance-Based Navigation Introduction In 2003, the FAA published THE ROADMAP TO PERFORMANCE-BASED NAVIGATION, which publicly announced the strategy to modernize the NAS (US National Airspace System). Performancebased navigation is a general term that defines navigation performance requirements for an air traffic route, instrument procedure, or defined portion of airspace. Performance-based navigation provides a basis for the design and implementation of non-conventional flight paths for airspace design and obstacle traditionally been equipped with multisensor RNAV systems are referred to as clearance. Using this strategy, the FAA intends to address current limitations on air Flight Management Systems. The transportation capacity by making more performance requirements for these efficient use of the airspace. The FAA systems are defined in specific FAA continues to work collaboratively with the Advisory Circulars and Technical Standards international community through the efforts Orders. of ICAO, Eurocontrol, and the North American Aviation Trilateral; and numerous RNP is the latest advancement in RNAV bilateral partnerships to achieve common systems evolution. RNP defines the requirements and operations. (The navigation performance level required to Roadmap is consistent with the ICAO operate in a particular airspace or on a Performance-Based Navigation Manual.) designated route (i.e. Enroute, Terminal, or Approach). RNP-approved systems The strategy bases its foundation on two provide the same onboard capability to key navigation concepts: RNAV (Area Navigation) and RNP (Required Navigation Performance). It also assures benefit to operators who invest in existing and future capabilities. RNAV vs. RNP conduct traditional RNAV operations. These systems also have the ability to navigate with a much higher degree of accuracy along with the ability for the flight crew to monitor the navigational performance of the system and alert the flight crew if a certain performance requirement is not met. This capability enables operations with reduced obstacle clearance criteria for terminal area procedures as well as closer route spacing - a major contributor to the benefits of performance-based navigation. Figure 1 depicts the general benefits to RNAV and RNP over conventional airspace design, routes and procedures. Honeywell Aerospace 1944 East Sky Harbor Circle Phoenix, AZ U.S. Toll Free: International Tel: EMEAI Toll Free: EMEAI Direct Dial: A October Honeywell International Inc. RNAV systems and their associated operational procedures have been evolving for air transport, regional and corporate aircraft for many years. Most RNAV systems are capable of utilizing navigation signals from various ground and spacebased facilities to achieve a high level of position accuracy. Aircraft that have Figure 1 - Airspace Requirements Comparison for Conventional, RNAV, and RNP Operations

179 RNP SAAAR Procedure Design Benefits of RNP SAAAR RNP capability provides an unprecedented flexibility in construction of approach procedures, resulting in improved efficiency, access, safety and capacity. Conventional approach procedures (VOR, ILS, etc.) use fixed obstacle evaluation areas based on the location and accuracy of the ground-based navigation aids and predefined capabilities of the aircraft s navigation system. RNP SAAAR criteria for obstacle evaluation, however, are flexible and designed to adapt to unique operational environments. They use reduced lateral obstacle evaluation areas and vertical obstacle clearance surfaces based on a RNP value (e.g. RNP 0.3 nm) and may contain curved RF legs (constant radius turns). Aircraft and operators gain authorization to fly these procedures to the specified RNP value through FAA approval and compliance with FAA Advisory Circular Containment Criteria The concept of RNP is a significant enhancement to airspace use, design and management. The benefits of RNP SAAAR are derived directly from procedure design flexibility, the use of reduced obstacle clearance areas and curved flight paths. RNP procedures are considered 3- Dimensional as they provide longitudinal, lateral and vertical path deviation information. Conventional procedure design predicated on ground-based navaids use trapezoidal obstacle clearance areas which increase as a function of the distance from the navaid (navigation accuracy increased as the aircraft came closer to the facility). Whenever obstacles are observed to be within the obstacle clearance area, approach minimums must be raised to ensure clearance from these obstacles. RNP SAAAR procedures rely solely on satellite based navigation (GPS) and, therefore, use linear obstacle evaluation areas for procedure design and determination of approach minimums. For the purpose of procedure design, RNP SAAAR represents the navigation performance required to maintain flight within the obstacle evaluation area associated with the procedure. In general terms, an approach with a specified RNP value means the perpendicular distance between the course centerline and the nearest obstacle must be at least 2X the RNP value specified for the approach. For example, an approach with an RNP value of 0.3 means that the closest obstacle perpendicular to the course centerline must be no closer than 0.6 NM away. The result is a lower approach minimum because obstacles that were previously considered using the trapezoidal method are no longer a factor when using linear containment criteria specified for RNP SAAAR. Aircraft Equipment In order to fully realize the benefits of RNP and to comply with federal regulations, airframe manufacturers rely on Honeywell s advanced avionics to provide the guidance required for RNP SAAAR operations. Honeywell s flight management systems incorporate highly accurate GPS and IRS information to safely guide aircraft through any approved RNP SAAAR procedure. A validated navigation database allows the FMS to read the approach designer s aircraft guidance along the approach path as well as the missed approach procedure, if necessary. In addition to the high level of navigation accuracy, the Enhanced Ground Proximity Warning System monitors the aircraft position and flight path to provide an extra level of safety. These technologies allow the operator to conduct RNP approaches to the high standards required for SAAAR operations. Flight Crew Operational Approval In addition to aircraft equipment requirements, flight crews must be properly trained and qualified in order to fly RNP SAAAR approaches. It is necessary to revise SOPs (Standard Operating Procedures) and checklists in order to provide pilots sufficient guidance to conduct RNP SAAAR operations. Typically, this guidance is developed in accordance with recommended policies and procedures provided by the OEM. The operational benefits to RNP SAAAR are numerous. A few examples of these benefits are: Increased operational efficiency Lower approach minimums More reliable, repeatable flight paths Improved Runway Capacity/Efficiency With today s separation standards for simultaneous runway operations, traffic flow is constricted. As RNP SAAAR procedures proliferate into the national airspace system, the application to operations involving parallel and converging runways and adjacent airports will prove extremely beneficial in reducing airspace congestion. Lower Approach Minimums RNP SAAAR approaches will provide access to terrain-challenged airports which were limited by high minimums or lack of precision instrument approaches. A comparison of the minimums at Palm Springs for the conventional vs. the RNP SAAAR approach is shown in figure 3. Figure 2 - Benefits of RNP SAAAR Approaches for Parallel, Converging, and Adjacent Runways Improved Flight Efficiency circuitous flight paths because of terrain The ability to design and fly highly accurate and/or airspace may be optimized utilizing and repeatable flight tracks with constant more direct routings to the runway, saving radius turns presents an opportunity to time and fuel. greatly increase operational efficiency in numerous areas. Procedures based on RNP SAAAR procedures also offer a wide Curved approach (and missed array of safety enhancements. approach) segments to avoid obstacles Lateral guidance using RF Vertical guidance (VNAV) is available legs increases situational awareness to the runway end. This provides flight and ensures obstacle clearance. crews with better situational awareness, especially at night or in System monitoring and alerting A mountainous terrain. required component of RNP SAAAR is the ability of the aircraft navigation system to monitor its achieved navigation performance, and to identify to the flight crew whether the operational requirement is or is not being met during an operation. This navigation system offers great benefits where terrain, traffic or complicated procedures exist today. Figure 4 - Trapezoidal Obstacle Clearance Requirements Figure 3 - Approach Minimums Comparison for Palm Springs Conventional vs. RNP SAAAR Figure 5 - Trapezoidal Containment vs. Linear Containment

180 LSZ-860 enhancements Honeywell has designed the LSZ-860 to improve upon the previous generation LSZ-850. These improvements include: High tolerance to aircraft noise which is detrimental to performance Increased strike ranging accuracy Doubled lightning detection out to 200 nautical miles Increased display of strike activity Upgrades are now available to all operators of Honeywell s LSZ-850 system. Supporting the system Honeywell's avionics are based on proven technology to provide you with exceptionally high reliability and simplified maintenance. Our award winning product support services include regularly scheduled training classes offered worldwide for both flight crews and maintenance personnel. When service is needed, a global dealer network is the front line for your Lightning Sensor System support. Honeywell's Customer and Product Support organization is committed to keeping your severe weather avoidance system operating day and night, around the world. Leading Particulars of the LSZ-860 LP-860 Receiver/Processor Part Number Output to display UDI, ARINC 429 Range 200 nautical miles Strikes Processed Up to 50 at any time* Display Format Sector or 360 degrees* Dimensions short 1/4 ATR 7.6"x2.4"x14.8" Weight 6.8 lbs Altitude 55,000 ft. Temperature -55 to +70 C Power Requirements 28V dc, 28VA max Mounting Tray P/N Connector Kit P/N X * May be limited by the displaying system AT-850/AT-855 Antenna AT-850 AT-855 (Teardrop)* (Brick) Part Number Dimensions 1.3"x6.1"x11.6" 1.7"x6.0"x7.0" Weight 2.5 lbs 2.5 lbs Altitude 55,000 ft. 55,000 ft. Temperature -55 to +70 C -55 to +70 C Connector Kit P/N X X * Tear drop antennas are preferred over brick antennas due to higher perfomance driven by aircraft mounting options. LU-850/LU-860 Controller LU-850 LU-860 (Rotary switch) (Pushbutton) Part Number X X Dimensions 1/2-3 ATI 1.7"x3.4"x2.6" 1.2"x5.8"x4.0" Weight 0.5 lb 0.6 lb Altitude 55,000 ft. 55,000 ft. Temperature -55 to +70 C -55 to +55 C Mounting Panel Panel Options: - Color Grey/Black Grey/Black - Heading on/off switch Yes No - Lighting 5V and 28V 5V or 28V Blue Filter Connector Kit P/N X X LSZ-860 Lightning Sensor System Find out more... For more information on Honeywell s LSZ-860 Lightning Sensor System, please contact Honeywell Aerospace North 19th Ave. Phoenix, AZ Toll Free: International: Manuals Pilot Operation Handbook System Description and Installation A Service Bulletin (support center conversion from LSZ-850 to LSZ-860) N April Honeywell International Inc. Striking back at severe weather

181 Analyzing weather... and noting a striking difference While most pilots would say that rain doesn't offer the best of flying conditions, most would agree that, by itself, it isn't necessarily enough to ground or divert a flight. What pilots need to avoid is rain containing lightning and its associated turbulence or, more importantly, areas of building thunderstorms that often have no precipitation but damaging lightning activity. Honeywell's LSZ-860 Lightning Sensor System (LSS) provides the tool to help identify areas of potentially destructive lightning. Because some of the heaviest turbulence occurs during the growth stage of a thunderstorm, before precipitation returns intensify, the LSZ-860 is the ideal complement to a weather radar. The system is designed to detect electrical discharge activity that the radar can not see. It then maps the lightning activity onto the weather radar display so the pilot can safely navigate the skies. Radar redundancy equals safety With safety being a primary objective in all Honeywell product designs, we are accustomed to designing cockpit systems with redundancy in mind. If a navigation system fails, there is back-up. If a comm fails, the pilot can revert to the other side. But what do you do if your radar fails? Honeywell s Lightning Sensor System can provide the desired backup. If there is lightning, there is the potential for destructive turbulence, hail and rain. By using the information gathered by the LSS you can safely avoid severe weather. Building thunderstorms Weather radars work by reflecting RF signals off precipitation in the clouds. When thunderstorms are beginning to build they can generate destructive turbulence and electrical activity prior to having sufficient water in them for the radar to detect. What looks like a safe flight path on radar may in fact contain significant lightning activity. The Honeywell LSS detects lightning activity out to 200 nautical miles and displays associated lightning strikes relative to their range and bearing. Cloud-to-cloud With weather radar you often see what appears to be a clear, inviting flight path between weather cells. What you don't see is the electrical activity that may be occurring between the cells. Seeing behind heavy rains Honeywell's LSS enhances the range of the weather radar by displaying electrical activity in areas where the radar signal has fully attenuated and can no longer penetrate. Weather detection symbols Lightning Alert Low rate Medium rate High rate For increased pilot awareness, all lightning signals received are displayed with a magenta lightning alert symbol. This is displayed for 5 seconds on the outside range ring at the correct bearing. Three unique lightning symbols represent the various levels of strike activity identified within the last two minutes. Symbols represent strike activity relative to the aircraft position. Up to 50 strikes can be processed on the display. Heading and velocity stabilized. Complete weather avoidance Honeywell's LSZ-860, the newest Lightning Sensor System, Proposed Flight Path LSZ-860 Typical System Lightning Sensor System detects electromagnetic discharges resulting from lightning activity and converts the signal into strikes that are displayed on a weather radar indicator or EFIS display. The LSS is an excellent enhancement to the weather radar because it detects weather information the radar cannot LP-860 Receiver/Processor 2. AT-850 teardrop antenna, or AT-855 brick antenna Display Sources Pre-flight 3. Radar Indicator The Lightning Sensor System not only has a 120 forward view of the aircraft that overlays a typical radar display, but also a 360 surrounding view. This feature provides critical weather 4. Electronic Flight Instrument System (EFIS) Lightning Sensor System avoidance information to the pilot prior to taxiing out and committing to a specific flight path LU-850 dedicated rotary switch or LU-860 panel mount controller Radar controller with integral LSS control 7. Radar indicator with integral LSS control

182 Maximizing airline efficiency Operating environments and procedures are customer specific. Therefore, customers evaluate and test all ten RAAS advisory options prior to selecting their configured software. Customers base their advisory on a variety of factors including pilot familiarity with the destination airports, typical amount of traffic or risk associated with the airports they serve, and standard operating procedures. The result is to maximize cockpit efficiency and pilot situational awareness and therefore reduce operational costs. Worldwide coverage There are more than 1,900 airports and 6,500 runways in the database. Additional airports and runways can be added upon customer request to ensure worldwide accuracy and availability. Cockpit efficency The system offers five routine voice advisories with an additional five non-routine call-outs for special circumstances. The limited number of advisories reduces cockpit chatter and allows a pilot to quickly react to specific situations without monitoring additional screens or flight deck hardware. Customers evaluate and select the advisories and audio levels appropriate to their operation. There is a menu of selectable audio volumes. All advisories are delivered calmly over the aircraft s audio system (speakers or headphones) in the operator s preference of a male or female voice announced in either feet or meters. Additionally, an optional RAAS inhibit switch is available to silence advisory messages during operation. These features enable you to select the advisories that will maximize operational efficiency. Honeywell aerospace Honeywell is a leading global provider of integrated avionics, engines, wheels and brakes systems and service solutions for aircraft manufacturers, airlines, business and general aviation, military, space and airport operations. For more information on Honeywell Aerospace, visit us online at Global network of support services Honeywell s resources span the Americas, Europe, Middle East, Africa, Asia and the South Pacific to deliver dedicated 24/7 service support. As a world leader in aviation aftermarket services, our global repair centers, logistics network and field services engineering teams are able to quickly repair, supply, and warranty equipment whenever and wherever it is needed. Runway Awareness and Advisory System Find out more For further information on Honeywell s Runway Awareness and Advisory System (RAAS), visit us online at Honeywell Aerospace 1944 E. Sky Harbor Circle Phoenix, AZ Toll Free: International: N August Honeywell International Inc. Reducing the risks of runway incursions and collisions

183 Honeywell s Runway Awareness and Advisory System (RAAS) - a safety solution that improves situational awareness for pilots and increases operational efficiency. Enhanced aircraft situational awareness and runway safety Runway safety management is a dynamic Incursion prevention flight delays caused by disorientation, a key process that involves measuring runway concern for pilots flying into unfamiliar airports. To help prevent such incursions, close calls and incursions, understanding the factors that collisions, the industry requested a safety system contribute to runway collision risks and taking Low installation costs that helps maintain situational awareness during action to reduce those risks. Recent FAA taxiing, take-off and landing. RAAS uses a RAAS identifies the aircraft position at the specific reports and Eurocontrol have estimated that at proven heads-up aural advisory system to alert airport by taking advantage of Honeywell s least one runway incursion takes place each the aircraft crew of their relative runway position Enhanced Ground Proximity Warning (EGPWS) day, which can cause scheduling delays and on the ground, on take-off and on approach to System worldwide runway database. Requiring aircraft damages. The FAA has identified three land. Based on research and FAA runway safety only a simple software upgrade, this system can major factors contributing to these runway reports, ten advisories were developed to provide be implemented in less than an hour, reducing the incursions: communication, airport familiarization maximum situational awareness to minimize the impact on airline operations. and cockpit procedures for maintaining most common runway incursions. The advisories orientation. Additionally, they attribute the loss of provide pilots with increased situational positional awareness as a causal factor in 44% awareness and can help reduce the number of of runway incursions. ROUTINE ADVISORIES OPTIONAL ROUTINE ADVISORIES OPTIONAL NON-ROUTINE ADVISORIES Aural messages that will always be announced to the flight crew Approaching Runway On Ground Approaching one-six right 34L 16R On Runway On Ground On runway three-four left 34L 16R Aural messages that will always be announced to the flight crew, if enabled Approaching In Air Approaching three-four left 34L 16R Distance Remaining Landing and Roll-Out 4,000 remaining, 3,000 remaining, 2,000 remaining, 1,000 remaining, 500 remaining 34L 16R If enabled, rare aural messages that will be announced to the flight crew only when appropriate Extended Holding On Runway On runway three-four left, on runway three-four left 34L 16R Taxiway Takeoff On taxiway! On taxiway! 34L 16R Speed >40 Knots GS Runway End Advisory Callout 100 remaining Speed >40 Knots GS Intersection Departure Insufficient Runway On runway three-four left, 2,000 remaining Immediately after implementation, the system tracks the aircraft s position, heading and ground speed using the aircraft s internal Global Positioning System (GPS). Logic algorithms create a virtual box around the EGPWS runway(s) and activate RAAS to announce the aircraft s position when the aircraft is entering or approaching an active runway. The logic algorithms also determine the appropriate advisory sequence and timing based on the aircraft s ground speed and the remaining length of the runway. Approaching Short Runway In Air Approaching three-four left, 3,000 available 34L 16R Rejected Takeoff 4,000 remaining, 3,000 remaining, 2,000 remaining, 1,000 remaining, 500 remaining 34L 16R Speed >40 Knots GS Select only those advisories appropriate to your operational needs. Key RAAS Benefits Reduced delays caused by crew disorientation Simple EGPWS software upgrade minimizes aircraft down-time Increased cockpit efficiency and reduced pilot workload Global operations support with worldwide airport runway database Increased situational awareness with heads-up voice advisories Select those advisories that best fit your operations to reduce costs and delays Why Honeywell? 30 years of avionics system experience An industry leader in safety system integration Broad range of avionics products and services Innovative technologies with proven reliability Global service and support network (24/7/365) 34L 16R Speed <40 Knots GS 34L 16R

184 Ovation In-flight XM Satellite Radio Live music, news, entertainment and information radio

185 In-flight XM Satellite Radio Honeywell offers XM Satellite Radio as part of your Ovation cabin system to provide passengers with live music and programming from coast to coast. Our system keeps travelers in touch with news and information from the world below while maximizing their entertainment options. Passengers hear up-to-the-minute headlines, business news, sports and weather and can choose from over 70 additional quality music channels. Features include State-of-the-art digital sound with unparalleled signal coverage One, two, four or eight receiver units from a single antenna Multiple receiver configurations to allow each passenger independent listening Built-in interface with the Ovation cabin management system Aircraft quality certified antenna 28V DC power XM broadcasts 100 channels of crystal clear digital audio from its state-of-the-art studios in Washington, DC. Two powerful satellites provide seamless coverage of the continental United States. Programming includes live news, entertainment, sports, and music programming from internationally recognized broadcast leaders including: 1 Channel Receiver (XM1) Size: 1.82 h x 6.45 w x 7.80 d Weight: 2.5 lbs 2 Channel Receiver (XM2) Size: 2.42 h x 6.45 w x 7.80 d Weight: 3.0 lbs 4 Channel Receiver (XM3) Size: 4.55 h x 6.45 w x 7.80 d Weight: 3.5 lbs 8 Channel Receiver (XM8) Size: 7.50 h x w x 7.80 d Weight: 7.5 lbs Teardrop Antenna (XMA) Size: 0.72 h x 2.70 w x 4.30 d Weight: 4.2 oz. All trademarks are the property of their respective owner. Your in-flight XM Satellite Radio integrates with the Ovation cabin management system and is controllable by Ovation button, LCD-scrollable, touch screen and remote passenger controls. Touch screen controls include feedback on XM category, channel, artist and programming title. For further information on Honeywell s XM Satellite Radio system, please visit us online at or call (602) Honeywell Aerospace N. 19th Avenue Phoenix, AZ Toll Free: US: A September Honeywell International Inc.

186 Customers Helping Customers Global Customer Committee Honeywell Business Aviation

187 Introduction and Mission Statement The Global Customer Committee is an independent group of business aviation professionals that works jointly with Honeywell to bring about improvement in aircraft, equipment, operations and services by seeking input from members on any concerns or questions based on the operator s experience, and to represent those topics to Honeywell. The Global Customer Committee s mission is to prevent problems from occurring through a free flowing exchange of information between members and Honeywell, working through a Top 25 action list that is consolidated and prioritized globally. Operating System Customers Helping Customers Committee members include operators, channel partners and pilots specialized in either mechanical or avionics components, in the following regions: Americas: 37 members Europe, Middle East, Africa and India: 23 members APAC: 14 members. Each region has two face to face meetings every year. In addition, there are two Global Telecoms between meetings. Collaboration Working teams collaborate directly with Honeywell on the highest priority actions from the Top 25 List OEM Liaisons communicate with the different Aircraft Manufacturer Customer Advisory Boards to work on issues at the aircraft level This partnership has produced great results, such as: AOG and customer service improvements Functionality added to Honeywell s MyAerospace website Technical fixes resulting in service bulletins, mechanical and electrical Direct Access Support Network Directory Mobile App Americas Leadership Peter Zeeb Americas Chairman Jon Dodson Communications Vice Chair Joe Bocsy Electrical Vice Chair Dan Frisone Operations Vice Chair Gordon MacSwain Mechanical Vice Chair Paco Perez Avila Honeywell Regional C&PS Director Operators Allen Ratterree (NJ) Andy Reiser (TX) Antonio Gascon (OH) Chris Shollenbarger (CA) Dan Frisone (OH) Dave Craig (MI) David McBride (AZ) Derek Ellis (CA) Gerald L. Ferriss (GA) Gordon MacSwain (OH) Iain McGarva (TX) James Grech (OH) Joe Bocsy - (OH) Joe Statt (AZ) John Benjamin (MN) Jonathan Dodson Kent Burke (GA) Mark Wagner (FL) Matt Miller (OR) Paul Westenkirchner (OH) Peter Zeeb (OR) Ron Mckune (WA) Stan Harris (TX) Steve Golden Todd Hotes (CT) Todd Kretschmar (TX) Victor Amadio (CAN) Walt Foley (CA) Willard Sawyer (OH) Yves Tessier (CT) Channel Partners Chris Christianson - Duncan Aviation (NE) Donald R. Fletcher - Standard Aero (GA) Jack Shields - Atals Aircraft Center (NH) Todd Smith - Atlas Aircraft Center (NH) Industry Organizations Elias Cotti NBAA (DC) Training Providers Jennifer Bensky - Flight Safety (TX) Paul Kuchta - Flight Safety (TX) EMEAI Leadership Antonio Lucchi EMEAI Chairman (+31) TBD Mechanical Vice Chair Stefano Trevisan Communications Vice Chair (+39) Antonio Lucchi Electrical Vice Chair (+31) Lee Kirchhofer Honeywell Regional C&PS Director Operators Adrian Hollenbach (ZA) Antonio Lucchi (NL) Arnold Leurs (NL) Bart Hautekeur (BE) Dean Hawkins (UK) Ed Gordon (ZA) João Salgueiro (PT) Marc Carstens (DE) Martin Hermansson (CH) Martin Spiegl (LB) +961 (1) Massimo Vallone (IT) Maurizio Di Loreto (IT) Osman Deniz (TR) Paulo Pestana (PT) Stefano Trevisan (IT) Tiziano Albrizio (MT) Channel Partners Andrea Weyrich - Aero-Dienst (DE) Eckhard Schwanzer - JAB (CH) Gerd Gsanger - Aero-Dienst (DE) Gunilla Hermansson - GKN Aerospace (SE) Hans-Peter Amacher - JAB (CH) Hans-Peter Schaffluetzel - JAB (CH) Jim Hill - Harrods Aviation (UK) Asia Pacific Leadership Pat Dunn Asia-Pac Chairman Samson Franklin Honeywell Regional C&PS Director Operators Craig Macartney (AU) Glenn Western (SG) Grant Ingall (AU) John Glynn (TH) (980) Murtaza Hassan (SG) Patrick Dunn (SG) Peter Cawthorne (HK) Peter Docking (AU) Philip Balmer (HK) Blake Haldeman Tang Jin (CN) Channel Partners David Wearmouth- MetroJet (HK) Desmond Tan - Hawker Pacific Asia Pte Ltd (SG) Yow Kim Fui - Dallas Airmotive Asia-Pacific Pte Ltd (SG) Interested in becoming a member or submit an issue to the Committee? Please visit our website at: committees.honeywell.com. For more information, please us at: GCC@Honeywell.com A September Honeywell International Inc.

188 Honeywell New Customer Establishment Instructions The following request for information is required in order to establish a new customer or request change(s) to an existing customer account. Please read and complete to help us expedite the establishment of your new or changed account. Customer 1. Complete Part I (pages 2-4) 2. Upon return of the New Customer Set up Package, please enclose the following to ensure a timely response: A) Completed New Customer Account Set Up Form (Part 1) including all signatures. B) End Use Certificate if applicable C) Tax Exemption Certificate(s) - Please note if your company is tax-exempt a certificate(s) must be returned with this information. If a complete tax exemption certificate(s) is not received, Honeywell must charge sales tax on your invoices. (except for US Government) 3. Return the complete package of the above items to your customer service representative. Customer Representative ** If setting up an existing customer that is already in an old legacy system, then customer rep will complete PART 1 (page 2 only) by obtaining the data from the legacy system. The credit application part will not be required. Rep will also still follow steps 1-3 below. 1. The Customer Representative will complete Part II (page 5). However, please assist the customer in Part I. 2. Upon receipt of the New Customer Set up Package, review the checklist for completeness. Do not forward the package until it is complete. Incomplete packages will delay customer account set up. 3. Upon completion of New Customer Set up Package or Change Request return to the Customer Representative forward completed package or change requests to Global Credit and Treasury Services. address is GCTS Aero SAP Customer Master, or Fax # Customer Representative Check List 1) The form is complete. a) Name, address, zip, state, city and country must be complete for at least the sold to account. b) General Data area must be filled out completely. c) Sales Data must be filled out completely on required fields. 2) Completed and Signed Credit Application (except for US Government) 3) End Use Certificate if applicable. 4) Tax Exemption Certificate(s) - Please note if your customer is tax-exempt a certificate(s) must returned with this information. If a complete tax exemption certificate(s) is not received, Honeywell must charge sales tax on the invoices. (except for US Government)

189 HONEYWELL NEW CUSTOMER SET UP/CREDIT APPLICATION Please return completed application, sales tax exemption or value added tax certificate and any additional documents with your New Customer Establishment Package to the address listed on page 1 of the Instructions. PART I - Items in Italics are optional. All other requested information must be filled out completely by Customer SOLD TO ACCOUNT (purchasing entity) check if this will also be a shipping location in addition to below. Customer Legal Name: Street Address: Zip Code: - City: Country: State: Phone Number: ( ) - Fax Number: ( ) - Address: If member of the European Union, enter the VAT Registration Number If you are a vendor of Honeywell Aerospace, check Yes No Are you a foreign entity on domestic soil? Yes No If yes, please enter the country: SHIP TO ACCOUNT (fill in only if shipping address is different than the Sold To Acct or in addition to the Sold To) Customer Legal Name: Street Address: Zip Code: - City: Country: *State:. Phone Number: ( ) - Fax Number: ( ) - Freight Forwarder: Account No.: Preferred Carrier: Account No.: *If state change, include a tax exemption certificate if applicable BILLING ACCOUNT (fill in only if this information is different than the Sold to Acct) Customer Legal Name: Street Address or PO Box: Zip Code: - City: Country: State: Phone Number: ( ) - Fax Number: ( ) - Address: PAYER ACCOUNT (fill in only if this information is different than the Billing Acct) Customer Legal Name: Street Address or PO Box: Zip Code: - City: Country: State: Phone Number: ( ) - Fax Number: ( ) - Address:

190 TRADE STYLE/DBA CHECK ONE: Proprietorship Partnership Corporation Subsidiary Division LLC BANK INFORMATION Bank Name Account Number Mailing Address City State Zip Code Your Account Officer Phone Number Fax Number TRADE REFERENCES (THREE) Company Name: Mailing Address: City & State: Zip Code: Phone Number: Fax Number: Contact Person: 1) 2) 3) Annual Company Sales Anticipated Monthly Purchases Do you have EDI and/or EFT capabilities Yes No Do you prefer to ALWAYS pay by credit card? Yes (if yes, no terms will be set for your new acct and all sales orders will require valid credit card information) Are you currently doing business with Honeywell? Yes No If yes: Division Location Financial Statement Required (check one): Attached Will Mail Direct D & B (DUNS # ) Federal ID # (USA only) Sales Tax or Value Added Tax ID # Resale Certificate, Tax Exemption or Value Added Tax form is mandatory to the completion of this application. Please fax with documents.

191 FINANCIAL RELEASE AUTHORIZATION I authorize the references named herein, both financial institutions and trade references, to release any financial and credit information known to them to Honeywell with the understanding that it will be used solely for credit purposes. Furthermore, if this credit application is accepted, I/We agree to pay for purchases in accordance with the terms and conditions set by Honeywell. TERMS OF SALE Honeywell (the Company) provides agreed goods and services in exchange for payment within terms. It is the Company s normal policy to extend payment terms of 30 days from invoice date to qualified applicants. Payment is expected at the Company s designated address (specified on the invoice) within 30 days of the invoice date. Thirty (30) day terms are upheld. Cash on Delivery (COD), Payment Prior to Shipment (PPS) or any other method of payment may be required pending receipt and review of a customer s credit application, financials and references. It is understood and agreed that, once Honeywell has approved the credit application, payment will be tendered according to the assigned credit terms. Honeywell may take any action required in case of failure to make payment as agreed. This may include, but is not limited to, use of outside agencies or attorneys. Costs and fees incurred by outside service agencies or attorneys will be an additional liability on the part of the debtor organization. STATEMENT OF JOINT AND SEVERAL LIABILITY Sole Proprietorships, Partnerships, Joint Ventures, Personally Held Corporations I (WE) agree that the Sole Proprietorship, Partnership, Joint Venture, or Personally Held Corporation indicated below will pay all invoices in accordance with agreed terms. All signatories for this organization agree, in the event of the failure of the organization to pay invoices as rendered, to personally reimburse the Company for all liabilities incurred. Company Name Authorized Signature Printed Name Title Date

192 PART II - To be completed by HW Customer Representative Date Type of Request (check one) New Customer Mirror of Customer from Legacy System Legacy System & Acct # Requestor First/Last Name (customer rep) Phone Number ( ) - Rep Fax Number ( ) - Site Name : Company Code: Distribution Channel: Commercial Government Both HW Resolver EID: Sales office # : Are partial deliveries allowed? Yes No Is customer willing to ship ahead of the initial requested ship date? Yes No If Yes, how many days? Sales office(s): Shipping Terms (Incoterms) * EXW Seller's Facility is standard policy Payment Terms * Cash In Advance is standard policy Price Group 01 Tax Information - All customers will be invoiced indisputable sales tax unless valid Sales Tax Exemption Certificates are provided with Set Up Package or Address Change Request Choose only one: Taxable Tax Exempt Is this a Government Account? Yes No If applicable enter the following: Cage Code DODAAC Currency: (For sites other than Company Code 1000) Order Pending? Yes No If yes, what is the total amount of the order? $ * For GCTSCMA Use Only SOLD TO ACCOUNT BILL TO ACCOUNT PAYER ACCOUNT SHIP TO ACCOUNT SHIP TO ACCOUNT OTHER -SPECIFY Partner Type SIGN OFF: DATE/TIME: NUMBER

193 UNIFORM SALES AND USE TAX CERTIFICATE MULTIJURISDICTION Issued to Seller: Honeywell I HEREBY CERTIFY THAT: Name of Firm (Buyer): Address: is engaged as a registered: - Common Carrier - Wholesaler - Retailer - Manufacturer - Lessor - Direct Pay - Other (Specify) and is registered with the below listed states and cities within which your firm would deliver purchases to us and that any such purchases are for wholesale, resale, ingredients or components of a new product to be resold, leased or rented in the normal course of our business. We are in the business of wholesaling, retaining, manufacturing, leasing (renting) the following: Description of Business: General description of products to be purchased from the seller: State/Local Registration Number State/Local Registration Number AL MS AZ NE AR NV CA NJ CO NM CT NY DC NC FL ND GA OH HI OK ID PA IL RI IN SC IA SD KS TN KY TX LA UT ME VT MD VA MA WA MI WV MN WI MO WY OTHER OTHER I further certify that if any property so purchased tax free is used or consumed by the firm as to make it subject to a Sales and Use Tax, we will pay the tax directly to the proper taxing authority when state law so provides or inform the seller for added tax billing. This certificate shall be part of each order, which we may hereafter give to you, unless otherwise specified, and shall be valid until canceled by us in writing or revoked by the city of state. Under penalties of perjury, I swear or affirm that the information on this form is true and correct as to every material matter. Authorized Signature: Title: (Owner Partner or Corporate Officer) Date: Note: Complete this form only if claiming tax-exempt status or return a copy of your Resale Certificate and/or Exemption Certificate with your completed application.

194 HONEYWELL CUSTOMER STATEMENT OF CERTIFICATION Compliance with United States Export Regulations The person executing this letter is assuming the responsibility of complying with these obligations both as an individual and as a representative of the company that he/she represents. Please ensure the signed letter appears on company letterhead and that all information is complete. It is Honeywell s policy to verify the end-use and end-users for all Honeywell product transactions, and in all transfers of technical data or software. This is to ensure compliance with applicable United States export control laws and regulations, specifically Parts 736 and 744 of the Export Administration Regulations, as well as with the laws and regulations of the selling country. Because the products you are purchasing, or software or technology you are licensing, may be exported and used outside of the United States and/or the selling country, please confirm the following: Our general type of business is: Our specific end-use is: 1. I (We) will not sell, export, re-export, divert or otherwise transfer any Honeywell products, technology or software for use in activities which involve the development, production, use or stockpiling of nuclear activities of any kind, chemical or biological weapons or missiles, unmanned aerial vehicles, or microprocessors for military use, nor use Honeywell products in any facilities which are engaged in activities relating to such weapons or applications, without prior authorization from the U.S. Government and Honeywell notification. If your request concerns any of the activities listed above, identify the activity here. 2. I (We) will not sell, export, re-export, divert or otherwise transfer any Honeywell products, technology or software to any entity or country subject to U.S. Government approval, including, but not limited to, Cuba, Iran, North Korea, Sudan, Syria unless otherwise authorized by the U.S. Government. This also applies for the selling country and their respective Debarred List issued by the Government. 3. I (We) acknowledge that United States law and the selling countries law prohibits the sale, export or re-export, diversion or transfer, or other participation in any export transaction involving Honeywell products with individuals or companies listed in the U.S. Commerce Department s Table of Denial Orders, the U.S. Treasury Department s list of Specially Designated Nationals or the U.S. Department of State s list of individuals debarred from receiving Munitions List items and other applicable lists, i.e., Entity List as well as the Denial Person/Company list of the selling country. 4. I (We) will abide by all applicable United States and/or selling country export control laws and regulations for all products purchased from Honeywell and will obtain any licenses or approvals required by the U.S. Government and/or the selling countries Government prior to the sale, export, reexport, diversion or otherwise transfer of Honeywell s products, software or technology. Signature Date Print Person s Name Company Name Title Address

195 Honeywell Tech Pub Request Form Order Date: 00/00/0000 Send To: Attention: From: Subject: Honeywell Technical Publications Team Mr./Mrs. Company Name Location Contact Number Valid Address New Request for A/C Platform: Make and Model of A/C A. Name of Owner/Operator: B. AC SN: XXXX Tail/Registration #: Current: XXXXX Final: XXXXXX C. Engine and APU Type: XXXXXX D. Date of Delivery or Date to be Delivered: 00/00/20XX E. Pubs to customer need date - : (On or about ) 00/00/20XX F. Media Type: Online G. Special Remarks/Comments: Ship to: c/o Full Company Name ATTN: John Smith Address City, State, Zip Code Phone: CC: c/o Full Company Name ATTN: John Smith Address City, State, Zip Code Phone:

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