AIRCRAFT SPECIFICATION SUMMARY

Transcription

1 AIRCRAFT SPECIFICATION SUMMARY GENERAL Registration Number Aircraft Model MSN Owner Date of Delivery Data as of Date Aircraft Total Hours Aircraft Total Cycles Annual Utilization (FC/FH) (FH/FC) WEIGHT AND STRUCTURAL DATA A4O-EA Max. Take Off Weight 40,370 kgs ERJ LR Max. Taxi Weight 40,530 kgs Max. Landing Weight 34,100 kgs OMAN AIR Max. Zero Fuel Weight 32,000 kgs 23/03/2011 Operating Empty Weight 22,535 kgs 31-Dec-17 Manufacturer s Empty Weight 22,422 kgs 16230:18 Winglets Installed [ ] Yes or [ ] No 14, :42 FH / 1933 FC AIRFRAME MAINTENANCE STATUS* Type of Check Date Aircraft FH / FC Date Aircraft FH / FC C Check 3C Chk 11/12/ :30 / ,000 FH 3/1/ :30 FH Heavy Check Specify Check: Last Accomplished Interval (Months / FH / FC) Next Due 8Y 11/12/ :30 / Years 25/11/ Y 10 Years 22/03/ Y 12 Years 22/03/2023 MAINTENACE PROGRAM Maintenance Program Provided by: Program Approved by Authority of: [ ] Customized or [ ] OEM [ ] FAA or [ ] EASA or [ ] Other: DGSAS OPERATIONAL STATUS ( Not locally Approved for ETOPS and Auto Land operations) LANDING GEAR Part Number Serial Number Gear TSN / CSN Date of Last Overhaul Gear TSN / CSN At Overhaul Date of Installation of Overhauled Gear Overhaul Interval (Years / Cycles) Time Remaining Until Overhaul (Years / Cycles) Landing Gear Brake Manufacturer Brake Type NOSE L/H MAIN R/H MAIN :18 / :18 / :18 / MO or 30,000 FC 144 MO or 30,000 FC 144 MO or 30,000 FC 39 MO or FC 39 MO or FC 39 MO or FC MEGGIT AIRCRAFT BRAKING SYSTEMS CORPORATION [ ] Steel or [ ] Carbon

2 ENGINES* Manufacturer: Model: S/N: Engine TSN / CSN Completion Date of Last Shop Visit Engine TSN / CSN At Last Shop Visit Completion Date of Last Performance Restoration Shop Visit Engine TSN / CSN At Last Performance Restoration Shop Visit Test Cell EGT Margin At Performance Restoration Shop Visit Cycles Remaining to 1 st LLP Limiter Current Operating Thrust Engine Actual Annual Utilization (FH/FC) Excluding Off-Wing Time (if not currently installed on this aircraft) GE CF34-8E5A :20 / :42 / Aug Mar / / Aug / Deg. C K 14K 2157:42 / :42 / 1933 AUXILIARY POWER UNIT* Manufacturer Part Number Serial Number Date of Manufacturer APU TSN / CSN / Completion Date of Last Hot Section Inspection (HSI) / Overhaul APU TSN / CSN At Hot Section Inspection (HSI) / Overhaul HAMILTON SUNDSTRAND E HSC-E Sep-07 Cycles Remaining to 1 st LLP Limiter (if applicable) APU Annual Utilization (Hrs/Cycs) FROM INSTALLATION ON 25 AUG :06 / 871 APU Time Recorded by: [ ] APU Clock or [ ] A/C Time, Ratio: ` INTERIOR CONFIGURATION* Seat Type PAX Quantity Manufacturer Part Number In Seat Video? (Y/N) In Seat Power? (Y/N) Entertainme nt Controls (PCU)? (Y/N) Tourist Class Seats 60 C & D Zodiac First Class Seats Bus. Class Seats 11 C & D Zodiac /103/105 & /103/105 Y Y Y /102/103/104 & /102 Y Y Y Convertible Seats Total present capacity: 71

3 IN-FLIGHT ENTERTAINMENT SYSTEM Entertainment System Name: Manufacturer: Passenger Entertainment (Audio) Passenger Entertainment (Video) Audio / Video On Demand Moving Map / Airshow Overhead Video: THALES I4500 IFE SYSTEM THALES [ ] Yes or [ ] No PSU Mounted Y Aisle Mounted Projector GALLEYS AND LAVATORIES Quantity Manufacturer Location PART NUMBER Type Galleys 3 C & D Zodiac Lavatories 2 C & D Zodiac G G G FWD AFT [ ] Atlas or [ ] KSSU or [ ] Other Flush [ ] or Vacuum [ ] CARGO COMPARTMENT Cargo Loading System Installed: Type of System Installed: Smoke / Fire Detection System Installed: Fire Suppression System Installed: [ ] Yes or [ ] NO Note: The cargo compartment loading systems comprise the cargo compartment nets [ ] Powered or [ ] Non-Powered [ ] Yes or [ ] No [ ] Yes or [ ] No FUEL SYSTEM Fuel Capacity (US Gallons) #1 Auxiliary Tank [} #2 Auxiliary Tank [] Fuel Instrument/Calibration in: Approximately 3095 Gal [ ] Provisioned [ ] Installed [ ] Provisioned [ ] Installed [ ] Kilograms or [ ] Pounds Capacity (US Gallons): Capacity (US Gallons): AVIONICS Auto Flight - 22 MODULE,ELECTRONIC-FLIGHT CONTROLS,FCM THRUST CONTROL QUADRANT- WITH AUTOTHROTT Qty. Manufacturer Part Number 4 HONEYWELL ED35E KAISER ELECTROPRECIS Communications - 23 HF Transceiver VHF Transceiver SDU SATCOM Data Unit PRERECORDED ANNOUNCEMENT Tape Reproducer or DVD Player (Video Entertainment) HF COMM TRANSCEIVER SELCAL Printer Fixed ELT Flight Deck Door Camera System 1 HONEYWELL HONEYWELL C&D PBS HONEYWELL HONEYWELL ARTEX

4 Indicating and Recording 31 DVDR DIGITAL VOICE-DATA RECORDER AUXILIARY FLIGHT DATA ACQUISITION 2 HONEYWELL SAGEM ED35E Navigation 34 ADC (Air Data Computer) INERTIAL REFERENCE UNIT Enhanced Ground Proximity Warning Computer Windshear System Installed? 4 ROSEMOUNT AEROSPACE 2015G2H2H-9 2 HONEYWELL HG2100AB02 1 HONEYWELL If yes, [ ] Reactive or [ ] Predictive? Weather Radar Transceiver 1 HONEYWELL INTEGRATED ELECTRONIC 1 THALES AVIONICS C16393AA02 STANDBY TCAS Computer 1 HONEYWELL ATC Mode S Transponder DME Interrogator 2 2 HONEYWELL HONEYWELL Marker Beacon Receiver 1 SENSOR SYSTEMS INC S VIDL MODULE - VOR, ILS, MKR BCN 2 HONEYWELL SOFTWARE RADAR ALTIMETER 2 HONEYWELL ADF 1 HONEYWELL GPS MODULE 1 HONEYWELL Control Display Unit 2 HONEYWELL

5 AIRCRAFT SPECIFICATION SUMMARY GENERAL Registration Number Aircraft Model MSN Owner Date of Delivery Data as of Date Aircraft Total Hours Aircraft Total Cycles Annual Utilization (FC/FH) (FH/FC) WEIGHT AND STRUCTURAL DATA A4O-EB Max. Take Off Weight 40,370 kgs ERJ LR Max. Taxi Weight 40,530 kgs Max. Landing Weight 34,100 kgs OMAN AIR Max. Zero Fuel Weight 32,000 kgs 01/04/11 Operating Empty Weight 22,518 kgs 31-Dec-17 Manufacturer s Empty Weight 22,422 kgs 16080:27 Winglets Installed [ ] Yes or [ ] No 14, :16 FH / 1952 FC AIRFRAME MAINTENANCE STATUS* Type of Check Date Aircraft FH / FC Date Aircraft FH / FC C Check 3C Check 4/1/ :27 / ,000 FH 24/01/ :22 FH Heavy Check Specify Check: Last Accomplished Interval (Months / FH / FC) Next Due 8Y 4/1/ :27 / Years 23/12/ Y 10 Years 1/4/ Y 12 Years 1/4/2023 MAINTENACE PROGRAM Maintenance Program Provided by: Program Approved by Authority of: [ ] Customized or [ ] OEM [ ] FAA or [ ] EASA or [ ] Other: DGSAS OPERATIONAL STATUS ( Not locally Approved for ETOPS and Auto Land operations) LANDING GEAR Part Number Serial Number Gear TSN / CSN Date of Last Overhaul Gear TSN / CSN At Overhaul Date of Installation of Overhauled Gear Overhaul Interval (Years / Cycles) Time Remaining Until Overhaul (Years / Cycles) Landing Gear Brake Manufacturer Brake Type NOSE L/H MAIN R/H MAIN :27 / :27 / :27 / MO or 30,000 FC 144 MO or 30,000 FC 144 MO or 30,000 FC 39 MO or FC 39 MO or FC 39 MO or FC MEGGIT AIRCRAFT BRAKING SYSTEMS CORPORATION [ ] Steel or [ ] Carbon

6 ENGINES* Manufacturer: Model: S/N: Engine TSN / CSN Completion Date of Last Shop Visit Engine TSN / CSN At Last Shop Visit Completion Date of Last Performance Restoration Shop Visit Engine TSN / CSN At Last Performance Restoration Shop Visit Test Cell EGT Margin At Performance Restoration Shop Visit Cycles Remaining to 1 st LLP Limiter Current Operating Thrust Engine Actual Annual Utilization (FH/FC) Excluding Off-Wing Time (if not currently installed on this aircraft) GE CF34-8E5A :10 / :26 / Dec Oct / :47 / Oct :47 / K 14K 2147:22 / :22 / 1953 AUXILIARY POWER UNIT* Manufacturer Part Number Serial Number Date of Manufacturer HAMILTION SUNDSTRAND E HSC-E Apr-11 APU TSN / CSN 18001:36 / Completion Date of Last Hot Section Inspection (HSI) / Overhaul 23-Dec-15 APU TSN / CSN At Hot Section Inspection (HSI) / Overhaul / Cycles Remaining to 1 st LLP Limiter (if applicable) APU Annual Utilization (Hrs/Cycs) 3295:36 / 2802 APU Time Recorded by: [ ] APU Clock or [ ] A/C Time, Ratio: INTERIOR CONFIGURATION* Seat Type PAX Quantity Manufacturer Part Number In Seat Video? (Y/N) In Seat Power? (Y/N) Entertainme nt Controls (PCU)? (Y/N) Tourist Class Seats 60 C & D Zodiac First Class Seats Bus. Class Seats 11 C & D Zodiac /103/105 & /103/105 Y Y Y /102/103/104 & /102 Y Y Y Convertible Seats Total present capacity: 71

7 IN-FLIGHT ENTERTAINMENT SYSTEM Entertainment System Name: Manufacturer: Passenger Entertainment (Audio) Passenger Entertainment (Video) Audio / Video On Demand Moving Map / Airshow Overhead Video: THALES I4500 IFE SYSTEM THALES [ ] Yes or [ ] No PSU Mounted Y Aisle Mounted Projector GALLEYS AND LAVATORIES Quantity Manufacturer Location PART NUMBER Type Galleys 3 C & D Zodiac Lavatories 2 C & D Zodiac G G G FWD AFT [ ] Atlas or [ ] KSSU or [ ] Other Flush [ ] or Vacuum [ ] CARGO COMPARTMENT Cargo Loading System Installed: Type of System Installed: Smoke / Fire Detection System Installed: Fire Suppression System Installed: [ ] Yes or [ ] NO Note: The cargo compartment loading systems comprise the cargo compartment nets [ ] Powered or [ ] Non-Powered [ ] Yes or [ ] No [ ] Yes or [ ] No FUEL SYSTEM Fuel Capacity (US Gallons) #1 Auxiliary Tank [} #2 Auxiliary Tank [] Fuel Instrument/Calibration in: Approximately 3095 Gal [ ] Provisioned [ ] Installed [ ] Provisioned [ ] Installed [ ] Kilograms or [ ] Pounds Capacity (US Gallons): Capacity (US Gallons): AVIONICS Auto Flight - 22 MODULE,ELECTRONIC-FLIGHT CONTROLS,FCM THRUST CONTROL QUADRANT- WITH AUTOTHROTT Qty. Manufacturer Part Number 4 HONEYWELL ED35E KAISER ELECTROPRECIS Communications - 23 HF Transceiver VHF Transceiver SDU SATCOM Data Unit PRERECORDED ANNOUNCEMENT Tape Reproducer or DVD Player (Video Entertainment) HF COMM TRANSCEIVER SELCAL Printer Fixed ELT Flight Deck Door Camera System 1 HONEYWELL HONEYWELL C&D PBS HONEYWELL HONEYWELL ARTEX

8 Indicating and Recording 31 DVDR DIGITAL VOICE-DATA RECORDER AUXILIARY FLIGHT DATA ACQUISITION 2 HONEYWELL SAGEM ED35E Navigation 34 ADC (Air Data Computer) INERTIAL REFERENCE UNIT Enhanced Ground Proximity Warning Computer Windshear System Installed? Weather Radar Transceiver INTEGRATED ELECTRONIC STANDBY 4 ROSEMOUNT AEROSPACE 2015G2H2H-9 2 HONEYWELL HG2100AB02 1 HONEYWELL If yes, [ ] Reactive or [ ] Predictive? 1 HONEYWELL THALES AVIONICS C16393AA02 TCAS Computer ATC Mode S Transponder DME Interrogator HONEYWELL HONEYWELL HONEYWELL Marker Beacon Receiver 1 SENSOR SYSTEMS INC S VIDL MODULE - VOR, ILS, MKR BCN SOFTWARE 2 HONEYWELL RADAR ALTIMETER 2 HONEYWELL ADF 1 HONEYWELL GPS MODULE 1 HONEYWELL Control Display Unit 2 HONEYWELL

9 AIRCRAFT SPECIFICATION SUMMARY GENERAL Registration Number Aircraft Model MSN Owner Date of Delivery Data as of Date Aircraft Total Hours Aircraft Total Cycles Annual Utilization (FC/FH) (FH/FC) WEIGHT AND STRUCTURAL DATA A4O-EC Max. Take Off Weight 40,370 kgs ERJ LR Max. Taxi Weight 40,530 kgs Max. Landing Weight 34,100 kgs OMAN AIR Max. Zero Fuel Weight 32,000 kgs 25-Aug-12 Operating Empty Weight 22,518 kgs 31-Dec-17 Manufacturer s Empty Weight 22,422 kgs 13614:16 Winglets Installed [ ] Yes or [ ] No 11, :33 / 2180 AIRFRAME MAINTENANCE STATUS* Type of Check Specify Check: Last Accomplished Date Aircraft FH / FC Interval (Months / FH / FC) Date Next Due Aircraft FH / FC C Check 2C Chk 1-Aug :39 / ,000 FH 20/01/ FH Heavy Check 8Y 8 Years 25/08/ Y 10 Years 25/08/ Y 12 Years 25/08/2024 MAINTENACE PROGRAM Maintenance Program Provided by: Program Approved by Authority of: [ ] Customized or [ ] OEM [ ] FAA or [ ] EASA or [ ] Other: DGSAS OPERATIONAL STATUS ( Not locally Approved for ETOPS and Auto Land operations) LANDING GEAR Part Number NOSE L/H MAIN R/H MAIN Serial Number Gear TSN / CSN Date of Last Overhaul Gear TSN / CSN At Overhaul Date of Installation of Overhauled Gear Overhaul Interval (Years / Cycles) Time Remaining Until Overhaul (Years / Cycles) Landing Gear Brake Manufacturer Brake Type 13614:16 / :16 / :16 / MO or 30,000 FC 144 MO or 30,000 FC 144 MO or 30,000 FC 56 MO or FC 56 MO or FC 56 MO or FC MEGGIT AIRCRAFT BRAKING SYSTEMS CORPORATION [ ] Steel or [ ] Carbon

10 ENGINES* Manufacturer: Model: S/N: Engine TSN / CSN Completion Date of Last Shop Visit Engine TSN / CSN At Last Shop Visit Completion Date of Last Performance Restoration Shop Visit Engine TSN / CSN At Last Performance Restoration Shop Visit Test Cell EGT Margin At Performance Restoration Shop Visit Cycles Remaining to 1 st LLP Limiter Current Operating Thrust Engine Actual Annual Utilization (FH/FC) Excluding Off-Wing Time (if not currently installed on this aircraft) GE CF34-8E5A :16 / :00 / Mar May / / Mar May / / K 14K 2469:27 / :57 / 1258 AUXILIARY POWER UNIT* Manufacturer Part Number Serial Number Date of Manufacturer APU TSN / CSN At Hot Section Inspection (HSI) / Overhaul 31-Aug-12 APU TSN / CSN 13730:00 / Completion Date of Last Hot Section Inspection (HSI) / Overhaul HAMILTION SUNDSTRAND E HSC-E P 29-Jul / Cycles Remaining to 1 st LLP Limiter (if applicable) APU Annual Utilization (Hrs/Cycs) 1395:18 / 1138 APU Time Recorded by: [ ] APU Clock or [ ] A/C Time, Ratio: INTERIOR CONFIGURATION* Seat Type PAX Quantity Manufacturer Part Number In Seat Video? (Y/N) In Seat Power? (Y/N) Entertainme nt Controls (PCU)? (Y/N) Tourist Class Seats 60 C & D Zodiac First Class Seats Bus. Class Seats 11 C & D Zodiac /103/105 & /103/105 Y Y Y /102/103/104 & /102 Y Y Y Convertible Seats Total present capacity: 71

11 IN-FLIGHT ENTERTAINMENT SYSTEM Entertainment System Name: Manufacturer: Passenger Entertainment (Audio) Passenger Entertainment (Video) Audio / Video On Demand Moving Map / Airshow Overhead Video: THALES I4500 IFE SYSTEM THALES [ ] Yes or [ ] No PSU Mounted Y Aisle Mounted Projector GALLEYS AND LAVATORIES Quantity Manufacturer Location PART NUMBER Type Galleys 3 C & D Zodiac Lavatories 2 C & D Zodiac G G G FWD AFT [ ] Atlas or [ ] KSSU or [ ] Other Flush [ ] or Vacuum [ ] CARGO COMPARTMENT Cargo Loading System Installed: Type of System Installed: Smoke / Fire Detection System Installed: Fire Suppression System Installed: [ ] Yes or [ ] NO Note: The cargo compartment loading systems comprise the cargo compartment nets [ ] Powered or [ ] Non-Powered [ ] Yes or [ ] No [ ] Yes or [ ] No FUEL SYSTEM Fuel Capacity (US Gallons) #1 Auxiliary Tank [} #2 Auxiliary Tank [] Fuel Instrument/Calibration in: Approximately 3095 Gal [ ] Provisioned [ ] Installed [ ] Provisioned [ ] Installed [ ] Kilograms or [ ] Pounds Capacity (US Gallons): Capacity (US Gallons): AVIONICS Auto Flight - 22 MODULE,ELECTRONIC-FLIGHT CONTROLS,FCM THRUST CONTROL QUADRANT- WITH AUTOTHROTT Qty. Manufacturer Part Number 4 HONEYWELL ED35E KAISER ELECTROPRECIS Communications - 23 HF Transceiver VHF Transceiver SDU SATCOM Data Unit PRERECORDED ANNOUNCEMENT Tape Reproducer or DVD Player (Video Entertainment) HF COMM TRANSCEIVER SELCAL Printer Fixed ELT Flight Deck Door Camera System 1 HONEYWELL HONEYWELL C&D PBS HONEYWELL HONEYWELL ARTEX

12 Indicating and Recording 31 DVDR DIGITAL VOICE-DATA RECORDER AUXILIARY FLIGHT DATA ACQUISITION Navigation 34 ADC (Air Data Computer) INERTIAL REFERENCE UNIT Enhanced Ground Proximity Warning Computer Windshear System Installed? Weather Radar Transceiver INTEGRATED ELECTRONIC STANDBY TCAS Computer ATC Mode S Transponder DME Interrogator Marker Beacon Receiver VIDL MODULE - VOR, ILS, MKR BCN SOFTWARE RADAR ALTIMETER ADF GPS MODULE Control Display Unit 2 HONEYWELL SAGEM ED35E ROSEMOUNT AEROSPACE 2015G2H2H-9 2 HONEYWELL HG2100AB02 1 HONEYWELL If yes, [ ] Reactive or [ ] Predictive? 1 HONEYWELL THALES AVIONICS C16393AA02 1 HONEYWELL HONEYWELL HONEYWELL SENSOR SYSTEMS INC S HONEYWELL HONEYWELL HONEYWELL HONEYWELL HONEYWELL

13 AIRCRAFT SPECIFICATION SUMMARY GENERAL Registration Number Aircraft Model MSN Owner Date of Delivery Data as of Date Aircraft Total Hours Aircraft Total Cycles Annual Utilization (FC/FH) (FH/FC) WEIGHT AND STRUCTURAL DATA A4O-ED Max. Take Off Weight 40,370 kgs ERJ LR Max. Taxi Weight 40,530 kgs Max. Landing Weight 34,100 kgs OMAN AIR Max. Zero Fuel Weight 32,000 kgs 14-Nov-12 Operating Empty Weight 22,518 kgs 31-Dec-17 Manufacturer s Empty Weight 22,422 kgs 12909:05 Winglets Installed [ ] Yes or [ ] No 10, :22 / 2103 AIRFRAME MAINTENANCE STATUS* Type of Check Last Accomplished Next Due Specify Interval Check: Aircraft FH / Date (Months / FH / FC) Date Aircraft FH / FC FC C Check 1C Chk 26-Sep :03 FH / 8678 FC 6,000 FH 6/3/ :03 FH 8Y 8 Years 14/11/2020 Heavy Check 10Y 10 Years 14/11/ Y 12 Years 14/11/2024 MAINTENACE PROGRAM Maintenance Program Provided by: Program Approved by Authority of: [ ] Customized or [ ] OEM [ ] FAA or [ ] EASA or [ ] Other: DGSAS OPERATIONAL STATUS ( Not locally Approved for ETOPS and Auto Land operations) LANDING GEAR Part Number NOSE L/H MAIN R/H MAIN Serial Number Gear TSN / CSN Date of Last Overhaul Gear TSN / CSN At Overhaul Date of Installation of Overhauled Gear Overhaul Interval (Years / Cycles) Time Remaining Until Overhaul (Years / Cycles) Landing Gear Brake Manufacturer Brake Type 12909:05 / :05 / :05 / MO or 30,000 FC 144 MO or 30,000 FC 144 MO or 30,000 FC 59 MO or FC 59 MO or FC 59 MO or FC MEGGIT AIRCRAFT BRAKING SYSTEMS CORPORATION [ ] Steel or [ ] Carbon

14 ENGINES* Manufacturer: Model: S/N: Engine TSN / CSN Completion Date of Last Shop Visit Engine TSN / CSN At Last Shop Visit Completion Date of Last Performance Restoration Shop Visit Engine TSN / CSN At Last Performance Restoration Shop Visit Test Cell EGT Margin At Performance Restoration Shop Visit Cycles Remaining to 1 st LLP Limiter Current Operating Thrust Engine Actual Annual Utilization (FH/FC) Excluding Off-Wing Time (if not currently installed on this aircraft) GE CF34-8E5A :40 / :46 / Aug-17 1-Jun / / Aug-17 1-Jun / / K 14K 399:16 / :28 / 1467 AUXILIARY POWER UNIT* Manufacturer HAMILTION SUNDSTRAND Part Number E Serial Number HSC-E Date of Manufacturer 16-Dec-10 APU TSN / CSN 17547:06 / Completion Date of Last Hot Section Inspection 20-Oct-17 APU TSN / CSN At Hot Section Inspection (HSI) / / Cycles Remaining to 1 st LLP Limiter (if applicable) APU Annual Utilization (Hrs/Cycs) 447:18 / 383 APU Time Recorded by: [ ] APU Clock or [ ] A/C Time, Ratio: INTERIOR CONFIGURATION* Seat Type PAX Quantity Manufacturer Part Number In Seat Video? (Y/N) In Seat Power? (Y/N) Entertainme nt Controls (PCU)? (Y/N) Tourist Class Seats 60 C & D Zodiac First Class Seats Bus. Class Seats 11 C & D Zodiac /103/105 & /103/105 Y Y Y /102/103/104 & /102 Y Y Y Convertible Seats Total present capacity: 71

15 IN-FLIGHT ENTERTAINMENT SYSTEM Entertainment System Name: Manufacturer: Passenger Entertainment (Audio) Passenger Entertainment (Video) Audio / Video On Demand Moving Map / Airshow Overhead Video: THALES I4500 IFE SYSTEM THALES [ ] Yes or [ ] No PSU Mounted Y Aisle Mounted Projector GALLEYS AND LAVATORIES Quantity Manufacturer Location PART NUMBER Type Galleys 3 C & D Zodiac Lavatories 2 C & D Zodiac G G G FWD AFT [ ] Atlas or [ ] KSSU or [ ] Other Flush [ ] or Vacuum [ ] CARGO COMPARTMENT Cargo Loading System Installed: Type of System Installed: Smoke / Fire Detection System Installed: Fire Suppression System Installed: [ ] Yes or [ ] NO Note: The cargo compartment loading systems comprise the cargo compartment nets [ ] Powered or [ ] Non-Powered [ ] Yes or [ ] No [ ] Yes or [ ] No FUEL SYSTEM Fuel Capacity (US Gallons) #1 Auxiliary Tank [} #2 Auxiliary Tank [] Fuel Instrument/Calibration in: Approximately 3095 Gal [ ] Provisioned [ ] Installed [ ] Provisioned [ ] Installed [ ] Kilograms or [ ] Pounds Capacity (US Gallons): Capacity (US Gallons): AVIONICS Auto Flight - 22 MODULE,ELECTRONIC-FLIGHT CONTROLS,FCM THRUST CONTROL QUADRANT- WITH AUTOTHROTT Qty. Manufacturer Part Number 4 HONEYWELL ED35E KAISER ELECTROPRECIS Communications - 23 HF Transceiver VHF Transceiver SDU SATCOM Data Unit PRERECORDED ANNOUNCEMENT Tape Reproducer or DVD Player (Video Entertainment) HF COMM TRANSCEIVER SELCAL Printer Fixed ELT Flight Deck Door Camera System 1 HONEYWELL HONEYWELL C&D PBS HONEYWELL HONEYWELL ARTEX

16 Indicating and Recording 31 DVDR DIGITAL VOICE-DATA RECORDER AUXILIARY FLIGHT DATA ACQUISITION Navigation 34 ADC (Air Data Computer) INERTIAL REFERENCE UNIT Enhanced Ground Proximity Warning Computer Windshear System Installed? Weather Radar Transceiver INTEGRATED ELECTRONIC STANDBY TCAS Computer ATC Mode S Transponder DME Interrogator Marker Beacon Receiver VIDL MODULE - VOR, ILS, MKR BCN SOFTWARE RADAR ALTIMETER ADF GPS MODULE Control Display Unit 2 HONEYWELL SAGEM ED35E ROSEMOUNT AEROSPACE 2015G2H2H-9 2 HONEYWELL HG2100AB02 1 HONEYWELL If yes, [ ] Reactive or [ ] Predictive? 1 HONEYWELL THALES AVIONICS C16393AA02 1 HONEYWELL HONEYWELL HONEYWELL SENSOR SYSTEMS INC S HONEYWELL HONEYWELL HONEYWELL HONEYWELL HONEYWELL