For Sale 1990 MD-87 Serial Number VIP Configured

Transcription

1 For Sale 1990 MD-87 Serial Number VIP Configured

2 Contact Quentin Brasie, ACI Aviation Consulting Aircraft Manufacturer McDonnell Douglas (Boeing) Aircraft Model DC9-87 (MD-87) Serial Number Year of Manufacture 1990 Country of Registration USA Registration Number N167AS Engine Type JT8D-217C Total Aircraft Hours 34, Total Aircraft Cycles 26,880 Location of Aircraft Rockford, IL This aircraft is subject to prior sale, commitment or withdraw from the market without prior notice. No warranty or guarantee is made or implied regarding the accuracy of the data presented herein and is subject to independent verification 2

3 Contact Quentin Brasie, ACI Aviation Consulting Engine Data Current Location Serial Number Total Time / Total Cycles Date and TSLSV Limit Item Cycles Remaining Left Engine #1 Position , Hrs. 34,439 Cyc. 6/13/ Hrs 3 Cyc. C9 Disk 3,626 Cycles 33.8 % Right Engine #2 Position , Hrs. 33,072 Cyc. 2/17/ Hrs 3 Cyc. C1 Disk Next disks in compressor and turbine sections 1,959 Cycles Next 5,245 Cycles 35.5% Landing Gear Data Position Serial Number / Part Number Overhaul Intervals Remaining Percent Remaining Nose Gear Assembly CP ,000 Cycles or 120 Months 8,118 Cycles Due - Mo 40.6 % 0 % Left Main Gear Assembly S ,000 Cycles or 120 Months 12,024 Cycles Due - Mo % 0 % Right Main Gear Assembly S ,000 Cycles or 120 Months 12,024 Cycles Due - Mo. 60.1% 0 % This aircraft is subject to prior sale, commitment or withdraw from the market without prior notice. No warranty or guarantee is made or implied regarding the accuracy of the data presented herein and is subject to independent verification 3

4 Corporate Configured Interior offering stylish accommodations for 19 passengers. Private work-stations, three lavatories, two galleys and a private bedroom suite. This is luxury. This aircraft is subject to prior sale, commitment or withdraw from the market without prior notice. No warranty or guarantee is made or implied regarding the accuracy of the data presented herein and is subject to independent verification 4

5 Avionics Contact Quentin Brasie, Nomenclature Part Number Serial Number Manufacturer Central Aural Warning System HO5A Unknown Marker Receiver Bendix VHF Comm 1 RTA-83A Allied Signal VHF Comm 2 RTA-83A Allied Signal ADF 700 # Collins ADF 700 # Collins TCAS Honeywell VHF Nav Bendix VHF Nav Bendix Radio Altimeter Collins Radio Altimeter Collins DME Collins DME Collins HF Collins HF Collins Mark VII EGPWS Allied Signal Digital Flight Guidance Computer Honeywell Digital Flight Guidance Computer Honeywell Weather Radar Unknown FMU CMA Canadian Marconi Co ADC #1 HG280D Honeywell ADC #2 HG280D Honeywell Flight Data Acquisition Unit E Hamilton Std EFIS SYSTEM GEN Honeywell EFIS SYSTEM GEN Honeywell Stall Warning Computer Allied Signal Stall Warning Computer Allied Signal EQAR Recorder Unknown Nomenclature Part Number Serial Number Manufacturer AHRU # Unknown AHRU # Unknown AHRU # Unknown COMPUTER HUD Sundstrand WEATHER RADAR TRANSC ` Unknown TRANSPONDER Honeywell TCAS G Unknown CDU MKIII Unknown CDU MKIII Unknown VHF COMM G Unknown This aircraft is subject to prior sale, commitment or withdraw from the market without prior notice. No warranty or guarantee is made or implied regarding the accuracy of the data presented herein and is subject to independent verification 5

6 Contact Quentin Brasie, ACI Aviation Consulting The fine print This aircraft has not been recently operated. There is maintenance due on this aircraft. The purchase of this aircraft will be based on an As Is / Where Is condition only. This aircraft is subject to prior sale, commitment or withdraw from the market without prior notice. No warranty or guarantee is made or implied regarding the accuracy of the data presented herein and is subject to independent verification. The aircraft is not currently airworthy. This aircraft is subject to prior sale, commitment or withdraw from the market without prior notice. No warranty or guarantee is made or implied regarding the accuracy of the data presented herein and is subject to independent verification 6