| Model: | Fokker 100 |
Registration: | I-ALPK | Reference number: | RJ_PK10 | Year: | 1987 | Engine: | Rolls Royce TAY 620-15
ESN #1: 17008
ESN #2: 17090 | TSN Engine: | #1: 36.724 hrs - 34.694 cyc
#2: 26.417 hrs - 22.410 cyc | Avionics: | Flap Control Data Unit (Fokker )
Maintenance Control Computer (Rockwell MCC-1000)
Instrument Landing system (Bendix/King RIA35A)
Digital Air Data Computer (Honeywell )
Flight Control Computer (Collins FCC-1000)
Digital Air Data Computer (Honeywell )
Flight Control Computer (Collins FCC-1000)
Flight Augmentation Computer (Collins FAC-1000)
Passenger Address (Collins PAU-700)
Inertial Reference Unit 1 (Honeywell HG1050 IRU)
Inertial Reference Unit 2 (Honeywell HG1050 IRU)
Inertial Reference Unit 3 (Honeywell HG1050 IRU)
Instrument Landing system (Bendix/King RIA35A)
Weather Radar (Bendix / King RTA-4A)
Automatic Direction Finder (Collins ADF-700)
Audio Management Unit (Gables )
VHF Omni Range (Bendix / King RVA 36A)
Enhance Ground Proximity Warning (Sundstrand Mk-V)
Distance Measuring Equipment (Collins DME-700)
Air Traffic Control (Collins TPR-900)
Skid Control Box (ABS, Local )
Air Traffic Control (Collins TPR-900)
Distance Measuring Equipment (Collins DME-700)
VHF Omni Range (Collins RVA 36A)
Flight Control Computer (Collins FCC-1000)
Emergency Power Unit (ACME-URDC AMPS500)
Very High Freq Com (Collins VHF-700B)
Flight Management Computer (Honeywell)
Flight Data Acquisition Unit (Teledyne 70-701W)
Flight Management Computer (Honeywell)
Instrument Landing system (Bendix/King RIA35A)
Very High Freq Com (Collins VHF-700B)
Selcal (TEAM)
Automatic Direction Finder (Collins ADF700)
Stall Warning Computer (Fokker )
Flight Warning Computer (Grimes)
Cabin Pressure Controller 1 (Garret Airl.Serv)
Cabin Pressure Controller 2 (Garret Airl.Serv)
Digital Aids Recorder (Penny & Giles) | Interior: | 98 pax config. | Exterior: | Overall white paint with blue tail. | Status: | RVSM, CAT III B and B-RNAV. JAR-OPS compliant.
Noise cert. Stage 3. | Asking price: | DEAL PENDING |
