Boeing MD 87

Technische Daten

Avionik & Ausstattung

• Vertical Gyro Rockwell Collins 2587335-113
• Digital Flight Guidance Computer Honeywell 403-4241-974
• Flight Guidance Control Panel Honeywell 403-4242-974
• VHF Com Transceiver Rockwell Collins 822-1045-401 618M-5
• Radio Management Panel Gables Engineering G7406-12
• HF Com Transceiver Rockwell Collins 622-3371-001 628T-1
• Interphone Amplifier Gables Engineering G610-11-700
• Passenger Address Amplifier Rockwell Collins 622-4096-001 346D-2B
• Cockpit Voice Recorder – Magnetic Tape Fairchild 93A100-80 A-100A
• Digital Flight Data Recorder – Solid St. Honeywell 980-4700-003
• Digital Flight Data Acquisition Unit Hamilton Sundstrand ED7425951-9
• Stall Warning Computer Honeywell 965-0449-002
• EFIS Symbol Generator Honeywell 405-5900-906
• EFIS Display Control Unit Honeywell 405-6510-903
• EFIS Mode Selector Panel Honeywell 405-6512-901
• Mach Airspeed Indicator Honeywell 259-4466-905
• Air Data Computer Honeywell HG280D80
• Directional Gyro Rockwell Collins 2588302-4
• Standby Altimeter Smiths Industries WL1604AM2
• Standby Horizon Indicator Thales Avionics 705-15V1
• Standby Airspeed/Altimeter Indicator Smiths Industries WL101AMS-1 100AMS
• Enhanced Ground Proximity Warning Computer Honeywell 965-0976-003 -212-212
• TCAS II Computer – Change 7.0 Honeywell 066-50000-2220 TPA-81A
• GNSSU (Global Navigation System Sensor Unit) Honeywell HG2021GM01
• Weather Radar Transceiver Honeywell 2041217-0413 RTA-4A
• Radar and TCAS Indicator Allied Signal 2041222-2402
• Radio Magnetic Indicator Honeywell 2594661-903
• ADF Receiver Honeywell 2041168-7501 DFA-75A
• Marker Beacon Receiver Rockwell Collins 2087821-2811 51Z-4
• VOR/ILS Nav Receiver – Incl FM imm. Rockwell Collins 403-4240-906 RNA-34A
• DME Interrogator Rockwell Collins 822-0329-020 Series 900
• VOR/ILS Nav Receiver – FM imm Rockwell Collins 822-0761-101 51RV-5B
• ATC Transponder – Mode S – ELS & EHS Compliant Honeywell 066-01127-1602 TRA-67A

Beschreibung

If BOEING – Mc Donnell Douglas MD 87