Multifunction Printer Pinouts Power R (115 VAC) / N (GND)Backlight <E (5 VDC) / M (GND) AIRINC 429 ConnectionsFMGC 1 IN V, WCFDUI IN <H,<IFMGC 2 IN A,BEVM IN <J, XAIDS DATA IN C,DDATA LINK T,U ReferenceAircraft Schematic Manual 31-35-01 Continue reading
VOR/DME DDRMI Pinouts Heading connects to a Hi Speed ARINC 429 output VOR1/DME1 and VOR2/DME2 connect to a Lo Speed ARINC429 output Power (115 VAC) CGround DIntegral Lighting (5 VDC) A/BHDG R *, S **HDG Alternate U *,V **VOR1 <B *, <C **DME1 <G *, <H **VOR2 <E +, <F ++ DME2 <I +, <J … Continue reading
The ATC has 2 control data, 1 or 2. For the purpose of the pinouts only the first control data has been used (the second one is redundant for a simulator). All pinouts are mapped to the J1 plug. 115 VAC is required for operation (a static inverter is used for our purpose to convert … Continue reading
Weather Radar, Collins Type WCP-701 PN 622-5129-020 pinouts Connector J1 Power +28 VDC M/L (GND) Integral Backlight +5 VDC P/e On/Off V/G (pinouts are used for a voltage self test but can be substituted for joystick button functionality)Predictive Windshear Auto-On/Disable g ARINC429 (low speed) <h connect to ARINC429 board INPUT A <j connect to ARINC429 … Continue reading
11VU Throttle Quadrant 2139VC Backlight Trim E (+5 VDC) / F, G (Gnd) Backlight Gravity Gear extension A (+5 VDC) / B (Gnd) Backlight Gravity Gear extension C (+5 VDC) / D (Gnd) 2145VC Instinctive Disconnect Autothrust (L lever) A/C 2146VC Instinctive Disconnect Autotrust (R lever) A/D 8KS1 (Throttle Lever, Engine 1) Plug A Potentiometer … Continue reading
77The left and right brake pedals are connected mechanically to the Brake Transmitter transducer on the FO rudder pedal mechanism. Pinouts Right Brake G/M(wiper)/U Left Brake Y/C(wiper)/H Reference ASM 32-42-01 Continue reading
Glare Panel Pinouts Continue reading
