Collision Avoidance Computer
Item Name Code (INC) 49761
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A computer specifically designed to continuously monitor dynamic flight data, combine it with predetermined flight criteria, and to issue aural and visual warnings of deviations from safe flight conditions.
Additional Information for Collision Avoidance Computer
A Collision Avoidance Computer is a device used in aviation to help prevent collisions between aircraft. It is part of the Flight Instruments supply class, which includes instruments used for navigation, communication, and monitoring during flight. The Flight Instruments supply class falls under the larger supply group called Instruments And Laboratory Equipment, which encompasses a wide range of instruments used in various industries, including aviation, scientific research, and laboratory testing.
Related Item Names for INC 49761 Collision Avoidance Computer
Airspeed-Altitude Computer Present Position Computer Pressure Altimeter Venturi Tube Attitude Indicator Turn And Slip Indicator Pitot Tube Pitot-Static Tube Static Tube Mach And True Air Speed Indicator Vertical Velocity Indicator Machmeter Air Speed Computer Mechanical Accelerometer Aircraft Inclinometer Aircraft Instruments Manifold Position Transmitter Position Indicator Recorder Subassembly Recorder Group Altitude Computer Azimuth-Elevation Deviation Indicator Control Surfaces Trim Indicator Data Display Group Course Indicator Linear Electrical Accelerometer Optical Element Cell Dummy Static Tube Indicator Housing Angle Of Attack Transmitter Flight Director Computer Air Data Computer Mach Number Computer Magnetic Recording Tape Reel Airspeed And Direction Indicator Computer Subassembly Head-Up Display Unit Air Speed Indicator Angle Indicator Gyroscopic Heading Indicator Airport Runway Instrument Landing Indicator Instruments And Laboratory Equipment Modification Kit Wrist Instrument Strap Flight Data Recorder Collision Avoidance Computer Data Acquisition Unit Head-Up Display Symbol Generator Head-Up Display Monitor Pressure Altimeter Subassembly Automatic Pressure Standby Servo Controlled Altimeter Subassembly Preset Command Information Servo Controlled Altimeter Subassembly Air Speed Indicator Subassembly Flight Instruments Angle Indicator Subassembly Attitude Indicator Subassembly Flight Instruments Course Indicator Subassembly Gyroscopic Heading Indicator Subassembly Mach And True Air Speed Indicator Subassembly Flight Instruments Position Indicator Subassembly Control Surfaces Trim Indicator Subassembly Turn And Slip Indicator Subassembly Vertical Velocity Indicator Subassembly Flight Data Recorder Interface Subassembly Flight Data Recorder Memory Unit Electronic Air Inlet Controller Flight Information Processor Fuel Management Computer Flight Information Display Unit Fuel Management Panel Fuel Savings Advisory Computer Ground Speed Indicator Control-Display Unit Static Tube To Case Section Adapter Automatic Pressure Standby Servo Controlled Altimeter Preset Command Information Servo Controlled Altimeter Stabilization Data Indicator Static Tube Protector Static Tube Subassembly Static Tube Base Static Tube Mast Static Tube Probe Static Tube Vane Assembly Multiple Aircraft Parameters Display Computer Multiple Aircraft Parameters Display Attitude And Heading Reference Unit Aircraft Pitot Static Drain Bottle Special Purpose Computer System Special Purpose Computer Autopilot Control Unit Impact Pressure Transducer
NATO Stock Numbers with Item Name 49761 Collision Avoidance Computer Page 1 of 1
- 9005000-30903
- RNCC: 3 | RNVC: 1 | DAC: 5
- 9005000-30901
- RNCC: 3 | RNVC: 1 | DAC: D
- 7517900-55004
- RNCC: 5 | RNVC: 2 | DAC: 5
- 066-01178-2101
- RNCC: 3 | RNVC: 2 | DAC: 4
- 066-01171-2304
- RNCC: 3 | RNVC: 2 | DAC: 4
- 7517900-10020
- RNCC: 3 | RNVC: 2 | DAC: 4
- 7517900-55020
- RNCC: 3 | RNVC: 2 | DAC: 4
- 7517900-20003
- RNCC: 3 | RNVC: 2 | DAC: B
- 7517900-71007
- RNCC: 3 | RNVC: 2 | DAC: 3
- 940-0351-010
- RNCC: 3 | RNVC: 2 | DAC: 4
- 5-ZLX-MBX-IGC
- RNCC: 3 | RNVC: 2 | DAC: 1
- 7517900-71007
- RNCC: 3 | RNVC: 2 | DAC: 4