ATTITUDE GYRO AND IND. SYSTEM
The gyroscopic unit which supplies attitude information to the necessary systems; for instance, vertical reference outputs for use as roll and pitch data to the autopilot computer. Includes the instruments operating by the gyroscopic principle, driven by air flow or an electric motor. Typical parts are vertical gyro and the gyro horizon.
3421
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Other Navigation Components
3400
NAVIGATION SYSTEM
3410
FLIGHT ENVIRONMENT DATA
3411
PITOT/STATIC SYSTEM
3412
OUTSIDE AIR TEMP. IND./SENSOR
3413
RATE OF CLIMB INDICATOR
3414
AIRSPEED/MACH INDICATOR
3415
HIGH SPEED WARNING
3416
ALTIMETER, BAROMETRIC/ENCODER
3417
AIR DATA COMPUTER
3418
STALL WARNING SYSTEM
3420
ATTITUDE AND DIRECTION DATA SYSTEM
3422
DIRECTIONAL GYRO AND IND. SYSTEM
3423
MAGNETIC COMPASS
3424
TURN AND BANK/RATE OF TURN INDICATOR
3425
INTEGRATED FLT. DIRECTOR SYSTEM
3430
LANDING AND TAXI AIDS
3431
LOCALIZER/VOR SYSTEM
3432
GLIDE SLOPE SYSTEM
3433
MICROWAVE LANDING SYSTEM
3434
MARKER BEACON SYSTEM
3435
HEADS UP DISPLAY SYSTEM
3436
WIND SHEAR DETECTION SYSTEM
3440
INDEPENDENT POS. DETERMINING SYSTEM
3441
INERTIAL GUIDANCE SYSTEM
3442
WEATHER RADAR SYSTEM
3443
DOPPLER SYSTEM
3444
GROUND PROXIMITY SYSTEM
3445
AIR COLLISION AVOIDANCE SYSTEM (TCAS)
3446
NON RADAR WEATHER SYSTEM
3450
DEPENDENT POSITION DETERMINING SYS
3451
DME/TACAN SYSTEM
3452
ATC TRANSPONDER SYSTEM
3453
LORAN SYSTEM
3454
VOR SYSTEM
3455
ADF SYSTEM
3456
OMEGA NAVIGATION SYSTEM
3457
GLOBAL POSITIONING SYSTEM
3460
FLT MANAGE. COMPUTING HARDWARE SYS
3461
FLT MANAGE. COMPUTING SOFTWARE SYS
3497
NAVIGATION SYSTEM WIRING