Quadrant Control Assemblies - Page 10 of 14

327 part numbers
269A7316-013 Lateral Control Assy NSN 1680-01-479-0407 Cross Reference: 269A7316-9
  • 269 series helicopter end application
16F3415-817 NSN 1680-01-481-6879 Cross Reference: 16F3415
16F3415-821 NSN 1680-01-481-6882 Cross Reference: 16F3415
16F3415-823 NSN 1680-01-481-6904 Cross Reference: 16F3415
C99F31235-1 Brake Assembly NSN 1680-01-484-2254
  • horizontal stabilizer trim aircraft location
  • e-8, jstars aircraft mission design series
3F1202-5 Throttle Quadrant NSN 1680-01-487-2088 Cross Reference: 5VV50060-111
  • f-22 aircraft mission design series
70070-30258-047 NSN 1680-01-488-9744 Cross Reference: 70070-30258
17P1F2020-513 NSN 1680-01-492-3893
17P1F2020-515 NSN 1680-01-492-3894
269A7363-2 Pedal Arm Rh NSN 1680-01-492-9301
269A7363-1 Pedal Arm Lh NSN 1680-01-492-9302
75G802075-1015 NSN 1680-01-495-7700
  • harrier end application
75G802075-1017 NSN 1680-01-495-7702
  • harrier end application
75A603513-1013 NSN 1680-01-496-7953 Cross Reference: 75A603513
75G802075-1013 NSN 1680-01-496-8217 Cross Reference: 75R802009
75A094260-1003 NSN 1680-01-501-0983 Cross Reference: 75A094260
75A094260-1001 NSN 1680-01-502-2978
  • aircraft, harrier av-8b end application
17P1F2020-517 NSN 1680-01-513-2786
697900-7 NSN 1680-01-520-9975 Cross Reference: 43116-011
  • hercules aircraft end application
75G802275-1011 NSN 1680-01-521-3227
  • av-8b aircraft mission design series
17P1F6033-1 Rudder Pedals Stature Adjust Support Assy NSN 1680-01-523-3605
  • stick and rudder pedal control aircraft location
  • c-17a aircraft aircraft mission design series
  • aluminum alloy material
  • t.o. 1c-17a-4-47 f.18 i.88 reference data and literature
7141029-500 NSN 1680-01-526-3453
  • cockpit aircraft location
  • t38-c cockpit aircraft mission design series
  • throttle quadrant, students functional description
3-50813-500 NSN 1680-01-526-4614
  • cockpit aircraft location
  • t-38c aircraft aircraft mission design series
  • throttle quadrant, instructors functional description
3F1209H Qu (inavy) Control Assembly NSN 1680-01-529-7744
  • fighter aircraft-first (f18 e/f) end application
  • agav criticality code justification
123AMM42158-611 Inavy: Quadrant Assembly NSN 1680-01-530-0935 Cross Reference: 123AMM42158
  • 8.000 inches overall length
  • 1.562 inches material thickness
  • c-2a aircraft only from 20 on end application
  • mid section entrance door-fail safe aircraft location
  • c-2a only aircraft mission design series