Bell Cranks - Page 44 of 59

1465 part numbers
3-73141-15 NSN 1680-01-419-0836
  • f-5 acft end application
  • aluminum alloy material
3-73327-1-5 NSN 1680-01-419-0837
  • f-5 acft end application
  • 2.750 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • magnesium material
6-73192-11 NSN 1680-01-419-0859
  • f-5 acft end application
65-13742-7 NSN 1680-01-420-0204
  • e-3a awacs aircraft end application
2-73881-11 Students And Instructors Manufacturers Suggested Name - Crank - Pedal Brake Operating NSN 1680-01-420-9534
  • 0.540 inches 1st end slot width
  • t-38 aircraft end application
  • 2.580 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
2-73881-12 Students And Instructors Manufacturers Suggested Name - Crank - Pedal Operating NSN 1680-01-421-0983
  • 0.540 inches 1st end slot width
  • t-38 aircraft end application
  • 2.580 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
002-410039-3 NSN 1680-01-421-1450
  • beechcraft bonanza end application
002-410039-7 NSN 1680-01-421-1451
  • beechcraft bonanza end application
17P1F1123-501 NSN 1680-01-421-7846
  • aircraft c-17a end application
  • bell crank special features
17P1F6064-1 NSN 1680-01-421-7847
  • aircraft c-17a end application
  • bell crank special features
17P1F8449-1 NSN 1680-01-421-7848
  • aircraft c-17a end application
  • bell crank special features
17P1F6206-501 NSN 1680-01-421-7850
  • aircraft c-17a end application
  • bellcrank special features
L5226266-001 Driver - Nonlinear Pitch Control Manufacturers Suggested Name - Bell Crank NSN 1680-01-422-1291
  • 1.885 inches 1st end slot width
  • 2.375 inches bore length
  • b-1b aircraft end application
  • 3.006 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
17P1F1123-1 NSN 1680-01-422-3384
  • aircraft c-17a end application
  • bell crank special features
17P1F6023-1 NSN 1680-01-422-3403
  • aircraft c-17a end application
  • bell, crank special features
17P1F6232-1 NSN 1680-01-422-6127
  • weapons system is c-17a aircraft, airlifter end application
74A460601-1005 NSN 1680-01-424-6222 Cross Reference: 10153920
  • f/a-18 hornet end application
  • pawl assembly-door and uplock mech, nlg special features
17P2C1552-501 Mlg Alternate Release Manufacturers Suggested Name - Crank NSN 1680-01-430-0440
  • c-17 aircraft end application
  • 6.500 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum material
17P2C1552-2 Alternate Release Mlg Manufacturers Suggested Name - Crank NSN 1680-01-430-0443
  • c-17 aircraft end application
  • 6.500 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
17P2C1552-1 Mlg Alternate Release Crank NSN 1680-01-430-0444
  • c-17 aircraft end application
  • 6.500 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
2134A-19 NSN 1680-01-431-9031 Cross Reference: ZC8-49-001-11-1
  • pacer dawn end application
17P2C1552-502 Mlg Alternate Release Crank NSN 1680-01-432-2887
  • c-17 aircraft end application
  • 1.722 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum material
17P6W8214-503 Lh No. 2 Support Spoiler Actuator Crank Assy NSN 1680-01-434-7392
  • c-17a acft end application
  • c/o 1ea crank, 4ea fittings, 10ea bushings special features
  • steel material
373895-2 NSN 1680-01-434-8400
  • c130j hercules acft end application
  • used on the locking ramp special features
373895-7 NSN 1680-01-434-8403
  • c130j hercules acft end application
  • used on the locking ramp special features