Bell Cranks - Page 45 of 59

1465 part numbers
17P3A1782-501 NSN 1680-01-436-7686
  • c-5a aircraft special features
75A657063-1005 NSN 1680-01-437-0378
  • av-8 aircraft end application
  • bobweight-bellcrank-tail special features
F20G8021010-501 NSN 1680-01-437-3200
  • hu-25 coast guard aircraft end application
  • aluminum alloy material
17P3A1777-503 NSN 1680-01-437-7336
  • c-17a aircraft special features
339003-7 NSN 1680-01-437-7693
  • hercules c130j, fixed wing acft end application
374439-2 NSN 1680-01-437-7694
  • hercules c130j, fixed wing acft end application
374440-3 NSN 1680-01-437-7695
  • hercules c130j, fixed wing acft end application
374440-5 NSN 1680-01-437-7696
  • hercules c130j, fixed wing acft end application
75A610004-2001 NSN 1680-01-437-7711
75A35307-2003 NSN 1680-01-437-8775
  • av-8 aircraft end application
  • material 7050-t7451, mms-1420 plate special features
  • steel material
352940-11 NSN 1680-01-438-8178
  • 11.820 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
F395-1052-1 NSN 1680-01-439-1340
  • preprovisioning support navicp is poe end application
145C3231-2 NSN 1680-01-440-2819
L3300297-001 Mlg Door Lock Assy Manufacturers Suggested Name - Bellcrank NSN 1680-01-441-8175
  • b-1b aircraft end application
  • stainless steel material
17P2N3026-501 NSN 1680-01-442-1011
  • bell crank special features
68A630003-1007 NSN 1680-01-443-2965
  • f-15 aircraft end application
  • location - bellcrank - stabilator mixer, input special features
  • phosphate surface treatment
68A630000-1005 NSN 1680-01-443-2966
  • f-15 aircraft end application
  • phosphate surface treatment
5128T23G01 NSN 1680-01-443-4230 Cross Reference: 5111T35G01
  • preprovisioning support navicp is poe end application
5128T27P01 NSN 1680-01-443-4363 Cross Reference: 5111T42P01
  • preprovisioning support navicp is poe end application
5114T75G01 NSN 1680-01-443-5854
  • preprovisioning support navicp is poe end application
L3400192-021 Submitted Name - Bellcrank Assy NSN 1680-01-444-5132
  • b-1b aircraft end application
  • bearing features provided
  • 8.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
  • mil-a-22771 military specification single material response material specification
A51C31595-1 NSN 1680-01-446-0361
  • f-14a/b aircraft end application
  • aluminum alloy material
123CM11000-503 NSN 1680-01-448-4108 Cross Reference: 123CM11000
  • e-2c acft end application
414C1160-4 NSN 1680-01-449-3359
  • used on the chinook helicopter special features
145C3110-3 NSN 1680-01-449-5942
  • used on the chinook helicopter special features