Bell Cranks - Page 46 of 59

1465 part numbers
145C2510-2 NSN 1680-01-449-5944
  • used on the chinook helicopter special features
145C3122-3 NSN 1680-01-449-5947
  • used on the chinook helicopter special features
114C3324-7 NSN 1680-01-449-6750
  • used on the chinook helicopter special features
160D321030-4 NSN 1680-01-449-7602
  • a-10a aircraft end application
145C3516-2 NSN 1680-01-449-9978
  • ch-47d chinook helicopter end application
69-1526-9 NSN 1680-01-450-0745
  • e-3 aircraft special features
  • c-17a acft end application
  • c/o 1ea crank, 4ea fittings, 10ea bushings special features
414E5015-35 NSN 1680-01-453-0934
  • ch-47d chinook helicopter end application
  • c-17a acft end application
  • c/o 1ea crank, 4ea fittings, 10 ea bushings special features
  • steel material
74A656010-1002 NSN 1680-01-454-5028
  • f18 e/f end application
  • agav criticality code justification
74A656010-1005 NSN 1680-01-454-5030
  • f18 e/f end application
  • agav criticality code justification
74A656010-1001 NSN 1680-01-454-5031
  • f18 e/f end application
  • agav criticality code justification
74A675205-1007 NSN 1680-01-454-6714 Cross Reference: 74A675205-1005
74A400580-1003 NSN 1680-01-455-3607
  • preprovisioning support navicp is poe end application
74A400580-1004 NSN 1680-01-455-3610
  • preprovisioning support navicp is poe end application
74A400701-1003 NSN 1680-01-455-3613
  • preprovisioning support navicp is poe end application
74A430953-1001 NSN 1680-01-455-3652
  • preprovisioning support navicp is poe end application
414E5015-23 Bellcrank NSN 1680-01-457-1487
  • raf mk2 chinook aircraft, seat adjustment end application
  • aluminum material
  • qq-a-250/12 federal specification single material response material specification
104658-1 NSN 1680-01-458-0017
  • used on merlin helicopter end application
17P3A1777-501 NSN 1680-01-459-6132
  • aircraft c-17a end application
17P1A4486-507 NSN 1680-01-459-6135
  • aircraft c-17a end application
17P1A4481-509 NSN 1680-01-459-6143
  • aircraft c-17a end application
17P1A4469-513 NSN 1680-01-459-6145
  • aircraft c-17a end application
74A656010-1003 NSN 1680-01-461-7282
  • f18 e/f end application
  • agav criticality code justification
74A675205-1008 NSN 1680-01-461-7285 Cross Reference: 74A675205-1006