Bell Cranks - Page 37 of 59

1465 part numbers
7-311517012 NSN 1680-01-155-6611
  • 0.750 inches bore length
  • 3.497 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
  • clevis ends style designator
7-311517039 NSN 1680-01-155-6612
70400-02209-044 NSN 1680-01-158-6085
  • aluminum alloy material
70400-02217-042 NSN 1680-01-158-6087
  • aluminum alloy material
7-311517002 NSN 1680-01-158-7161
70400-08101-046 NSN 1680-01-158-9652
  • uh-60, rotary wing aircraft end application
7-311511127 NSN 1680-01-160-1291
7-311511125 NSN 1680-01-161-1205
406-001-502-101 NSN 1680-01-164-3962
406-001-503-101 NSN 1680-01-164-3963
406-001-503-102 NSN 1680-01-164-3964
406-001-336-105 NSN 1680-01-164-8431 Cross Reference: 406-001-323-101
  • oh-58d kiowa warrior helicopter end application
7-311511117 NSN 1680-01-165-7006
7-311517052 NSN 1680-01-171-9248
7-318000174 NSN 1680-01-174-5836
  • electro optical augmentation system end application
7-311518006 NSN 1680-01-178-5056
406-001-504-105 NSN 1680-01-181-4088
  • target acquisition designation sight (tads) end application
406-001-505-105 NSN 1680-01-181-4089 Cross Reference: 406-001-505-101
  • feat criticality code justification
  • flight safety critical aircraft part special features
406-001-505-106 NSN 1680-01-181-4090 Cross Reference: 406-001-505-102
7-311518020 NSN 1680-01-182-9032
1881B354-01 NSN 1680-01-183-7316
  • aircraft b1b end application
  • steel material
  • main landing gear, uplock fsc application data
75A326117-1001 NSN 1680-01-184-9993
  • aluminum alloy material
  • mounting assembly, rear engine fsc application data
206-001-702-5 NSN 1680-01-185-3203
406-001-704-101 NSN 1680-01-185-3204
406-001-707-101 NSN 1680-01-185-3205