Bell Cranks - Page 35 of 59

1465 part numbers
209-001-107-101 NSN 1680-01-079-1212
  • flight safety critical aircraft part special features
  • aluminum alloy material
70400-02217-041 NSN 1680-01-079-6380
128CM12000-13 NSN 1680-01-081-8044
  • cadmium surface treatment
128CM12000-11 NSN 1680-01-082-7955
  • 2.541 inches bore length
  • 4.954 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • steel material
  • raised face pivot hole, clevis both ends style designator
70400-02209-042 NSN 1680-01-082-9221
128CM12001-9 NSN 1680-01-085-0442
  • between 1.374 inches and 1.376 inches bore diameter
  • 4.140 inches bore length
  • steel material
  • cadmium surface treatment
128CM12004-10 NSN 1680-01-087-1540
  • 1.687 inches bore diameter
  • steel material
  • cadmium and zinc surface treatment
128L10034-6 NSN 1680-01-089-4042 Cross Reference: 128L10034-4
  • fulcrum bore and fulcrum shaft features provided
1128L40501-5 NSN 1680-01-089-4044 Cross Reference: 1128L40501-1, 1128L40501-3, 1128L40501-5/-6
  • fulcrum shaft features provided
1128L40501-6 NSN 1680-01-089-4046 Cross Reference: 1128L40501-2, 1128L40501-4
  • fulcrum shaft features provided
70400-08101-044 NSN 1680-01-090-2048
  • between 1.790 inches and 1.820 inches bore diameter
  • 4.190 inches bore length
  • 7.940 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • cadmium surface treatment
  • clevis ends twisted, other arm offset style designator
128L10034-5 NSN 1680-01-090-9311 Cross Reference: 128L10034-3
  • fulcrum bore and fulcrum shaft features provided
128CM12004-9 NSN 1680-01-091-2437
  • 1.687 inches bore diameter
  • steel material
70400-01412-042 NSN 1680-01-091-8224
  • 5.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
128CM12001-10 NSN 1680-01-092-7730
  • between 1.374 inches and 1.376 inches bore diameter
  • 4.140 inches bore length
  • steel material
  • cadmium surface treatment
70400-02501-045 NSN 1680-01-092-8101
  • blackhawk uh-60 end application
70400-02503-044 NSN 1680-01-093-2894
  • blackhawk uh-60 airframe end application
128CM12003-5 NSN 1680-01-099-8538
70250-13110-042 NSN 1680-01-101-9707
  • uh-60 blackhawk airframe/aux power unit end application
414C1165-2 NSN 1680-01-105-1731
  • ch-47 airframe unit end application
414C3310-2 NSN 1680-01-105-1732
414C1165-1 NSN 1680-01-105-5787
  • ch-47, rotary wing aircraft end application
414C1160-2 NSN 1680-01-105-5788
414C1131 NSN 1680-01-105-8792 Cross Reference: 414C1131-1
  • ch-47, rotary wing aircraft end application
414C1230-1 NSN 1680-01-105-8794