Bell Cranks

1465 part numbers
114C1131-6 NSN 1680-00-004-2420
  • 0.5015 inches bore diameter
  • 2.719 inches bore length
  • fulcrum bore features provided
  • fsc app data: control stick, aircraft special features
  • magnesium material
A51M42508-11 NSN 1680-00-005-0125
  • between 0.500 inches and 0.501 inches bore diameter
  • between 1.457 inches and 1.463 inches bore length
  • f-14 aircraft end application
  • titanium material
  • raised face pivot hole, clevis both ends style designator
53G970601-10 NSN 1680-00-005-3724
  • 0.4395 inches bore diameter
  • 1.400 inches bore length
  • f-4 aircraft end application
  • titanium material
53G970601-5 NSN 1680-00-005-3726
  • 0.4395 inches bore diameter
  • 1.500 inches bore length
  • f-4 aircraft end application
  • titanium material
  • ams4928 assn standard single material response material specification
53G970601-9 NSN 1680-00-005-3727
  • 0.4395 inches bore diameter
  • 1.400 inches bore length
  • f-4 aircraft end application
  • titanium material
  • ams4928 assn standard single material response material specification
53G970602-10 NSN 1680-00-005-3728
  • 0.502 inches bore diameter
  • 1.310 inches bore length
  • f-4 aircraft end application
  • titanium material
  • ams4928 assn standard single material response material specification
53G970602-3 NSN 1680-00-005-3729
  • 0.4395 inches bore diameter
  • 0.890 inches bore length
  • f-4 aircraft end application
  • titanium material
  • ams4928 assn standard single material response material specification
53G970602-4 NSN 1680-00-005-3730
  • 0.4395 inches bore diameter
  • 0.890 inches bore length
  • f-4 aircraft end application
  • outer wing slat mechanism special features
  • titanium material
53G970602-9 NSN 1680-00-005-3731
  • 0.502 inches bore diameter
  • 1.310 inches bore length
  • f-4 aircraft end application
  • outer wing slat mechanism special features
  • titanium material
53G970701-35 NSN 1680-00-005-3732 Cross Reference: 53G970701-13
  • 0.8765 inches bore diameter
  • 3.545 inches bore length
  • fulcrum bore features provided
  • fsc app data: inner wing slats, f-4 aircraft special features
  • steel material
53G970701-36 NSN 1680-00-005-3733 Cross Reference: 53G970701-14
  • 0.8765 inches bore diameter
  • 3.545 inches bore length
  • fulcrum bore features provided
  • fsc app data: inner wing slats, f-4 aircraft special features
  • steel material
53G970701-15 NSN 1680-00-005-3734 Cross Reference: 53G970701-9
  • 0.6265 inches bore diameter
  • 1.720 inches bore length
  • fulcrum bore features provided
  • fsc app data: inner wing slats, f-4 aircraft special features
  • titanium alloy material
53G970701-48 NSN 1680-00-005-3736 Cross Reference: 53G970701-20, 53G970701-38
  • 0.6265 inches bore diameter
  • 2.000 inches bore length
  • f-4 aircraft end application
  • steel material
  • ams6427 assn standard single material response material specification
53G970601-6 NSN 1680-00-005-7278
  • 0.4395 inches bore diameter
  • 1.500 inches bore length
  • f-4 aircraft end application
  • titanium material
  • ams4928 assn standard single material response material specification
53G970602-15 NSN 1680-00-005-9107 Cross Reference: 53G970602-5
  • 0.4395 inches bore diameter
  • 0.875 inches bore length
  • f-4 aircraft end application
  • aluminum alloy material
53G970602-16 NSN 1680-00-005-9108 Cross Reference: 53G970602-6
  • 0.4395 inches bore diameter
  • 0.875 inches bore length
  • f-4 aircraft end application
  • aluminum alloy material
53G970602-7 Outer Wing Slat Mechanism NSN 1680-00-005-9109
  • 0.502 inches bore diameter
  • 1.911 inches bore length
  • f-4 aircraft end application
  • fulcrum bore provided special features
  • aluminum alloy material
53G970602-8 Outer Wing Slat Mechanism NSN 1680-00-005-9110
  • 0.502 inches bore diameter
  • 1.911 inches bore length
  • f-4 aircraft end application
  • fulcrum bore provided special features
  • aluminum alloy material
S6140-62620-009 NSN 1680-00-006-4481
  • 0.249 inches bore diameter
  • between 0.870 inches and 0.875 inches bore length
  • bearing features provided
  • aluminum alloy material
  • anodize surface treatment
107C2705-11 NSN 1680-00-007-9791
114C1232-6 NSN 1680-00-014-0703
  • 1.580 inches bore diameter
  • 1.460 inches bore length
  • bearing and counterbore features provided
  • 3.410 inches all ends center to center distance between fulcrum and arm end hole/slot/ball
  • magnesium alloy material
65207-03055-041 NSN 1680-00-023-9359
53G970701-27 NSN 1680-00-024-3633
  • between 0.877 inches and 0.878 inches bore diameter
  • between 2.027 inches and 2.032 inches bore length
  • aircraft end application
  • fulcrum bore provided special features
  • steel material
53G970701-29 Inner Wing Slats NSN 1680-00-024-3641
  • between 0.627 inches and 0.628 inches bore diameter
  • between 1.715 inches and 1.725 inches bore length
  • aircraft end application
  • fulcrum bore provided special features
  • titanium material
272-5065004-19 NSN 1680-00-028-8410
  • 0.875 inches bore diameter
  • b-57 aircraft end application
  • bearing features provided
  • magnesium alloy material
  • dichromate surface treatment