Bell Cranks - Page 8 of 59

1465 part numbers
68A351005-1005 NSN 1680-00-280-0717
  • aluminum alloy material
  • anodize surface treatment
68A351104-1005 NSN 1680-00-280-0720
  • bearing and fulcrum bore features provided
68A610043-1003 NSN 1680-00-280-7116
  • aluminum alloy material
68A610043-1004 NSN 1680-00-280-7117
  • aluminum alloy material
1284721-101 NSN 1680-00-283-3966
  • between 1.625 inches and 1.626 inches bore diameter
  • between 0.516 inches and 0.526 inches bore length
  • paint surface treatment
  • nose landing gear, acft fsc application data
1292032-101 NSN 1680-00-283-4230
  • between 1.192 inches and 1.193 inches bore diameter
  • between 1.058 inches and 1.068 inches bore length
  • paint surface treatment
  • stabilizer, aircraft fsc application data
68A351122-1003 NSN 1680-00-283-8116
  • 0.625 inches bore diameter
  • 3.000 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.500 inches 2nd end end hole/ball diameter
  • anodize surface treatment
68A610010-1008 NSN 1680-00-283-8239
  • between 1.235 inches and 1.265 inches bore diameter
  • 2.142 inches bore length
  • aluminum alloy material
68A620018-1003 NSN 1680-00-283-8246
  • 1.250 inches bore diameter
  • 5.500 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.250 inches 2nd end end hole/ball diameter
  • aluminum alloy material
68A640043-1003 NSN 1680-00-283-8248
  • aluminum alloy material
68A351106-1001 NSN 1680-00-283-8492
  • aluminum alloy material
  • anodize surface treatment
1283092-105 NSN 1680-00-284-1797
  • between 3.596 inches and 3.597 inches bore diameter
  • aluminum alloy material
  • paint surface treatment
  • horizontal stabilizer, acft fsc application data
1285566-101 NSN 1680-00-292-5374 Cross Reference: 1285622-105
  • aluminum alloy material
  • paint surface treatment
  • hook, arresting, airframe fsc application data
1285634-101 NSN 1680-00-292-5378
  • steel material
  • paint surface treatment
  • arresting hook bumper, airframe fsc application data
68A451015-1003 NSN 1680-00-296-4138
  • 0.191 inches bore diameter
  • 3.270 inches bore length
S14-30-3121-2 NSN 1680-00-303-8586
  • 0.750 inches bore diameter
  • 0.625 inches bore length
  • fulcrum bore provided special features
  • magnesium alloy material
0660244-6 NSN 1680-00-304-4569
  • 3.562 inches bore length
  • bearing and counterbore features provided
  • fulcurm bore provided special features
339701 NSN 1680-00-306-3559
  • 0.129 inches bore diameter
  • 0.080 inches bore length
  • 0.500 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.195 inches 2nd end end hole/ball diameter
  • flat, one or more holes both arms style designator
348539 Manufacturers Suggested Name - Lever - Nlg - Manual Release Mech NSN 1680-00-306-3840
  • c-130 aircraft end application
  • plain fulcrum bore shape
  • 0.375 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
  • qq-a-601 federal specification single material response material specification
272-5065006-29 NSN 1680-00-307-0830
  • b-57c aircraft end application
  • magnesium material
61C010-12 NSN 1680-00-307-9700
  • bqm-34 end application
3480537 NSN 1680-00-308-6320 Cross Reference: 4393814
8B414227-21 NSN 1680-00-313-0462
8B414227-22 NSN 1680-00-313-0463
68A351015-1003 NSN 1680-00-314-3157
  • 0.812 inches bore diameter
  • 3.048 inches bore length
  • aluminum material
  • anodize surface treatment