Bell Cranks - Page 34 of 59

1465 part numbers
K651026-5 NSN 1680-01-021-8259
  • between 0.749 inches and 0.750 inches counterbore diameter
  • aluminum alloy material
K651028-5 NSN 1680-01-021-8260
  • between 0.749 inches and 0.750 inches bore diameter
  • aluminum alloy material
K651048-3 NSN 1680-01-021-8263
  • 0.812 inches counterbore diameter
  • aluminum alloy material
204-001-809-7 NSN 1680-01-024-8989
  • magnesium material
160D521113-4 NSN 1680-01-025-5340 Cross Reference: 160D521113-2
  • aluminum alloy material
160D622310-1 NSN 1680-01-026-4917 Cross Reference: 162D622310-1001
  • control installation, fuselage, airframe fsc application data
209-001-762-5 NSN 1680-01-026-8910
  • between 0.348 inches and 0.358 inches bore length
  • aluminum alloy material
88D74-1 NSN 1680-01-027-5570
  • e-3a aircraft end application
  • stainless steel material
220-24500-101 NSN 1680-01-028-2217
  • 0.812 inches counterbore diameter
  • between 0.270 inches and 0.280 inches counterbore depth
  • between 0.440 inches and 0.447 inches bore diameter
  • between 1.901 inches and 1.916 inches bore length
  • aluminum alloy material
220-28493-102 NSN 1680-01-028-2218
  • 0.749 inches counterbore diameter
  • 1.380 inches bore length
  • aluminum alloy material
  • anodize surface treatment
220-28301-104 NSN 1680-01-029-5607
  • bearing and fulcrum bore features provided
  • aluminum alloy material
65-38934-501 NSN 1680-01-033-8038 Cross Reference: 65-38934-1
  • 0.250 inches bore diameter
  • aircraft e-3a end application
  • aluminum alloy material
  • rudder trim control fsc application data
220-28301-103 NSN 1680-01-034-3112
  • 0.749 inches counterbore diameter
  • 0.750 inches bore length
  • aluminum alloy material
  • anodize surface treatment
18-73141-1 NSN 1680-01-039-6076
  • raised faced holes, clamp pivot hole, offset style designator
16T7309-803 NSN 1680-01-045-0500 Cross Reference: 16T7309-5, 16T7309-801
  • f-16 aircraft end application
4F53776-101B NSN 1680-01-045-9982
  • bushing 2; unthreaded diameter hole: 0.375in special features
16K2714-3 NSN 1680-01-051-3552
  • f-16 aircraft end application
  • drawing name - bellcrank assembly, drive canopy special features
16K2856-3 NSN 1680-01-052-0937 Cross Reference: 16K2856-1
  • steel material
68A620061-1001 NSN 1680-01-060-8969
  • aluminum alloy material
68A620061-1002 NSN 1680-01-061-6200
  • aluminum alloy material
165-52321-6 NSN 1680-01-068-1546
  • magnesium material
16C0119-1 NSN 1680-01-068-8033
  • f-16 aircraft end application
3F23038-101 NSN 1680-01-073-6448
  • aluminum alloy material
3F23057-101 NSN 1680-01-073-9624
  • aluminum alloy material
15-004-223 NSN 1680-01-076-5955
  • 1.375 inches bore length
  • steel material
  • passivate surface treatment