Bell Cranks - Page 42 of 59

1465 part numbers
838889-401 NSN 1680-01-391-2069
  • c-17a aircraft end application
  • used on crew seat special features
  • aluminum alloy material
  • flat, one or more holes both arms style designator
DAA3255A118-029 NSN 1680-01-392-6787
  • b-2a acft end application
2010659-101 NSN 1680-01-392-7308
17P2N3026-1 NSN 1680-01-392-9857
  • c-17a aircraft end application
  • aluminum alloy material
  • tongue end, vertical holes other arm style designator
1559238-105 NSN 1680-01-393-9567
145C3510-5 NSN 1680-01-394-8582 Cross Reference: 145C3510-1
  • ch-47 helicopter end application
  • steel material
3338413-1 NSN 1680-01-395-8286
  • c-130 aircraft end application
  • aluminum alloy material
  • clevis, blind hole and flanged arm style designator
3338413-3 NSN 1680-01-396-0882
  • c-130 aircraft end application
  • aluminum alloy material
17P2F8151-1 NSN 1680-01-396-9957
  • c-17a aircraft end application
  • aluminum alloy material
  • raised faced holes, offset arm style designator
145C3516-1 NSN 1680-01-397-0417
  • 0.610 inches bore diameter
  • 0.753 inches bore length
  • ch-47 helicopter end application
  • steel material
  • clevis, tongue style designator
5091737 NSN 1680-01-399-4144
  • 0.250 inches bore diameter
  • 0.063 inches bore length
  • av-8b harrier aircraft, apg-65 radar end application
  • steel material
  • flat, offset both arms style designator
5110469 NSN 1680-01-399-4145
  • av-8b aircraft end application
  • steel material
5091736 NSN 1680-01-399-4147
  • av-8b aircraft end application
  • steel material
17P2A3147-503 NSN 1680-01-407-2843
  • c-17a aircraft end application
L5875012-002 NSN 1680-01-407-5457
  • b-1b aircraft end application
3338413-2 NSN 1680-01-407-8268
  • c-130 aircraft end application
3338413-4 NSN 1680-01-407-8271
  • c-130 aircraft end application
74A610015-2001 Yoke Control Stick NSN 1680-01-408-6544
  • aircraft model f/a-18 end application
17P2C1181-1 NSN 1680-01-409-0363
17P2C1181-501 Fwd Mlg End Driven Torque Tube Manufacturers Suggested Name - Arm Assy NSN 1680-01-411-8595
  • 1.004 inches 1st end slot width
  • c-17 aircraft end application
  • 29.375 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.751 inches 2nd end end hole/ball diameter
406-001-300-101 NSN 1680-01-411-9218
  • oh-58d aircraft end application
17P2C1187-1 Mlg End Driven Aft Torque Tube Manufacturer Suggested Name - Arm Assy NSN 1680-01-412-0355
  • 3.793 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
L5875012-001 NSN 1680-01-412-7298
  • b-1b bomber end application
DAA3255A142-009 NSN 1680-01-413-5383
  • 0.7500 inches bore diameter
  • b-2 aircraft end application
  • 2.021 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.190 inches 2nd end end hole/ball diameter
76207-10009-115 NSN 1680-01-416-2634
  • aircraft, model s76 end application