Bell Cranks - Page 50 of 59

1465 part numbers
160D321030-3 NSN 1680-01-494-0291 Cross Reference: 160D321030
  • a-10 end application
17P2G1325-505 NSN 1680-01-495-1130
74A425101-1006 NSN 1680-01-495-3648 Cross Reference: 74A425101-1004, 74A425107-2002
  • f/a-18 end application
  • agav criticality code justification
  • 3arm, and 4 coaxial holes special features
  • steel material
74A425101-1005 NSN 1680-01-495-3655 Cross Reference: 74A425101-1003, 74A425107-2001
  • f/a-18e/f end application
  • agav criticality code justification
  • steel material
4C27084-111C Lever-flap Control Handle Center Console NSN 1680-01-495-5564 Cross Reference: 4C27084
  • 1.120 inches bore diameter
  • 3.620 inches bore length
  • c-5 aircraft end application
  • aluminum material
  • anodize surface treatment
17P2G1340-501 NSN 1680-01-495-8503
74A675205-2009 NSN 1680-01-496-1421
  • f/a18e/f aircraft end application
  • 2.222 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • clevis ends style designator
17P4F3095-501 Verticle Stabilizer Control Assembly-lower Rudder NSN 1680-01-496-6781
  • c-17a end application
75A613782-2009 NSN 1680-01-499-5172
  • harrier ii aircraft end application
145C3311-3 Bell Crank Assembly NSN 1680-01-499-6225
  • chinook helicopter end application
  • aluminum alloy material
74A675205-2010 (inavy) Bell Crank NSN 1680-01-500-3933
  • f-18 e/f end application
  • agav criticality code justification
5-95616-13 Bell Crank Assembly NSN 1680-01-500-7122
  • 5-95839, bell crank installation end application
  • magnesium alloy material
160D627110-5 NSN 1680-01-502-0854 Cross Reference: 160D627110
  • 1.560 inches bore diameter
  • between 3.767 inches and 3.777 inches bore length
  • a-10 aircraft end application
  • 5.418 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • steel material
212-001-747-1 Walking Beam NSN 1680-01-502-4159
  • helicopter end application
K616283-1 NSN 1680-01-502-7805
  • seasprite, helicopter end application
1506255-101 Bellcrank Assy NSN 1680-01-503-4686
  • tristar; l1011 end application
69-10813-5 NSN 1680-01-505-0384
17P2C1370-505 Rigid Connecting Link NSN 1680-01-508-5307
  • 0.790 inches bore diameter
  • between 2.270 inches and 2.280 inches bore length
  • c-17 aircraft end application
  • bearing and lubrication fitting accommodation features provided
  • plain fulcrum bore shape
17P2C1370-506 NSN 1680-01-508-8186
K633058-11 NSN 1680-01-509-4119
5-89370-1 NSN 1680-01-509-9052
5-89370-2 NSN 1680-01-509-9066
74A661307-1001 Crank Bell NSN 1680-01-510-6732 Cross Reference: 74A661307-1003
  • f/a-1 (e/f) end application
  • agav criticality code justification
5-67388-12 Crank Assembly-lockout Outboard Aileron NSN 1680-01-511-9072
  • c-135 acft end application
  • counterbore and bearing features provided
  • aluminum alloy material
  • ams4050 federal specification single material response material specification
5-89370-4 NSN 1680-01-513-1556