Bell Cranks - Page 33 of 59

1465 part numbers
68A351109-2003 NSN 1680-01-009-9297
  • steel material
  • anodize surface treatment
160D123210-6 NSN 1680-01-009-9472
  • aluminum alloy material
  • control, fuselage, airframe fsc application data
160D123151-1 NSN 1680-01-009-9474
  • aluminum alloy material
  • control, rudder, fuselage fsc application data
160D120310-7 NSN 1680-01-010-2818 Cross Reference: 160D120310-5
  • aluminum alloy material
  • cable, control, fuselage aircraft fsc application data
160D121210-1 NSN 1680-01-010-2819
  • aluminum alloy material
  • control, pitch, fuselage aircraft fsc application data
160D722110-1 NSN 1680-01-010-2820 Cross Reference: 162D722110-1001
  • aluminum alloy material
  • trim tab, fuselage aircraft fsc application data
160D622130-1 NSN 1680-01-010-2823 Cross Reference: 162D622130-1001
  • aluminum alloy material
  • control, fuselage aircraft fsc application data
160D622325-5 NSN 1680-01-010-2824 Cross Reference: 160D622325-1, 160D622325-3, 162D622325-1001
  • steel material
  • control, fuselage aircraft fsc application data
160D121225-3 NSN 1680-01-010-2825 Cross Reference: 160D121225-1
  • between 0.873 inches and 0.874 inches bore diameter
  • between 0.813 inches and 0.823 inches bore length
  • aluminum alloy material
  • clevis ends style designator
  • control installation, fuselage, airframe fsc application data
1292894-107 NSN 1680-01-011-0976
  • wing aircraft fsc application data
160D123205-3 NSN 1680-01-011-8860
  • aluminum alloy material
160D123145-3 NSN 1680-01-012-7144
  • between 0.875 inches and 0.876 inches bore diameter
  • between 0.965 inches and 0.970 inches bore length
  • aircraft model a10 end application
  • aluminum alloy material
160D123205-5 NSN 1680-01-012-7145 Cross Reference: 160D123205-7
  • between 0.750 inches and 0.751 inches bore diameter
  • 1.360 inches bore length
  • aircraft model a10 end application
  • aluminum alloy material
160D627110-1 NSN 1680-01-013-1842 Cross Reference: 160D627110-3, 162D627110-1001
160D121235-1 NSN 1680-01-013-8799
  • aluminum alloy material
  • pitch control, fuselage aircraft fsc application data
160D622310-2 NSN 1680-01-015-0847 Cross Reference: 162D622310-1002
  • 0.875 inches bore diameter
  • between 2.000 inches and 2.010 inches bore length
  • 6.212 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • raised face pivot hole, clevis both ends style designator
  • control installation, fuselage, airframe fsc application data
160D523120-1 NSN 1680-01-015-0848 Cross Reference: 160D523120-3
  • aluminum alloy material
  • control installation, fuselage, airframe fsc application data
160D521113-1 NSN 1680-01-015-0849 Cross Reference: 160D521113-3
  • aluminum alloy material
  • control installation, fuselage, airframe fsc application data
160D725150-1 NSN 1680-01-015-7316 Cross Reference: 160D725150-3, 162D725150-1001
  • 0.624 inches bore diameter
  • 0.500 inches bore length
  • aluminum alloy material
  • control installation, fuselage, airframe fsc application data
5-98328-3000 NSN 1680-01-017-7715
5-98328-3001 NSN 1680-01-017-7716
K653022-9 NSN 1680-01-020-2717
  • 1.062 inches bore diameter
  • aluminum alloy material
K652172-5 NSN 1680-01-021-8256
  • between 0.748 inches and 0.749 inches counterbore diameter
  • between 0.234 inches and 0.238 inches counterbore depth
  • 0.625 inches bore diameter
  • between 2.938 inches and 2.943 inches bore length
  • aluminum alloy material
K653057-3 NSN 1680-01-021-8257
  • between 0.874 inches and 0.875 inches counterbore diameter
  • between 0.308 inches and 0.313 inches counterbore depth
  • aluminum alloy material
K651083-3 NSN 1680-01-021-8258 Cross Reference: K651083-1
  • between 0.748 inches and 0.749 inches counterbore diameter
  • between 0.234 inches and 0.239 inches counterbore depth
  • between 0.749 inches and 0.750 inches bore diameter
  • between 1.250 inches and 1.255 inches bore length
  • aluminum alloy material