Nonrotating Shaft Eye Brackets - Page 4 of 12

291 part numbers
3101688-1 NSN 1680-01-420-3953
7597170G1 NSN 1680-01-421-1158
  • 2.900 inches overall length
  • pacer dawn end application
  • aluminum alloy material
212-011-701-125 NSN 1680-01-426-0770
  • h-1 iroquois end application
19048-00 NSN 1680-01-429-2261 Cross Reference: A-1920
1250041-101 NSN 1680-01-436-0318
  • s-3b aircraft end application
1250041-102 NSN 1680-01-436-0323
  • s-3b aircraft end application
17P1A4424-503 NSN 1680-01-437-5020
  • c-17a aircraft end application
67A79B39 NSN 1680-01-438-7124
  • used for support equipment end application
293942 NSN 1680-01-439-2413 Cross Reference: 10106353
  • f-18 aircraft end application
68A413043-2003 NSN 1680-01-443-0666
  • f-15 aircraft end application
68R096017-2047 Manufacturers Suggested Name - Support NSN 1680-01-445-7591
  • f-15i aircraft end application
  • steel material
17P2G5001-505 NSN 1680-01-446-5560
  • c-17 aircraft end application
23057423 Rh Propeller Gearbox Strut Fitting NSN 1680-01-446-7733
  • used on c130j hercules end application
S6165-62064-015 NSN 1680-01-451-3846 Cross Reference: S6165-62064-15
  • sh-3a aircraft end application
  • anodize finish special features
S6165-62064-014 NSN 1680-01-451-3850 Cross Reference: S6165-62064-14
  • sh-3a aircraft end application
  • anodize finish special features
5005780 NSN 1680-01-454-1441
  • used on f-16 engine start system end application
3392AS327 Forward Helo Bracket NSN 1680-01-467-5184
  • 3.263 inches width
  • 9.730 inches overall length
  • 9.730 inches overall height
  • sh60b end application
  • 1.750 inches bore inside diameter
3355434-1 NSN 1680-01-473-0323
  • 5.000 inches width
  • 5.000 inches overall length
  • c-130j end application
  • aluminum alloy material
  • qq-a-250/12 federal specification single material response material specification
17P2F8851-1 NSN 1680-01-476-3652
AWE7320-1 Fitting-strut NSN 1680-01-477-9181
  • 1 plain mounting hole type and quantity
17P2G1206-2 NSN 1680-01-478-7390
17P2G1206-1 NSN 1680-01-479-6023
KC73213-001 NSN 1680-01-481-4765
133-100183-7 NSN 1680-01-482-4147
  • t-6, joint primary aircraft trainer (j-pat) end application
K633116-3 Crank Cargo Door Latch NSN 1680-01-486-1216
  • between 0.375 inches and 0.377 inches bore inside diameter
  • 1 plain mounting hole type and quantity
  • 0.201 inches mounting hole diameter
  • steel material