Remote Control Levers - Page 25 of 32

798 part numbers
L6317076-011 NSN 1680-01-369-7844
  • 0.500 inches overall width
  • 2.600 inches center to center distance between link and shaft holes
  • 0.2500 inches link end hole diameter
  • steel material
  • ams 5643 assn standard single material response material specification
68A410637-1001 NSN 1680-01-369-9323
  • f-15 aircraft; main landing gear end application
  • bolt assembly, drag brace; t.o. 4a4-22-4, fig 53 special features
17P1C7213-1 NSN 1680-01-369-9812
  • c-17a aircraft end application
  • aluminum alloy material
17P2A3123-1 NSN 1680-01-370-2072
17P1C7223-1 NSN 1680-01-370-2073
  • 0.790 inches major diameter
  • splined bore type
  • 1.000 inches center to center distance between link and shaft holes
5363-702 NSN 1680-01-372-2210
  • ffg guided missile frigate end application
AJH7143-501 NSN 1680-01-372-2596
  • c-17a airlifter airplane end application
4022T59G02 NSN 1680-01-372-7958
85010-55 NSN 1680-01-373-0616
  • pacer dawn end application
  • part of fuel selector valve assembly special features
DAA3519A003-009 NSN 1680-01-373-6673
  • pacer special end application
  • 5.300 inches center to center distance between link and shaft holes
  • between 1.335 inches and 1.345 inches shaft end thickness
  • between 0.615 inches and 0.620 inches link end thickness
  • between 0.260 inches and 0.265 inches distance between fork inside spread
472P011C024-1 NSN 1680-01-374-0362
  • aircraft harrier av8 a/b end application
A55H10501-11 NSN 1680-01-374-2094
  • 0.750 inches overall width
  • between 0.127 inches and 0.133 inches keyway width
  • 0.750 inches keyway length
  • f-14d tomcat airplane end application
  • 0.375 inches shaft end thickness
204-18711-1 NSN 1680-01-375-0950
  • e-3a awacs aircraft end application
  • plain straight bore type
  • aluminum alloy material
1536-00-1 NSN 1680-01-375-5967
75A800065-1005 NSN 1680-01-376-8049
  • harrier gr5 spares end application
DL1422M1-1 NSN 1680-01-376-9194
  • used on embriere 312 aircraft end application
DL1422M1-2 NSN 1680-01-376-9195
  • used on embriere 312 aircraft end application
L6310146-005 NSN 1680-01-379-4900
  • 3.100 inches overall width
  • 0.5625 inches bore diameter
  • 1.128 inches bore length
  • b-1b aircraft end application
  • plain straight bore type
MBEU140956 NSN 1680-01-380-0932
  • aircraft fa-18 end application
  • bottom cross shaft seat bucket special features
MBEU147198 NSN 1680-01-380-4427
  • f/a-18 hornet aircraft end application
  • lever-outer s.p.s.m; matl; cres ams 5659 h 1100 special features
MBEU140833 NSN 1680-01-380-4437
  • f/a-18 hornet aircraft end application
  • lever-pawl go forward mech special features
75A603558-2003 NSN 1680-01-381-2437
  • harrier gr5/7 end application
748951B NSN 1680-01-381-3592
  • b-2a aircraft end application
  • forward unlock drive unit assembly special features
374091-1 NSN 1680-01-382-1149
  • aircraft c-130 end application
  • link end threaded hole features provided
  • crank elevator torque tube special features
  • aluminum alloy material
3403160-1 NSN 1680-01-384-2151