Remote Control Levers - Page 24 of 32

798 part numbers
75A800066-1021 NSN 1680-01-303-1725 Cross Reference: 75A800066-1009, 75A800066-1015
  • aircraft model av-8 end application
75A800066-1013 NSN 1680-01-306-4125
  • aircraft model av-8 end application
L5303533-009 NSN 1680-01-309-3132
  • b-1b aircraft; forward instructor seat end application
  • steel material
  • ams 5520 assn standard single material response material specification
3C11286-101 NSN 1680-01-309-5894
  • 11.120 inches center to center distance between link and shaft holes
  • between 0.377 inches and 0.379 inches link end hole diameter
  • aluminum alloy material
DAA3131D696-001 NSN 1680-01-310-0246
  • pacer special end application
70410-02453-102 NSN 1680-01-310-2224 Cross Reference: 70410-02453
  • 1560-01-081-9238 end application
1284958-101 NSN 1680-01-326-2553
  • aircraft model s3a end application
  • steel material
  • ams 5643 assn standard single material response material specification
1284958-102 NSN 1680-01-326-2554
  • aircraft model s3a end application
  • steel material
  • ams 5643 assn standard single material response material specification
65488 NSN 1680-01-327-6325
  • corrosion resistant special features
  • steel material
7-311610020-1 NSN 1680-01-334-7619 Cross Reference: 7-311610012, 7-311610012-3
  • 0.510 inches overall width
  • between 0.375 inches and 0.377 inches bore diameter
  • 0.593 inches bore length
  • ah-64a end application
  • plain straight bore type
74A733108-2002 NSN 1680-01-335-1768 Cross Reference: 10321344, 3930AS548-2
68A480638-1005 NSN 1680-01-338-6041
  • f-15e acft end application
  • actuator attach, down lock, arresting hook special features
  • steel material
S6130-80071-003 NSN 1680-01-341-5175
  • 1.487 inches center to center distance between link and shaft holes
  • 0.687 inches link end thickness
  • clevis link end, securing hol (s) shaft end style designator
1128ES40058-5 NSN 1680-01-346-2828
  • a-6e acft end application
  • stainless steel and nickel alloy material
75A353062-2003 NSN 1680-01-347-5765
  • steel material
  • ams 5629 assn standard single material response material specification
1128ES40058-1 NSN 1680-01-349-8299
  • ea-6b acft end application
50-524414-5 NSN 1680-01-351-0963
17P6W8223-1 NSN 1680-01-357-2013
  • 1.6275 inches bore diameter
  • 5.775 inches bore length
  • plain straight bore type
  • 7.672 inches center to center distance between link and shaft holes
  • 5.775 inches shaft end thickness
DAA3116A152-003 NSN 1680-01-359-0058
  • pacer special end application
12881-3 NSN 1680-01-360-8311
  • 0.880 inches overall width
  • ch53e helo end application
  • 0.250 inches link end thickness
  • steel material
  • nickel surface treatment
2843239-101 NSN 1680-01-365-1501
  • pacer special end application
  • n/h/a rollover mechanism assembly special features
65-56834-1 NSN 1680-01-365-6070
  • e-3a aircraft; fillet flap installation end application
748975A NSN 1680-01-368-1543 Cross Reference: 748975
  • b-2 aircraft end application
  • used on the forward uplock drive unit assembly special features
756810 NSN 1680-01-368-5416
  • pacer special; drive unit, angle, p/n 748657b end application
L6314072-003 NSN 1680-01-369-4707
  • b-1 bomber end application
  • steel material