Remote Control Levers - Page 23 of 32

798 part numbers
7-311518019 NSN 1680-01-188-9886
300367-101 Tablock H-link Assembly NSN 1680-01-189-1446
  • aircraft kc135r end application
75A667165-1001 NSN 1680-01-190-8642
75A667224-2001 NSN 1680-01-190-8643
458-52251-502 NSN 1680-01-193-8970
  • between 1.250 inches and 1.268 inches major diameter
  • 9 spline quantity
  • aircraft model kc-135 end application
  • 1.016 inches minor diameter
  • splined bore type
458-52251-503 NSN 1680-01-193-8971
  • between 1.250 inches and 1.268 inches major diameter
  • 9 spline quantity
  • aircraft kc-135 end application
  • 1.016 inches minor diameter
  • splined bore type
458-52251-504 NSN 1680-01-193-8972
  • between 1.250 inches and 1.268 inches major diameter
  • 9 spline quantity
  • aircraft kc-135 end application
  • 1.016 inches minor diameter
  • splined bore type
458-52251-507 NSN 1680-01-193-8973 Cross Reference: 458-52251-505
  • aircraft kc-135 end application
  • 3.000 inches center to center distance between link and shaft holes
  • 1.950 inches shaft end thickness
  • 0.860 inches link end thickness
  • between 0.313 inches and 0.327 inches link end hole diameter
458-52251-508 NSN 1680-01-193-8974 Cross Reference: 458-52251-506
  • aircraft kc-135 end application
  • 3.000 inches center to center distance between link and shaft holes
  • 1.950 inches shaft end thickness
  • 0.860 inches link end thickness
  • between 0.313 inches and 0.327 inches link end hole diameter
65-19484-1 NSN 1680-01-200-5560
  • aircraft model c-18a end application
7-311610014-3 NSN 1680-01-203-2063
  • 0.640 inches overall width
  • between 0.504 inches and 0.506 inches bore diameter
  • 1.310 inches bore length
  • plain straight bore type
  • 0.942 inches center to center distance between link and shaft holes
7-311514091-3 NSN 1680-01-203-5221 Cross Reference: 7-311514091
  • ah-64 airframe, rotary wing aircraft end application
7-311512095-3 NSN 1680-01-203-8258
L3400146-011 NSN 1680-01-205-1435
  • 1.000 inches overall width
  • aircraft model b-1b end application
  • 0.550 inches shaft end thickness
  • 0.090 inches link end thickness
  • pivot hole through one wall only; nha l3400134 special features
1292797-101 NSN 1680-01-206-1303
  • between 2.668 inches and 2.690 inches bore length
  • plain straight bore type
739169 NSN 1680-01-210-6833 Cross Reference: 736169, 736505
  • 0.844 inches major diameter
  • 26 spline quantity
  • b-1b acft; valve, flow control p/n 735342 end application
  • 0.750 inches minor diameter
  • splined bore type
75A613001-2003 NSN 1680-01-223-0751
  • between 1.312 inches and 1.313 inches bore diameter
  • 1.375 inches bore length
  • plain straight bore type
  • 7.080 inches center to center distance between link and shaft holes
  • 1.375 inches shaft end thickness
30076 NSN 1680-01-227-7371
  • used on valve 48180-5 special features
581R013 NSN 1680-01-234-4360
12W9275-13 NSN 1680-01-262-4293
  • f-111a/d/e/ef/fb aircraft end application
107C2311-6 NSN 1680-01-268-8145
  • model ch-46d helicopter end application
751788-1-1 NSN 1680-01-282-0332
10330-1 NSN 1680-01-284-9869
A5528 NSN 1680-01-292-4899
L5303533-013 NSN 1680-01-302-7574
  • b-1b aircraft; forward instructor seat end application
  • steel material
  • ams 5520 assn standard single material response material specification