Electrical-electro Control Panels - Page 42 of 78

1928 part numbers
L5301355-001 NSN 1680-01-481-5727
  • between 5.550 inches and 5.750 inches overall length
  • between 2.688 inches and 2.718 inches overall height
  • b-1b end application
  • aluminum alloy panel material
  • hardened nuclear hardness critical feature
30224-0101 NSN 1680-01-481-9267
  • b-1b aircraft end application
901-172-319-101 NSN 1680-01-482-6766
901-370-356-501 NSN 1680-01-482-6816 Cross Reference: 8522800-920, 901-370-356, C-12487/A
901-172-301-101 NSN 1680-01-482-7056
901-172-291-101 NSN 1680-01-482-7069
901-370-365-201 Aircraft High Power Amplifier NSN 1680-01-482-7078 Cross Reference: 109547
  • cv-22 end application
  • as differientiated by source control reference number differentiating characteristics
70550-22105-053 NSN 1680-01-482-7296
  • mark iii helicopter (sh60-b) end application
KC84453-001 NSN 1680-01-482-8033
  • 3.000 inches overall height
  • between 5.725 inches and 5.755 inches overall width
  • sh-2 (a) seasprite helicopter end application
  • aluminum panel material
  • panel, control-exterior lights functional description
071-01578-0000 NSN 1680-01-482-8430
  • product model cp500 end application
8520118-902 NSN 1680-01-482-9388
  • ch-47d heliccopter end application
  • reversionary select panel, cplt special features
DCU-284/A NSN 1680-01-483-1392 Cross Reference: 765-101000-513, 765101000G513
  • c-17, t.o.8d26-4-4-4 end application
1128EDC001-11 (inavy)control Display Indicator NSN 1680-01-483-2520 Cross Reference: 1128EDC001
  • agav criticality code justification
1128AV43021-19 (inavy)master Light Control NSN 1680-01-483-2530 Cross Reference: 1128AV43021
  • agav criticality code justification
1128AV43036-5 (inavy)interior Lights Control NSN 1680-01-483-2572
  • agav criticality code justification
3705AS164-1 NSN 1680-01-483-2581 Cross Reference: 3705AS164
  • i-cap ii; ea-6b aircraft end application
  • agav criticality code justification
1128AV43022-9 (inavy)interior Lights Control NSN 1680-01-483-2585
  • agav criticality code justification
3705AS234-1 Navigation Control Panel NSN 1680-01-483-2587 Cross Reference: 665AS4100-2
  • i-cap peculiar aircraft (ea-6b) end application
  • agav criticality code justification
1128AV43022-11 (inavy)interior Lights Control NSN 1680-01-483-2588
  • agav criticality code justification
133-340133-3 NSN 1680-01-483-4112
  • t-6 joint primary aircraft trainer (j-pat) end application
133-340138-45 NSN 1680-01-483-4113
  • t-6 joint primary aircraft trainer (j-pat) end application
133-340139-1 NSN 1680-01-483-4114
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360025-3 NSN 1680-01-483-4118
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360048-3 NSN 1680-01-483-4119
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360048-1 NSN 1680-01-483-4120
  • t-6 joint primary aircraft trainer (j-pat) end application