Indicator Panels - Page 15 of 35

866 part numbers
17P1E1142-1 NSN 1680-01-393-2317
  • c-17 globemaster aircraft end application
  • aluminum alloy panel material
  • panel control-light, pedestal special features
3338017-1 NSN 1680-01-393-6169
  • c-130h aircraft end application
  • light indicator type
  • aluminum alloy panel material
  • used on the scns nav relay panel special features
  • 8 quantity
70550-21900-118 NSN 1680-01-393-6859 Cross Reference: 844182-16
  • between 5.730 inches and 5.750 inches overall width
  • sf-60f acft end application
  • dial indicator type
  • aluminum panel material
3341088-3 NSN 1680-01-393-7355
  • c-130h aircraft end application
  • buzzer indicator type
  • aluminum alloy panel material
  • pilot; co-pilot audio missile warning panel special features
  • 1 quantity
75A800043-1023 NSN 1680-01-394-2991
872361-3 NSN 1680-01-394-3987
  • between 5.735 inches and 5.750 inches overall length
  • between 5.235 inches and 5.250 inches overall height
  • between 5.235 inches and 5.250 inches overall width
  • 0.090 inches overall thickness
  • c-130 airplane end application
872361-1 NSN 1680-01-394-3995
  • 0.090 inches overall thickness
  • c-130 airplane end application
  • any acceptable indicator type
  • aluminum alloy, qq-a-250/11, alloy 6061, t6 panel material
  • anodize surface treatment
A55A14347-1 NSN 1680-01-394-5959
  • aircraft model f14 end application
70550-21900-111 NSN 1680-01-397-0765
504-230-002 NSN 1680-01-397-2496
  • aircraft model f-14d end application
  • panel, front, assembly (a5) rf/cip special features
590-474-001 NSN 1680-01-397-8314
3339045-1 NSN 1680-01-398-5830
  • 24.000 inches overall height
  • 21.000 inches overall width
  • 0.125 inches overall thickness
  • c-130 hercules aircraft end application
  • aluminum alloy panel material
3339045-3 NSN 1680-01-398-5831
  • 24.000 inches overall height
  • 21.000 inches overall width
  • 0.125 inches overall thickness
  • c-130 hercules aircraft end application
  • aluminum alloy panel material
3339046-1 NSN 1680-01-398-5832
  • 24.000 inches overall height
  • 21.000 inches overall width
  • 0.125 inches overall thickness
  • c-130 hercules aircraft end application
  • aluminum alloy panel material
3339046-3 NSN 1680-01-398-5834
  • 24.000 inches overall height
  • 21.000 inches overall width
  • 0.125 inches overall thickness
  • c-130 hercules aircraft end application
  • aluminum alloy panel material
3341097-5 NSN 1680-01-398-8112
  • c-130 hercules aircraft end application
  • aluminum alloy and plastic panel material
  • panel assembly; special features
3341097-7 NSN 1680-01-398-8113
  • c-130 hercules aircraft end application
  • aluminum alloy and plastic panel material
  • panel assembly; special features
204-40502-48 NSN 1680-01-399-3534
21049403-101 NSN 1680-01-399-5493
6H4414-1 NSN 1680-01-408-2085
  • aircraft model ea-6b end application
414E3038-2B NSN 1680-01-409-2928
820996-410 NSN 1680-01-410-7276
441-36207-004 NSN 1680-01-411-0766 Cross Reference: 10106350
  • aircraft f/a 18 end application
  • panel fault function usage design
  • panel, fault function special features
  • 441-36207-004 type/model designation
530408-110 NSN 1680-01-411-9310
1515622-103 NSN 1680-01-413-1964
  • used on tristar acft. end application