Electrical-electro Control Panels - Page 19 of 78

1928 part numbers
DAA3233A020-025 NSN 1680-01-384-4509
  • pacer special end application
  • control panel-overhead lighting special features
A55A10196-3 NSN 1680-01-384-4789
  • f14 acft end application
128AV50200-3 NSN 1680-01-384-5189
  • aircraft a-6e end application
  • mount constant speed drive usage design
  • constant speed drive panel assembly special features
L5306281-011 NSN 1680-01-385-8525
16E1077-851 NSN 1680-01-386-0168
  • f-16 aircraft end application
  • main fuel panel; front seat special features
766-302000-505 NSN 1680-01-386-2863
  • c-17a aircraft end application
  • front panel assembly special features
3341424-1 NSN 1680-01-386-4989
  • c-130 cargo aircraft end application
  • mounting holes on all 4 corners mounting configuration
  • aluminum panel material
  • pilots lighting control panel special features
41646-1 NSN 1680-01-386-5060 Cross Reference: 10-0178-1
  • 5.656 inches overall length
  • 2.563 inches overall height
  • 5.656 inches overall width
  • between 0.210 inches and 0.230 inches overall thickness
  • ch-53d and ch-53e helicopter. end application
65912-01250-044 NSN 1680-01-387-6715
  • mh-53 helo end application
A51A10200-5 NSN 1680-01-388-0310
  • f-14d aircraft end application
476270-01-01 NSN 1680-01-388-1892 Cross Reference: ZC8-60-931-1-1
  • pacer dawn end application
DAA3272A001-047 NSN 1680-01-388-2203
  • pacer special end application
  • hardened nuclear hardness critical feature
3341171-1 NSN 1680-01-388-6863
  • 0.063 inches overall thickness
  • c-130 hercules aircraft end application
  • aluminum alloy panel material
410387-01 NSN 1680-01-388-9584
53-79264-301 NSN 1680-01-388-9625
768-301003-501 NSN 1680-01-389-6320
768-101000-505 NSN 1680-01-390-3578
  • c-17 aircraft end application
  • feat criticality code justification
DAA3233A017-017 NSN 1680-01-390-4546
  • b-2 aircraft end application
75A800045-1033 NSN 1680-01-391-7622
75A802109-1007 NSN 1680-01-391-8806
6H4060-1 NSN 1680-01-392-0027
  • a-6e end application
  • aluminum alloy panel material
  • panel controls ground refueling operation special features
3341411-1 NSN 1680-01-392-0477
  • c-130 aircraft end application
  • switches /control accessory components and quantity
  • aluminum alloy panel material
  • equipped with guarded switches special features
3339749-9 NSN 1680-01-392-4904
  • c-130h aircraft end application
3341419-1 NSN 1680-01-392-6081
  • 4.750 inches overall length
  • c-130 aircraft end application
  • four mounting holes at corner edge of panel mounting configuration
  • aluminum alloy panel material
  • pilot; co-pilot overhead control panel special features
DAA3272A003-014 NSN 1680-01-392-8317
  • pacer special end application