Electrical-electro Control Panels - Page 40 of 78

1928 part numbers
A51A9287-21 Elect Control Inavy) Panel NSN 1680-01-476-2619 Cross Reference: 6414-203
A51A9287-27 NSN 1680-01-476-2621 Cross Reference: 6414-221
  • f-14 fighter aircraft end application
  • as differentiated by source conrtol drawing reference number differentiating characteristics
A51A9287-25 NSN 1680-01-476-2622 Cross Reference: 6414-202
  • f-14 end application
  • as differentiated by source control drawing reference number differentiating characteristics
773-101000-507 NSN 1680-01-476-4902
769-101000-513 NSN 1680-01-476-4903
6L4710-2 NSN 1680-01-476-6892
  • ea6b special electronic aircraft item end application
  • plastic panel material
  • black 37038 with filled white 17875 letters special features
  • panel assembly-fuel mgmt supplementary features
A51A9287-23 Electrical. Control Panel NSN 1680-01-476-9359 Cross Reference: 6414-204
3356664-1 NSN 1680-01-477-1067
3356664-5 NSN 1680-01-477-1068
A51A10109-23 NSN 1680-01-477-4904
  • f14 aircraft end application
  • agav criticality code justification
3342306-1 NSN 1680-01-477-8471
A/W 37T-1A NSN 1680-01-477-9550 Cross Reference: 3654AS100, 3654AS100-1
74G870623-1327 NSN 1680-01-478-2255 Cross Reference: 74A870623-1155, 74G870623-1243, 74G870623-1269, 74SB283001908
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870621-1999 NSN 1680-01-478-2344 Cross Reference: 74A870621-1549, 74G870621-1691, 74G870621-1827, 74G870621-1917, 74G870621-1981, 74SB283001907
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1427 NSN 1680-01-478-3192 Cross Reference: 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1429 NSN 1680-01-478-3193 Cross Reference: 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1563 NSN 1680-01-478-3194 Cross Reference: 74A870605-1229, 74G870605-1209, 74G870605-1277, 74G870605-1293, 74G870605-1341, 74G870605-1433, 74G870605-1511, 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1431 NSN 1680-01-478-3195 Cross Reference: 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1569 NSN 1680-01-478-3196 Cross Reference: 74A870605-1253, 74G870605-1215, 74G870605-1279, 74G870605-1347, 74G870605-1439, 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1437 NSN 1680-01-478-3197 Cross Reference: 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1441 NSN 1680-01-478-3198 Cross Reference: 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1445 NSN 1680-01-478-3199 Cross Reference: 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870605-1435 NSN 1680-01-478-3200 Cross Reference: 74SB283001909
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G880649-1041 NSN 1680-01-478-3201 Cross Reference: 74G880649-1053, 74SB283001906
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870622-1067 NSN 1680-01-478-3202 Cross Reference: 74SB283001905
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description