Electrical-electro Control Panels - Page 20 of 78

1928 part numbers
504302 NSN 1680-01-392-9056 Cross Reference: 3341407-1
  • 14.000 inches overall length
  • 8.340 inches overall width
  • c-130 aircraft end application
  • offset mounting holes mounting configuration
  • aluminum alloy panel material
3338148-3 NSN 1680-01-392-9860
  • c-130 hercules aircraft end application
  • panel-nav station defensive system; special features
17P1E1301-501 NSN 1680-01-393-0224
  • c-17a aircraft end application
  • rectangular; four mounting holes mounting configuration
  • aluminum alloy, qq-a-250/11, alloy 6061, t6 panel material
  • control panel for areomedical system special features
17P1E1129-1 NSN 1680-01-393-0225
  • c-17a aircraft end application
  • aluminum alloy, qq-a-250/11, alloy 6061, t6 panel material
  • control panel for anti-ice and defog special features
17P1E1524-1 Electrical - Gang Lock - Ads (peu-141/a) Backup Control Panel NSN 1680-01-393-0226
  • c-17a aircraft end application
  • four mounting holes mounting configuration
  • aluminum alloy, qq-a-250/11, alloy 6061, t6 panel material
  • effectivi type 17a001 through 17a040, 17t001 special features
16F8455-811 NSN 1680-01-393-1370 Cross Reference: 16F8455-805
  • f-16 aircraft end application
DAA3272A003-013 NSN 1680-01-393-1371
  • b-2 aircraft end application
765-301000-503 NSN 1680-01-393-1722
  • c-17 aircraft end application
3337114-3 NSN 1680-01-393-6206
  • 31.710 inches overall length
  • c-130h aircraft end application
  • aluminum alloy panel material
3337208-1 NSN 1680-01-393-6944
  • 9.280 inches overall length
  • c-130h aircraft end application
  • circut breakers accessory components and quantity
  • control aircraft power systems usage design
  • aluminum alloy panel material
3337208-3 NSN 1680-01-393-6945
  • c-130h aircraft end application
  • aluminum alloy panel material
  • controls power supply to aircraft systems special features
3337030-5 NSN 1680-01-393-6951
  • c-130h aircraft end application
  • aluminum alloy panel material
  • main instrument panel; pilot and co-pilot special features
3337030-7 NSN 1680-01-393-6953
  • c-130h aircraft end application
  • aluminum alloy panel material
  • co-pilots main instrument panel special features
3337085-3 NSN 1680-01-393-6954
  • c-130h aircraft end application
  • aluminum alloy panel material
  • co-pilots side instrument panel special features
3337086-3 NSN 1680-01-393-6956
  • c-130h aircraft end application
  • aluminum alloy panel material
174310-0002 NSN 1680-01-393-7581 Cross Reference: ZC8-81-205-1-1
  • pacer dawn end application
  • cockpit control unit assembly special features
3341429-3 NSN 1680-01-393-8863
  • 5.620 inches overall length
  • 2.470 inches overall width
  • c-130h aircraft end application
  • four mounting slots at corners mounting configuration
  • aluminum alloy panel material
3339796-1 NSN 1680-01-393-8865
  • c-130h aircraft end application
  • aluminum alloy panel material
3338021-3 NSN 1680-01-393-8894
  • c-130h aircraft end application
  • aluminum alloy panel material
  • navigators instrument switching panel special features
DCU-284/A NSN 1680-01-393-9343 Cross Reference: 765-101000-505
3337114-1 NSN 1680-01-394-2551
  • c-130h aircraft end application
  • aluminum alloy panel material
3341185-1 NSN 1680-01-394-3990
  • c-130h aircraft end application
  • aluminum alloy panel material
  • radome anti-icing control panel special features
3341170-1 NSN 1680-01-394-7765
3341107-5 NSN 1680-01-394-7771
  • c-130h aircraft end application
LS7885B1 NSN 1680-01-395-1871