Electrical-electro Control Panels - Page 23 of 78

1928 part numbers
152582-1 NSN 1680-01-410-9898
  • support equipment for f/a-18 aircraft fsc application data
3341091-5 NSN 1680-01-411-1338 Cross Reference: 3341091-1
  • c-130 aircraft end application
  • aluminum alloy panel material
1978729-4 NSN 1680-01-411-6930
  • aircraft, k-dc10 end application
3759029-6 NSN 1680-01-411-6931
  • aircraft, k-dc10 end application
41806-1 NSN 1680-01-411-7074
  • h-53 helicopter (non-jsl) end application
40799725-1 NSN 1680-01-411-9331 Cross Reference: 4079725-1
  • c-130e aircraft end application
108476 NSN 1680-01-412-4300
  • 700 w power amplifier end application
  • front special features
70600-81826-108 NSN 1680-01-412-6104 Cross Reference: 710820-8
  • aircraft model sh-60f end application
7-511620101-1 NSN 1680-01-412-9299
  • ah-64d apache longbow helicopter end application
417316-01-01 NSN 1680-01-413-2239
  • 5.750 inches overall length
  • c-130h aircraft end application
  • aluminum alloy panel material
20000532248-001 NSN 1680-01-413-2240
  • 6.000 inches overall length
  • 5.750 inches overall width
  • ac-130u aircraft end application
  • aluminum alloy panel material
3342076-3 NSN 1680-01-413-2242
  • c-130h aircraft end application
  • plastic panel material
20000532262-001 NSN 1680-01-413-2244
  • 2.625 inches overall length
  • 5.365 inches overall width
  • ac-130u aircraft end application
  • four panel fasteners, pfsc35-38a mounting configuration
  • aluminum alloy panel material
20000532202-041 NSN 1680-01-413-9342
  • ac-130u aircraft end application
  • aluminum alloy panel material
20000532260-001 NSN 1680-01-413-9343
  • ac-130u aircraft end application
  • aluminum alloy panel material
  • control for ins (navigation) special features
20000532206-081 NSN 1680-01-413-9345
  • ac-130u aircraft end application
  • aluminum alloy panel material
20000532204-041 NSN 1680-01-413-9348
  • ac-130u aircraft end application
  • aluminum alloy panel material
20000532232-041 NSN 1680-01-413-9349
  • ac-130u aircraft end application
  • aluminum alloy panel material
PEK-166/A37G-16 NSN 1680-01-414-4880 Cross Reference: 103E4226G4
  • c-17 aircraft end application
  • feat criticality code justification
41847-1 NSN 1680-01-414-4935
  • ch-53e helicopter end application
800-006623-1 NSN 1680-01-414-7024 Cross Reference: 20000532075-011, 732M38G02
  • ac-130u aircraft end application
800-003630-1 NSN 1680-01-414-7025 Cross Reference: 20000532074-001
  • ac-130u aircraft end application
17B1U6011-503 NSN 1680-01-414-7245 Cross Reference: 10-50000-04
160D180425-11 NSN 1680-01-414-7459
  • a-10 aircraft end application
  • t.o. 1a-10a-4-21, fig 18, i-34 reference data and literature
160D181815-5 NSN 1680-01-414-7460
  • a-10 aircraft end application
  • t.o. 1a-10a-4-94-1, f-3, i-38 reference data and literature