Electrical-electro Control Panels - Page 43 of 78

1928 part numbers
133-360055-1 NSN 1680-01-483-4121
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360066-1 NSN 1680-01-483-4122
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360067-1 NSN 1680-01-483-4123
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360068-1 NSN 1680-01-483-4124
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360070-1 NSN 1680-01-483-4125
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360069-1 NSN 1680-01-483-4126
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360073-1 NSN 1680-01-483-4127
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360075-1 NSN 1680-01-483-4128
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360090-1 NSN 1680-01-483-4129
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360076-1 NSN 1680-01-483-4130
  • t-6 joint primary aircraft trainer (j-pat) end application
133-360096-1 NSN 1680-01-483-4131
  • t-6 joint primary aircraft trainer (j-pat) end application
133-380057-3 NSN 1680-01-483-4135
  • t-6 joint primary aircraft trainer (j-pat) end application
16F8425-3 NSN 1680-01-483-8778
  • f-16 end application
1223016-103 NSN 1680-01-483-9883 Cross Reference: 1223016
770-301001-507 Front Panel Assy-environmental System Panel NSN 1680-01-484-1038
  • c-17a aircraft end application
  • 10 each dzus fastners mounting configuration
  • feat criticality code justification
123AV80036-1 Cec Control Panel Assy NSN 1680-01-484-1105
  • any acceptable panel material
  • agav criticality code justification
C99A30443-1 NSN 1680-01-484-2257
  • e-8, jstars end application
  • aluminum alloy panel material
74A800648-1045 NSN 1680-01-484-3319
  • fighter aircraft-first (f18 e/f) end application
  • agav criticality code justification
5M2370-004 Multiplex Bus Impedance Matching Panel NSN 1680-01-484-3332 Cross Reference: AE143-003-99, P17976
  • agav criticality code justification
65552-55580-041 NSN 1680-01-484-4235
  • fuel control panel usage design
  • nhap-n6-507-0555 fsc application data
65552-55580-042 NSN 1680-01-484-4236
  • emergency control panel usage design
  • nhap-n6-507-0555 fsc application data
7-W13200111-1 NSN 1680-01-484-4957
  • apache attach helicopter end application
75G800299-1001 NSN 1680-01-484-7906
  • nha pn 75a800131 fsc application data
EGD-0936-3 NSN 1680-01-485-3052
  • 5.720 inches overall length
  • 2.960 inches overall width
  • 0.130 inches overall thickness
  • 4 1/4 turn dzus fasteners accessory components and quantity
  • aluminum alloy, qq-a-250/11, alloy 6061, t6 panel material
11465563-002 NSN 1680-01-485-5539
  • 0.190 inches overall thickness
  • draw-er-114-6556 end application
  • aluminum alloy panel material
  • material is qq-a-250/11 6061 t4 special features