Electrical-electro Control Panels - Page 64 of 78

1928 part numbers
70552-02411-041 NSN 1680-01-569-4629
204-16418-10 NSN 1680-01-569-6774
204-60746-5 NSN 1680-01-570-0089
193-10540-000 NSN 1680-01-570-2611
4077156-0504 NSN 1680-01-570-5550
74G870604-1135 NSN 1680-01-570-8203
HM022-123-81 Panel NSN 1680-01-570-8387
  • 1680-01-570-8387 end application
S7055-12003-041 NSN 1680-01-571-0067
  • f-16 aircraft; t.o.11f32-2-43-2 end application
  • b-52h aircraft end application
HM022-367-11 NSN 1680-01-572-3332
  • ch-47 end application
  • 8.750 inches overall length
  • 4.510 inches overall height
  • 5.150 inches overall width
  • kc-135 aircraft end application
160D180425-13 Control Ele Panel NSN 1680-01-573-1034
  • a-10 aircraft end application
C99A53400-1 Crypto Load Panel NSN 1680-01-573-1394
  • ln e-8c jstars end application
G7493-10 NSN 1680-01-573-3258
  • four screws one in each corner mounting configuration
  • 5.688 inches overall length
  • 1.063 inches overall height
  • between 0.207 inches and 0.253 inches overall thickness
  • 2 ms3498-9 grommet assembly, 1 at each end mounting configuration
  • plastic panel material
  • 5.688 inches overall length
  • 1.063 inches overall height
  • between 0.207 inches and 0.253 inches overall thickness
  • c-2a aircraft end application
  • 2 ms3498-8 grommet assembly, 1 at each short end mounting configuration
70450-01825-105 NSN 1680-01-573-5859 Cross Reference: 1120000-005, 70450-01825
900-5141-001 Upper Lighted Panel NSN 1680-01-573-7614
  • helicopter, utility end application
900-5141-002 Upper Lighted Panel NSN 1680-01-573-7615
  • helicopter, utility end application
  • helicopter, utility end application
74G870621-1991 NSN 1680-01-574-3367
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870621-1985 NSN 1680-01-574-3400
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870621-1989 NSN 1680-01-574-3404
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description
74G870621-1993 NSN 1680-01-574-3409
  • af/a-18 airframe end application
  • any acceptable panel material
  • used on f-18 aircraft functional description