Aircraft Interior Lining Panels - Page 9 of 24

585 part numbers
9809F33022-105 NSN 1680-01-521-8533 Cross Reference: 9809F33022
9809F03020-103 NSN 1680-01-521-8598 Cross Reference: 9809F03020
968412-101 NSN 1680-01-522-3740
  • c-17 acft end application
  • c-17a acft end application
1535118-145 Partition Assembly NSN 1680-01-525-9853
  • l-1011, tristar, aircraft end application
012N8928-103 NSN 1680-01-526-5669
  • f-18 e/f fighter aircraft end application
  • agav criticality code justification
  • 14.59"x10.27" lexan plastic kickshield special features
74A803612-1001 NSN 1680-01-526-5858 Cross Reference: 74A803612
  • c-17a aircraft end application
  • right side side for which designed
  • c-17a aircraft mission design series
123ABP10095-11 Enclosures NSN 1680-01-528-8791
  • 0.031 inches thickness
  • e-2c aircraft end application
  • airborne equip - overhead console aircraft location
  • e-2c aircraft mission design series
  • plastic material
171337-1 Blank Inavy: Module NSN 1680-01-529-8131 Cross Reference: 171337
  • 9.875 inches overall length
  • 1.590 inches overall width
  • 0.125 inches thickness
  • 4920-01-499-7080 next higher assembly identification designator
  • target control system end application
171338-1 Double Blank Inavy: Module NSN 1680-01-529-8141 Cross Reference: 171338
  • 9.875 inches overall length
  • 1.590 inches overall width
  • 0.125 inches thickness
  • 4920-01-499-7080 next higher assembly identification designator
  • target control system end application
  • bunk station 41 aircraft location
  • b-52h acft aircraft mission design series
  • c-17a aircraft end application
  • c-17a aircraft end application
  • e-8 aircraft joint stars end application
5HC13135-115 NSN 1680-01-539-5147
901-031-150-286 Panel NSN 1680-01-540-7173
  • cv-22 aircraft end application
901-031-150-281 Panel NSN 1680-01-540-7174
  • cv-22 aircraft end application
901-031-150-289 Panel NSN 1680-01-540-7176
  • cv-22 aircraft end application
900-18195-4 Cv-22 Aircraft NSN 1680-01-540-8268
  • panel end application
  • c-17acft end application
  • effectivi type 17a033-059 and on special features
  • c-17 aircraft mission design series
  • aluminum alloy material
  • qq-a-250/13 federal specification 1st material response material specification
  • cv-22 aircraft end application