01-541-4296
Explosion Suppressa Foam Segment
9.800" overall length 1.100" overall width void filler m/o thermarest AX5052, per avco spec M10462
01-541-4303
Explosion Suppressa Foam Segment
Void filler m/o thermarest AX5052, per avco spec M10462
01-541-4307
Explosion Suppressa Foam Segment
Void filler m/o thermarest AX5052, per avco spec M10462
01-541-4314
Explosion Suppressa Foam Segment
19.750" overall length void filler m/o thermarest AX5052, per avco spec M10462
01-541-4400
Aircraft Skin
42.500" overall length 32.500" overall width skin-top same as -9 except for material, add 0.25 excess to all edges, for spares only; nha 3-12201; heat treat T3
01-541-4419
Aircraft Window Panel
Used on f111 aircraft. canopy assembly
01-541-4504
Door Aircraft Parts Kit
Used on C-17A. kit used to repair or modify otbd mlg door hinges; kit consists of patch assys, 7 x 12 ply fabric carbon fiber woven b-stage epoxy impregnated dms type 2 class 2 grade c; tape patch; hinge assys; washers; nut; bolts
01-541-4707
Aircraft Skin
Used on A-10. 100.000" overall length 38.000" overall width outer skin instl heat treat T0
01-541-4714
Aircraft Skin
Used on A-10A. 100.000" overall length 38.000" overall width outer skin instl heat treat T0
01-541-4787
Aircraft Skin
Used on A-10. 100.000" overall length 38.000" overall width outer skin instl heat treat 0
01-541-4804
Aircraft Skin
Used on A-10A. 100.000" overall length 38.000" overall width outer skin instl heat treat T0
01-541-4806
Structural Component Air Support
Used on A-10A. support
01-541-4813
Aircraft Spar
Used on A-10A. rear spar
01-541-4950
Aircraft Window Panel
Used on f111 aircraft. canopy assembly
01-541-4997
Structural Component Aircraf Web
Used on KC-135. bonded web assy oppoiste -50; bond per bac 5425
01-541-5014
Aircraft Pylon
Pylon
01-541-5079
Structural Component Air Bracket
Used on f-22 raptor.
01-541-5080
Structural Component Air Bracket
Used on f-22 raptor.
01-541-5082
Structural Component Air Bracket
Used on f-22 raptor.
01-541-5083
Structural Component Air Bracket
Used on f-22 raptor.
01-541-5084
Structural Component Air Bracket
Used on f-22 raptor.
01-541-5085
Structural Component Air Bracket
Used on f-22 raptor.
01-541-5086
Structural Component Air Fitting
Used on f-22 raptor.
01-541-5087
Structural Component Air Bracket
Used on f-22 raptor.
01-541-5088
Structural Component Air Bracket
Used on f-22 raptor.
01-541-5117
Structural Aircraft Plate
Used on arr list code; cover installation; f/a-18e model code to support ecp 6038. (navy) spacer, plate
01-541-5118
Structural Aircraft Plate
Used on arr list code;cover installation;f/a-18e&f model code to support ecp 6038. navy name is spacer, plate smic is qf, which is non-critical
01-541-5119
Radome
Used on support. navy name is bushing
01-541-5122
Structural Component Air Support
Used on support; fuselage assembly; stuctural assembly; f/a-18e moodel code to support ecp 6038; f/a-18f model code in support of ecp 6038. (navy) support
01-541-5158
Radome
Used on radome assemlby; arr list code; first pbl; f/a-18e model code to support ecp 6038. (navy) radome assembly
01-541-5176
Radome
Used on cable assembly, radi;ainac/ric au llirlh300;arr list code;first pbl;radome assembly. cable assembly, ra smic is qe, which is non-critical
01-541-5179
Radome
Used on arr list code;first pbl;radome assembly;roller assembly. navy name is roller fsc represents airframe structural components
01-541-5224
Aircraft Latch Assembly
Used on fighter aircraft (f18 e/f); arr list code. 1.600" overall length 1.063" overall width navy: latch assembly, aircraft; dwg: latch assembly - push button, heavy duty, adjustable bolt push button; heavy duty; adjustable bolt
01-541-5261
Aircraft Skin
Used on skin; skin assembly; f/a-18e model code to support ecp 6038; f/a-18f model code in support of ecp 6038. (navy) skin
01-541-5440
Stiffener Aircraft Rib
Rib assy nha 160D611101
01-541-5566
Structural Component Air Support
Used on A-10A. 14.000" overall length 2.500" overall width 0.050" material thickness angle alcd sheet; used on -5 frame assy; effectivity 1
01-541-5615
Tubing Aircraft Support
Used on f-22 raptor.
01-541-5616
Structural Aircraft Panel
Used on f-22 raptor. louver
01-541-5618
Tubing Aircraft Support
Used on f-22 raptor.
01-541-5619
Structural Aircraft Panel
Used on f-22 raptor. louver
01-541-6180
Structural Component Air Support
Used on A-10A. 14.000" overall length 2.500" overall width 0.050" material thickness angle alcd sheet; used on frame assy, effectivity 1
01-541-6182
Structural Aircraft Plate
Used on A-10. 2.000" overall length 0.800" overall width 0.090" material thickness link
01-541-6183
Aircraft Spar
Used on A-10. 61.000" overall length 4.000" overall width 0.016" material thickness rear spar heat treat T3; dim. are stocksize; alcd sheet
01-541-6190
Structural Component Air Fitting
Used on F-16. 15.000" overall length 6.500" overall width 1.500 " material thickness fitting nha 16B6806; alternat stock size maybe fabricated from 4.000 x 6.5 x 15 plate stock; spec fms-4097-T861
01-541-6194
Structural Component Air Fitting
Used on F-16. 15.000" overall length 6.500" overall width 1.500 " material thickness fitting nha 16B6806 alternate stock size maybe fabicated from 4.000 x 6.5 x 15.plate stock; spec fms-4097-T861
01-541-6250
Access Aircraft Door
Used on f-15 acft. access-lower ics FS481.53-497.04
01-541-6253
Aircraft Fairing
01-541-6254
Aircraft Fairing
01-541-6267
Structural Component Air Fitting
Arm
01-541-6295
Aircraft Windshield Panel
Used on sf111 aircraft.
