01-504-9211
Structural Component Air Support
Used on l-1011 tristar.
01-504-9229
Structural Component Air Support
Used on l-1011 tristar.
01-504-9231
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9235
Structural Component Air Support
Used on l-1011 tristar.
01-504-9236
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9240
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9243
Structural Component Air Support
Used on l-1011 tristar.
01-504-9248
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9251
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9253
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9254
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9255
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9260
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9262
Structural Aircraft Panel
Used on l-1011 tristar.
01-504-9354
Structural Component Air Support
01-504-9792
Structural Aircraft Panel
49.000" overall length 8.000" overall width ramp side rail heat treat per STP54-101, material thickness 0.063; dim are stock matl
01-504-9793
Structural Aircraft Panel
49.000" overall length 8.000" overall width ramp side rail heat treat per STP54-101, materialthickness 0.063; dim are stock matl
01-505-0056
Structural Component Air Bracket
01-505-0080
Structural Component Fitting Set
Fitting assembly
01-505-0206
Aircraft Windshield Assembly
01-505-0224
Structural Component Air Bracket
01-505-0235
Structural Component Air Bracket
01-505-0250
Structural Aircraft Plate
01-505-0254
Structural Aircraft Plate
01-505-0288
Structural Component Air Bracket
Used on tornado. mounting plate assembly, rh
01-505-0290
Structural Component Air Bracket
Used on tornado. mounting plate assembly, lh
01-505-0373
Aircraft Fairing
Fairing assy, translating-te effectivy from 17A107-184; nha 17P625350; c/o 1 p/n -11 cap, AMS4902, .040X4X5 sheet, stocksize; rivets (ar) ; 2 p/n -21 strips, .032 x 1 x 21 stocksize, sheet, ams-t-9046, comp cp-3 cond annealed; 1 p/n -23 shin, .040 x 11 x 29 sheet stocksize; 1 p/n -25 channel, .040 x 5 x 24 sheet stocksize; 1 p/n -31tube sub assy.
01-505-0374
Aircraft Fairing
Fairing assy, translating te effective from 17A106; nha 17P6W5350; same as -503 except where shown; c/o rivets (ar) ; 1 channel, p/n -19, .040 x 5 x 24 sheet; 2 strips, p/n -21, .032 x 1 x 21 sheet; 1 cap p/n -9, .040 x 4 x 5 sheet; 1 -11 cap, .040 x 4 x 5 sheet; 1 skin p/n -13, .040 x 11 x 29 shet; 1 cap -15, .040 x 4 x 5 sheet; dimensions are stocksize
01-505-0467
Structural Component Air Support
41.200" overall length tee nha L2300390 u/o b-1b 1
01-505-0472
Structural Aircraft Plate
Used on forward engine shroud nacelle. 5.300" overall length 1.900" overall width 0.020" material thickness clip hres AMS5542 inconel x-750; thermal treat-inconel h-T101
01-505-0474
Structural Component Air Support
41.200" overall length tee nha L2300390 u/o b-1b 1
01-505-0506
Structural Aircraft Plate
Used on forward engine shroud nacelle. 5.500" overall length 1.000" overall width 0.020" material thickness clip cres, AMS5542, inconel x-750; thermal treat - inconel HT101
01-505-0515
Structural Aircraft Plate
Used on forward engine shroud nacelle. 5.500" overall length 1.000" overall width 0.020" material thickness clip hres, AMS5542, inconel x-750; thermal treat-inconelh-T101
01-505-0520
Structural Aircraft Plate
Used on forward engine shroud nacelle. 5.300" overall length 1.900" overall width 0.020" material thickness clip hres, AMS5542, inconel x-750; themal treat-inconel h-T101
01-505-0522
Structural Aircraft Plate
Used on forward engine shroud nacelle. 5.300" overall length 1.900" overall width 0.020" material thickness clip hres, AMS5542, inconel x-750; themal treat-inconel h-T101
01-505-0524
Structural Aircraft Plate
Used on forward engine shroud nacelle. 5.300" overall length 1.900" overall width 0.020" material thickness clip hres, AMS5542, inconel x-750; thermal treat-inconel h-T101
01-505-0541
Structural Aircraft Plate
01-505-0578
Aircraft Skin
Used on main landing gear wheel well skin for the c130 hercules.
01-505-0665
Access Aircraft Cover
Cover assy, access-outbd pylon-wing stub c/o 1 retainer plate, make from S124682-2D10-6; 1 door stock size .160X10X10, heat treat T6, sub p/n HL327-6-7, pin; 18 nut's p/n MS21042L08
01-505-0668
Aircraft Fairing
Fairing assy, translating, wg stub supersedes -511; effectivity 17A107-17A999; annealed (formerly mil-t-9046) ; c/o 1 bracket, 1 fairing assy, 2 filler, 1 tube assy, 2 guide assy, 2 bracket assy, 2 panels, 3 former assy, 1 bulkhead, misc. hardware, pin (ar) , rivets (ar) , 10 clips, 15 fastener
01-505-0671
Aircraft Door
Door assy, anti-icing, slat 2 rsupercedes -501, same except ecn chgs.; c/o 1 (-7) door, .100 x 8.0 x 21.0, 4 angles p/n 17P6N1029-517, -518, -519, -521, 4 angles p/n 17P6N1058-501, misc. hardware; alclad sheet; effectivity from 17A086-124; nha 17P6N1002
01-505-0673
Structural Aircraft Panel
Panel instl-structural, inbd trailing edge, outbd flap e/o parts list revision -503 same -501; c/o 14 nuts, make from MS21063L3-10; 1 shear clip stock size .125X4X7, sheet glass re-enforced plastic phenolic, 1 shim
01-505-0674
Structural Aircraft Panel
Panel instl-structural, inbd trailing edge; outbd flap wper e/o parts list revision, -504 same as -502, except 24 nuts p/n NAS1329C08-75, 5 nutplates make from MS21063L3-10; shear clip stock size .125X4X7, alclad 2024-T3, 1 shim stock size .065X1.5X7.25; sheet glass reinforced phenloic
01-505-0675
Structural Aircraft Panel
Panel instl-structural, outbd trailing edge, outbd flap c/o 1 doubler stock size .125X4X5; 14 shim stock size .065X1.5X9; 1 te assy; 4 washer, 4 bolts, 104 screws; 5 blind rivet, 56 rivet; per e/o parts list revision -505 same as -503
01-505-0760
Airframe Modification Kit
01-505-0761
Airframe Modification Kit
01-505-0827
Structural Aircraft Plate
2.500" overall length 1.750" overall width clip nha L2300360 u/o b-1b 1
01-505-0842
Structural Component Air Support
01-505-0862
Structural Component Air Support
01-505-0866
Structural Component Air Support
Clevis support, latch fwd & aft pylon opposite A02S8079-10
