01-541-6296
Aircraft Windshield Panel
Used on sf111 aircraft.
01-541-6602
Tubing Aircraft Support
Used on f-22 raptor. m/o 6013 aluminum
01-541-6636
Structural Aircraft Panel
01-541-6730
Aircraft Fairing
Used on F-15. 6.100" overall length 1.600" overall width 0.020" material thickness clip (lh) used on -8 rh fairng assy; (opposite -16 lh used on -7 lh fairing assy) ; cres sh cond a
01-541-6966
Structural Component Air Bracket
Used on f-22 raptor. bracket
01-541-6967
Structural Component Air Bracket
Used on f-22 raptor. bracket
01-541-6968
Structural Component Air Bracket
Used on f-22 raptor. bracket
01-541-6971
Tubing Aircraft Support
Used on f-22 raptor. support tubing
01-541-6972
Structural Component Air Support
Used on f-22 raptor. support
01-541-6973
Tubing Aircraft Support
Used on f-22 raptor. 4.000" overall length 3.000" overall width 0.063" material thickness support dim. are stock material; m/f: 6013-T4 alum sht, final cond T6
01-541-6974
Structural Component Air Fitting
Used on f-22 raptor. fitting
01-541-6975
Tubing Aircraft Support
Used on f-22 raptor. support tubing
01-541-6978
Structural Aircraft Plate
Used on f-22 raptor. plate
01-541-6979
Structural Aircraft Plate
Used on f-22 raptor. splice
01-541-6991
Airfoil Rib
Used on c/kc-135. 7.300" overall length 4.600" overall width 0.056" material thickness opposite -2; sheet clad; heat treat 0; finish srf-2.30; c/o -3 rib, 69-45274-3 nose rib, rivet-blind
01-541-7015
Door Aircraft Hinge
Hinge m/f extrusion 160D412036-3
01-541-7032
Structural Component Air Fitting
Fitting
01-541-7034
Structural Component Air Fitting
Fitting
01-541-7196
Aircraft Channel
01-541-7197
Aircraft Channel
01-541-7353
Structural Aircraft Plate
33.000" overall length 5.000" overall width 0.091" material thickness rib doubler matl al 2024-0 sht qq-a-355 0 temp; -1 opp; u/o 1150-3118
01-541-7378
Structural Component Air Support
Spar nha 160D712171; heat treat T76511
01-541-7391
Structural Component Air Support
Used on A-10. 2.500" overall length 2.100" overall width 0.040" material thickness clip heat treat T3
01-541-7472
Door Aircraft Hinge
Used on C-17A. 7.000" overall length 5.000" overall width 3.500" material thickness hinge c/o 1 (bushing m/f 54928911-8A038) , 1 fitting 3.5 x 5 x 7 gr lgwise; heattreat T7451 alum plate, fatique qualified; DMS2459; dim. are stock matl
01-541-7496
Structural Component Air Support
53.600" overall length retainer matl al 2024-T4, qq-a-362; opp -43; dim are stock material
01-541-7555
Structural Component Air Support
01-541-7560
Structural Component Air Support
01-541-7589
Structural Component Air Fitting
Fitting
01-541-8013
Structural Aircraft Plate
Used on f-22 raptor. 7.000" overall length 5.000" overall width 2.500" material thickness splice dim. are stock material; m/f: 6al-4v ann titanium plate
01-541-8015
Structural Aircraft Plate
Used on f-22 raptor. plate
01-541-8033
Structural Aircraft Plate
Used on f-22 raptor. 31.000" overall length 15.000" overall width 3.000" material thickness louver m/f -108 louver; heat treat T8151; alum plate; -116 maybe used for replacment except see attach.method; can be used as replacement for -106 or -102 except see attach method
01-541-8034
Structural Component Air Bracket
Used on f-22 raptor. 3.000" overall length 2.000" overall width 0.063" material thickness bracket, assy of c/o 1 (-199 bracket) , 2 rivet, 1 nut
01-541-8036
Airfoil Rib
Rib matl al 7075 qq-a-362 T42; opp-2
01-541-8037
Airfoil Rib
Used on kc-135 aircraft. rib matl al 2024, qq-a-362
01-541-8038
Airfoil Rib
4.400" overall length 1.700" overall width rib matl al 2024 qq-a-362; dim are stock matl
01-541-8039
Structural Component Air Bracket
Used on f-22 raptor. 2.000" overall length 2.000" overall width 0.050" material thickness bracket assy c/o 1 (-201 bracket) , 1 nut, 2 rivet; ann titanium sheet; -102 opposite
01-541-8040
Door Aircraft Hinge
Used on C-17A. 8.800" overall length 4.250" overall width 3.120" material thickness hinge opposite -503; effectivity 17A164-17A999; nha 17P2A3901; c/o 1 (-15 fitting, 3.5 x 5 x 9.5 gr lgwise, DMS2459 plate fatique qualified T7451 AL7050; dim. are stock matl
01-541-8443
Airfoil Rib
Opposite -2
01-541-8447
Access Aircraft Door
Used on C-17A. door, access same as -217 except; u/o -515; -222 opposite; c/o 2 latch assy, 1 door (-223) , 8 bolt, 8 washer flat, 8 nut, ar washer
01-541-8461
Structural Component Air Bracket
Used on f-22 raptor. 10.000" overall length 4.000" overall width 0.071" material thickness bracket c/o 1 (-570 bracket) , ref (bracket 5HF71081 & 5HF71082) , 2 nut, 4 rivet; opposite -519
01-541-8462
Structural Component Air Bracket
Used on f-22 raptor. 10.000" overall length 4.000" overall width 0.071" material thickness bracket c/o 1 (-570 bracket) , ref (5HF71081& 5HF71082 bracket) , 2 nut, 4 rivet; opposite -519
01-541-8463
Structural Component Air Bracket
Used on f-22 raptor. 9.000" overall length 3.000" overall width bracket assy c/o 1 (-283 bracket) , 8 nut, 16 rivet; ann titanium sheet
01-541-8464
Structural Component Air Bracket
Used on f-22 raptor. 3.000" overall length 2.000" overall width 0.063" material thickness bracket assy c/o 1 (-204 bracket) , 1 nut, 2 rivet; ann titanium sheet
01-541-8633
Aircraft Fairing
Cover, drum housing technical document 25-00-19-1
01-541-8638
Aircraft Fairing
Fairing motor technical document 25-00-19-1
01-541-8651
Aircraft Fairing
Fairing, levelwind technical document 25-00-29-1
01-541-8719
Aircraft Former
Used on f/a-18;seal-lower, l.e. flap, instl. navy-former, aircraft
01-541-8720
Structural Component Air Fitting
Used on F/A-18. navy-clip
01-541-8733
Structural Component Air Bracket
Used on f-22 raptor. bracket assy effectivity A4001-A4999; opposite-102; c/o 1 (-201 bracket) , 1 nut, 2 rivet; ann titanium sheet
