01-544-2312
Aircraft Skin
01-544-2317
Structural Component Aircraf Web
01-544-2321
Structural Component Aircraf Web
01-544-2324
Aircraft Skin
01-544-2325
Structural Component Air Support
01-544-2377
Structural Component Air Fitting
Fitting, panel, aft
01-544-2403
Aircraft Spar
01-544-2404
Structural Aircraft Plate
01-544-2406
Aircraft Spar
01-544-2407
Structural Component Air Support
01-544-2409
Structural Aircraft Plate
01-544-2520
Structural Component Air Support
Used on KC-135. support angle opposite -70; dimensions are stock sized bac 1503-1509 x 2
01-544-2525
Structural Component Air Support
Used on KC-135. kc-135 dim are stock sized bac 1503 - 2811 x .80
01-544-2529
Structural Component Air Support
Used on KC-135. rib 1&2 attach angle dim are stock sized bac 1503-1491 x 1.70
01-544-2532
Structural Component Air Support
Used on KC-135. support angle opposite -59; dim are stock sized bac 1490-2561 x 2.60
01-544-2543
Structural Aircraft Plate
Used on KC-135. 0.600" overall length 0.400" overall width 0.001" material thickness filler heat treat T3
01-544-2555
Structural Aircraft Plate
Used on KC-135. 1.500" overall length 1.400" overall width 0.040" material thickness gusset heat treat T3
01-544-2557
Structural Component Air Support
Used on KC-135. rib chord-upper dim are stock sized alter bac 1503 - 2719 x 31.90
01-544-2561
Aircraft Stiffener
Used on KC-135. stiffener alter bac 1490 - 2728 x 6.2 lg
01-544-2562
Structural Component Air Support
Used on KC-135. support angle bac 1490-2561 x 2.80
01-544-2616
Fuselage Aircraft Fairing
438.000" overall length 48.000" overall width
01-544-2618
Fuselage Aircraft Fairing
01-544-2619
Aircraft Channel
01-544-2621
Structural Aircraft Plate
Divider
01-544-2623
Fuselage Aircraft Fairing
438.000" overall length 48.000" overall width
01-544-2625
Aircraft Channel
01-544-2626
Fuselage Aircraft Fairing
01-544-2628
Structural Aircraft Plate
Divider
01-544-2664
Aircraft Slat
01-544-2665
Aircraft Slat
01-544-2675
Structural Component Air Support
Support make from -7 (identical except for surface treatment) , nha:17P6P5502
01-544-2676
Structural Component Air Support
Support make from -6 (identical except for surface treatment) ; nha:17P6P5502
01-544-2677
Structural Aircraft Panel
Used on f-22 raptor.
01-544-2728
Structural Aircraft Plate
Filler
01-544-2732
Structural Aircraft Plate
4.800" overall length 0.800" overall width 0.078" material thickness filler dim. are stock material
01-544-2733
Stiffener Aircraft Rib
01-544-2742
Structural Component Aircraf Web
Bonded web
01-544-2757
Structural Aircraft Plate
4.800" overall length 3.900" overall width 0.032" material thickness doubler-access door dim. are stock material
01-544-2763
Structural Component Air Support
8.300" overall length chord lower-trailing beam
01-544-2781
Structural Component Air Support
8.300" overall length chord, upper-trailing edge beam
01-544-2788
Structural Aircraft Plate
2.000" overall length 1.100" overall width 0.080" material thickness filler dim. are stock material
01-544-2801
Structural Aircraft Plate
1.100" overall length 0.500" overall width 0.080" material thickness filler dim. are stock material
01-544-2811
Aircraft Skin
Skin-inner
01-544-2823
Aircraft Truss Assembly
Make from 25-2113 forging or optional 7079 aluminum forged block per qq-a-367
01-544-2830
Structural Component Air Support
49.500" overall length 4.200" overall width 0.091" material thickness chord lower dim. are stock material
01-544-2892
Aircraft Hinge
01-544-2893
Structural Aircraft Plate
01-544-3001
Aircraft Wing Assembly
01-544-3210
Structural Component Air Support
Support make from -7; nha: 17P6P5501
