01-178-0406
Structural Aircraft Panel
01-178-0441
Aircraft Wing Assembly
01-178-0452
Structural Aircraft Plate
01-178-0453
Structural Aircraft Plate
01-178-0456
Structural Component Air Support
Used on acft model kc-135. al alloy 2024-T3511 per qq-a-200/3; finish f-2.16; 6.200 in. lg; nha 35-35420 turbo compressor deletion installation
01-178-0457
Structural Component Air Support
Used on acft model kc-135. innconel 625 sheet per ams 5599, annealed; finish f-25.01; stock size 8.100 in. lg, 4.700 in. w, 0.063 in. thk; nha 39-28098-3 support assembly
01-178-0458
Structural Component Air Support
Used on acft model a-10. aluminum alloy forging per qq-a-367 7075-T73, fittings are replaceable items iaw mil-i-8500 for replaceable configurations see dwg no. NR160J1101
01-178-0472
Wing Landing Flap
Used on F-111. spared for flap installation
01-178-0473
Aircraft Former
Same as -33; nha 65-10506
01-178-0475
Aircraft Tip
Used on FB-111. c/o approximately 15 components, use only on 12W5151-835
01-178-0476
Aircraft Tip
Used on FB-111. c/o approximately 15 components use only on 12W5151-836
01-178-0477
Aircraft Tip
Used on F-111. c/o 3 ea. retainer precipitation static discharger
01-178-0489
Thermal Special Purpo Insulation
Pad-bulkhead, canted, main landing gear, fuselage section; end item identification:aircraft, model f-111
01-178-0992
Aircraft Slat
01-178-1011
Aircraft Wing Assembly
01-178-1031
Structural Aircraft Plate
Used on acft model kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; stock size 5.500 in. lg, 4.400 in. w, 0.050 in. thk; semi-circular shaped; 4 0.229 in. dia holes; nha 35-35434
01-178-1032
Structural Aircraft Plate
Used on acft model kc-135. corrosion resistant steel per ams 5537; finish f-8.05; 28.500 in. lg, 3.400 in. w, 0.040 in. thk; nha 65-16032-33, -34, -51
01-178-1033
Structural Aircraft Plate
Used on acft model kc-135. al alloy clad sheet 2024-T3 per qq-a-200/3; 8.510 in. lg, 3.600 in. w, 0.050 in. thk, 1.800 in. radius both ends; 12 holes for 6/32 in. dia bolts; curved to 11.54 in. radius
01-178-1034
Structural Component Air Support
2024-T3511 alum al; 1.880 in lg; 1.600 in w; 1.290 in h; two 0.375 dia holes inline; rtsegopposite of 78286/65201-042
01-178-1035
Structural Component Air Support
2024-T3511 alum al; two 0.375 dia holes inline; 1.880 in l; 1.600 in w; 1.290 in h
01-178-1040
Structural Component Air Support
Used on acft model b-1b. consist of 3 brackets, 1 rivet a/r; nha L3010083; located at 275.8
01-178-1041
Structural Component Air Support
Used on acft model kc-135. steel aisi 17-4ph per ams 5355; made from -801 investment casting; heat treated to 180-210 ksi per bac 5619; c/o 2 high-temp bearings, 1 bracket, 2 bearing retainers; bracket finish f-8.07
01-178-1042
Structural Component Air Support
Used on acft model kc-135. dc/o 2 high-temp bearings, 1 bracket, 2 bearing retainers, 1 key; bracket finish f-8.07; steel aisi 17-4ph perams 5355; heat treated 180-210 ksi per bac 5619; bracket made from -801 investment casting
01-178-1043
Structural Component Air Support
Used on acft model b-1b. steel alloy 9ni-4co-.20c bar; stock size 2.750 in. lg, 1.750 in. w, 1.380 in. thk; nha L8800102
01-178-1044
Structural Component Air Fitting
Used as side support attachment fitting on apu; 2.750 lg, 1.750 wd at base; 1.429 o/a h, 0.240 thk at base; 0.871 dia projection w/0.422 dia thru hole centered on bottom; 2 .3125 dia in-line holes opposite side; nha L8700002
01-178-1045
Structural Component Air Support
01-178-1049
Structural Aircraft Panel
C/o 3 skins, 2 cores, 1 closeout; opposite -001; nha L1200901
01-178-2686
Structural Aircraft Plate
Nha 69-1062-11
01-178-2705
Structural Aircraft Plate
Used on acft model kc-135. corrosion resistant steel sheet aisi 17-7ph per mil-s-25043, annealed surface cond 2d; surface finish f-12.206; stock size 4.200 in. lg, 0.600 in. w, 0.040 in. thk; heat treated 180-200 ksi; nha 65-69413
01-178-2706
Structural Aircraft Plate
32.500" overall length 0.500" overall width 0.040" material thickness c/o 1 strip, 15 welded studs; nha 65-1348
01-178-2707
Structural Aircraft Plate
6.000" overall length 3.500" overall width 0.063" material thickness nha 69-38511
01-178-2710
Structural Component Air Bracket
C/o 1 bracket, 2 strap; nha 69-25973
01-178-3469
Structural Aircraft Panel
01-178-3470
Structural Aircraft Panel
01-178-3502
Structural Component Air Support
Used on acft model c-135.
01-178-3503
Structural Component Air Bracket
10.800" overall length 5.100" overall width 0.080" material thickness finish f-12.206; nha 69-3777-2
01-178-3504
Structural Component Air Bracket
9.900" overall length 4.000" overall width 0.080" material thickness finish f-12.206; nha 69-37772
01-178-3505
Structural Component Air Fitting
3.700" overall length 1.960" overall width 0.620 " material thickness heat treat 180-200 ksi; finish f-12.205; make from -1; nha 69-38514-1
01-178-3508
Structural Aircraft Panel
C/0 beams, spacers & mtg hardware
01-178-3509
Structural Aircraft Panel
C/o beams, spacers
01-178-3510
Structural Aircraft Panel
C/o beams, fittings
01-178-3519
Aircraft Former
19.500" overall length 16.000" overall width 0.071" material thickness heat treat T42; finish f-2.30; nha 204-70011-1
01-178-3520
Aircraft Former
17.500" overall length 13.500" overall width 0.063" material thickness heat treat T42; finish f-2.30; nha 204-70011-1
01-178-3521
Aircraft Leading Edge
01-178-3527
Aircraft Skin
28.000" overall length 24.000" overall width finish srf 14.011 plus srf 12.205 to skin lap area; nha 204-70011-1
01-178-3528
Aircraft Skin
26.000" overall length 15.000" overall width finish srf 14.011 plus srf 12.205 to skin lap area; nha 204-70011-1
01-178-3529
Aircraft Skin
13.000" overall length 6.000" overall width finish srf 14.011 plus srf 12.205 to skin lap area; nha 204-70011-1
01-178-5073
Access Aircraft Door
01-178-6282
Aircraft Windshield Panel
01-178-6296
Fluid Aircraft Manifold
2.800" overall length
