01-173-5460
Aircraft Former
01-173-5461
Aircraft Former
01-173-5462
Aircraft Former
01-173-5463
Aircraft Former
01-173-5464
Aircraft Former
01-173-5465
Aircraft Former
01-173-5466
Aircraft Former
01-173-5469
Aircraft Spar
Used to support center wing structure
01-173-5629
Fluid Aircraft Manifold
8.360" overall length 1.31 in. dia end contains 3 0.218 in. dia holes with nutplates on flange
01-173-5630
Fluid Aircraft Manifold
8.486" overall length 7.016" overall width 1 0.027 in. dia hole along machined boss
01-173-5631
Fluid Aircraft Manifold
8.286" overall length 7.016" overall width 1 0.027 in. dia hole along machined boss
01-173-5632
Fluid Aircraft Manifold
10.670" overall length 10.120" overall width 6 0.257 in. dia equally spaced holes in one end fitting
01-173-5633
Fluid Aircraft Manifold
32.300" overall length 23.660" overall width contains gusset between forks on end
01-173-5634
Fluid Aircraft Manifold
11.600" overall length 6.000" overall width
01-173-5731
Structural Aircraft Panel
Used on ah-1 series helicopter.
01-173-5848
Fuselage Aircraft Fairing
01-173-5849
Fuselage Aircraft Fairing
01-173-6001
Structural Component Air Support
C/o 1 spar, 1 core, 1 rub strip, 1 skin, 1 doubler, laminated build-up
01-173-6063
Structural Aircraft Plate
Used on acft model a-10. 0.071 sheet aluminum alloy 6061-T6 per qq-a-250/11, 2.900 in. lg o/a
01-173-6067
Structural Aircraft Plate
Chloroprene, impregnated cotton duct laminated, mil-d-882 class i
01-173-6069
Aircraft Fairing
32.000" overall length 8.000" overall width 0.040" material thickness
01-173-6070
Structural Component Air Support
Used on acft model a-10. aluminum alloy sheet per qq-a-250/11 6061-T6, 9.900 in. lg. o/a
01-173-6089
Aircraft Former
6.000" overall length 4.380" overall width
01-173-6090
Aircraft Former
6.000" overall length 4.380" overall width
01-173-6091
Aircraft Former
17.000" overall length 4.000" overall width 2.000" material thickness
01-173-6958
Aircraft Fairing
16.770" overall length 0.500" material thickness
01-173-7410
Structural Aircraft Plate
Used on acft model c-135. aluminum alloy clad per qq-a-362 2024-0, 2.200 in. lg, 0.800 in. w, 0.040 in. thk
01-173-7412
Structural Component Air Support
Used on acft model b-1b. fitting machined from al alloy bar 7075-T73511 per qq-a-200/11; 2.490 in. lg, 1.600 in. w at base, 0.905 in. w at clevis, 1.804 in. h; clevis holes 0.500 in. dia; c/o 1 -003 fitting
01-173-7413
Structural Component Air Support
Used on acft model b-1b. al precision forging, alloy 7075-T73; 5.930 in. o/a lg, 3.000 in. o/a w, 4.180 in. o/a h; clevis like projection without holes 1.000 in. w, 0.408 in. slot; 2 0.257 in. dia holes 1.000 in. apart in base arm; 4 0.316 in. dia holes in corners of retangular part ofbase; nha L6311083
01-173-7414
Structural Component Air Support
Used on acft model b-1b. corrosion resistant steel investment casting 17-4 ph per AMS5342; 4.290 in. lg, 2.880 in. o/a w, 1.650 in. o/a thk, 2.520 in. between clevis forks; 2 in line holes in clevis 0.375 in. dia; c/o 1 -005 support
01-173-7415
Structural Component Air Support
Used on acft model b-1b. lal alloy 7075-T73 per qq-a-200/11; 2.000 in. lg, 1.880 in. w, 0.805 in. h; 2 0.098 in. dia pilot holes in base; 5/16 in. hole upper section, .560 in dia 10aa finish around hole both sides; nha L6311083
01-173-7417
Structural Component Air Support
Used on acft model b-1b. val alloy 7075-T73511 per qq-a-200/11; 3.600 in. lg, 0.900 in. w, 1.062 in. h; clevis one end perpendicular to lg, slot w 0.500 in., 2 0.25 in. dia holes in line; shim on back opposite end 1.820 in. lg; nha L6311083; opposite p/n -002
01-173-7418
Structural Component Air Support
Used on acft model b-1b. wal alloy 7075-T73511 per qq-a-200/11; 3.600 in. lg, 0.900 in. w, 1.062 in. h; clevis one end perpendicular to lg, slot w 0.500 in., 2 0.250 in. dia holes in line; shim on back opposite end 1.820 in. lg; nha L6311083; opposite p/n -001
01-173-7419
Structural Component Air Support
Used on acft model b-1b. al alloy 7075-T7351 per qq-a-200/11; c/o 1 -003 bracket, 1 L6310106-003 bracket, 1 L6310104-003 fitting, and assorted rivets; nha L6311583
01-173-7420
Structural Component Air Support
Used on acft model b-1b. al alloy 7075-T7351 per qq-a-225/9; c/o 1 -003 bracket, 1 L6310104-003 fitting, 1 L6310106-003 fitting, asorted rivets; nha L6311583
01-173-7423
Aircraft Former
Used on acft model c-135.
01-173-7424
Aircraft Former
Used on acft model c-135.
01-173-7425
Aircraft Former
01-173-7426
Aircraft Former
Used on acft model c-135.
01-173-7427
Aircraft Former
Used on acft model c-135.
01-173-7428
Longeron
Used on aircraft,model c-135.
01-173-7429
Aircraft Skin
Used on acft model c-135.
01-173-8631
Structural Component Air Bracket
Opp -10; heat treat H1000; finish 60HA01; nha L1702000
01-173-8632
Structural Component Air Bracket
36.760" overall length make L9170031-003; heat treat 190-210 ksi; nickel plated milc-c-26074; opp-010; nha L1702000
01-173-8633
Structural Component Air Bracket
35.100" overall length make L9170031-003; heat treat 190-210 ksi; nickel plated mil-c-26074; opp-010; nha L1702000
01-173-8634
Structural Component Air Bracket
Nickel plated mil-c-26074, class i; heat treat 190, 000-210, 000 psi; opp -009; nha L1702000
01-173-8635
Structural Component Air Bracket
Make L9170032-003; heat treat STO111LA0002 to 190, 000-210, 000 psi; opp --14; nha L1702000
01-173-8636
Structural Component Air Bracket
Make L9170035-003; heat treat 190, 000-210, 000; opp -006; nha L1700000
01-173-8637
Structural Component Air Bracket
Make L19170035-003; heat treat 190, 000-210, 000 psi; opp -006; nha L1700000
01-173-8638
Structural Component Air Bracket
Make from L9170038-003; heat treat 190-210 ksi; opp -006; nha L1702000
