01-173-8639
Structural Component Air Bracket
Make L9170038-003; heat treat 190, 000 to 210, 000 psi; opp -006; nha L1700000
01-173-8640
Structural Component Air Bracket
Make from L9170038-003; heat treat 190, 000-210, 000 psi; opp -10; nha L1702000
01-173-8641
Structural Component Air Bracket
43.000" overall length make L9170026-003; heat treat 190-210 ksi; nickel plated mil-c-26074; opp-013; nha L1702000
01-173-8642
Structural Component Air Bracket
41.940" overall length make L9170026-003; heat treat 190-210 ksi; nickel plated mil-c-26074; opp -009; nha L1702000
01-173-8643
Structural Component Air Bracket
40.460" overall length make from L9170026-003; heat treat 190-210 ksi; nickel plated mil-c-26074; nha L1702000; opp -009
01-173-8644
Structural Component Air Bracket
38.720" overall length make L9170031-003; heat treat 190-210 ksi; nickel plated mil-c-26074; opp -013; nha L1702000
01-173-8645
Structural Component Air Bracket
36.760" overall length make L9170031-003; heat treat 190-210 ksi; nickel plated mil-c-26074; opp-009; nha L1702000
01-173-8646
Structural Component Air Bracket
35.100" overall length make L9170031-003; heat treat 190-210 ksi; nickel plated mil-c-26074; opp-009; nha L1702000
01-173-8647
Structural Component Air Bracket
Nickel plated mil-c-26074 class i; heat treat 190, 000-210, 000 psi; opp -009; nha L1702000
01-173-8648
Structural Component Air Bracket
Made from L9170032-003; heat TREATST0111LA0002 to 190, 000-210, 000; opp -13; nha L1702000
01-173-8649
Structural Component Air Bracket
Opp -009; heat treat T0H1000; finish 60HA01; nha L1702000
01-173-8650
Structural Component Air Bracket
Make from L91700035-003; heat treat 190, 000-210, 000; opp -005; nha L1700000
01-173-8651
Structural Component Air Bracket
Make L19170035-003; heat treat 190, 000-210, 000 psi; opp -005; nha L1700000
01-173-8652
Structural Component Air Bracket
Make L9170038-003; heat treat 190, 000-210, 000 psi; opp -005; nha L1700000
01-173-8653
Structural Component Air Bracket
Make L9170038-003; heat treat 190, 000 to 210, 000 psi; opp -009; nha L1702000
01-173-8666
Structural Aircraft Plate
Used on f-4 acft. matl al alloy, qq-a-250/5, 2024-0; matl size 0.040 by 1.200 by 4.000 in. lg; used on fairing assy, leading edge inboard closing
01-173-8672
Aircraft Former
Used on acft model c-135.
01-173-8673
Aircraft Former
Used on acft model c-135.
01-173-8674
Aircraft Former
16.000" overall length 8.000" overall width 0.040" material thickness
01-173-8675
Aircraft Former
2.500" overall length 2.500" overall width 0.071" material thickness heat treat 150-170 ksi
01-173-8676
Aircraft Former
2.500" overall length 2.500" overall width 0.071" material thickness heat treat 150-170 ksi
01-173-8677
Aircraft Former
2.600" overall length 2.500" overall width 0.071" material thickness heat treat 150-170
01-173-8678
Aircraft Former
2.600" overall length 2.500" overall width 0.071" material thickness heat treat 150-170 ksi
01-173-8679
Aircraft Former
1.600" overall length 2.400" overall width 0.071" material thickness heat treat 150-170 ksi
01-173-8680
Aircraft Former
Used on acft model c-135.
01-173-8681
Aircraft Former
Used on acft model c-135.
01-173-8682
Aircraft Former
Used on acft model c-135.
01-173-8683
Aircraft Former
Used on acft model c-135.
01-173-8684
Aircraft Former
01-173-8685
Aircraft Former
01-173-8686
Aircraft Former
01-173-8687
Aircraft Former
01-173-8688
Aircraft Former
01-173-8689
Aircraft Former
Used on acft model c-135.
01-173-8693
Airfoil Rib
13.620" overall length 2.406 in w at 1st end
01-173-8694
Stiffener Aircraft Rib
10.250" overall length 1.656" overall width
01-173-8698
Canopy Aircraft Panel
Used on b-1b bomber aircraft. opposite -012; part of -101 window assy & install, side, escape hatch - fwd; c/o; seal (1) , window (1) bushing (77) ; instl
01-173-8699
Canopy Aircraft Panel
Used on b-1b bomber aircraft. flight safety critical
01-173-8727
Fluid Aircraft Manifold
18.080" overall length 6.060" overall width c/o-tube, flange, coupling, nut; may be used for all replacements of -3; tube, fuel, inboard, lh external tank; nha 16P006-811; eff on 5c 0001 9999
01-173-9413
Wing Dive Brake Flap
Used on f-18 acft.
01-173-9585
Access Aircraft Door
Used on acft model b-1b. nha L3011110; c/o: -004 hinge half (1) , door (1) , seal (1) , bracket (1) , latch (1) , bolt (8)
01-173-9703
Structural Component Air Support
U/a: position no.1 slat track; oposite -016; u/o acft 1 & subq; n/a: L1702000; make from -009 forging, ST0160LB0005 teel die forging, alloy PH13-8m
01-173-9704
Structural Component Air Bracket
41.940" overall length make L9170026-003; heat treat 190-210 ksi; nickel plate mil-c-26074; opp -010; nha L1702000
01-173-9705
Structural Component Air Bracket
40.460" overall length make from L9170026-003; heat treat 190-210 ksi; nickel per mil-c-26074; opp - 010; nha L1702000
01-173-9706
Structural Component Air Bracket
38.720" overall length make L9170031-003; heat treat 190-210 ksi; nickel plated mil-c-26074; opp-014; nha L1702000
01-173-9707
Structural Component Air Bracket
01-173-9735
Structural Component Air Support
Used on c-5 acft. matl al alloy, qq-a-367, 7075-T6; 50, 000 psi tension
01-174-0713
Aircraft Frame
01-174-0742
Structural Aircraft Plate
Pylon, center section, inboard
01-174-0743
Structural Component Air Support
Used on f-4 acft. matl AMS5520; clindrical shaped; 1.250 in. lg; 0.250 in. od; 0.030 in. thk wall; used as pin-tubular on stabilator inboard trailing edge panel
