01-097-6181
Longeron
Used on c-5a acft. matl titanium alloy; do not use cadmium plated tools on this item; used on pylon apron;
01-097-6182
Longeron
Do not use cadmium plated tools on this item
01-097-6184
Aircraft Skin
Used on c-5 airplane.. matt; titanium alloy, do-not use cadmium plated tools on this item, matt stock size; 114.000 in. lg, 9.000 in. w, 0.032 in. thk, install opposite p/n 4P50006-123c
01-097-6187
Aircraft Skin
Used on f-16a belgium aircraft. c/o sealant per fms-1044-5, -25 plate 0.100 x 9 x 12, -53 plate .100 x 5.6 x 6, -79 skin .100 x 55 x 66; material of plates
01-097-6188
Aircraft Skin
Nha p/n 16B415-3; eff 61 0117-9999; superseded p/n 16B4601-13 ni ecn 79988
01-097-6190
Aircraft Stringer
33.720" overall length stock 1M57594 by 33.720 in
01-097-7290
Access Aircraft Door
Opposite to p/n 7738290-10
01-097-7360
Aircraft Stiffener
Do not use cadmium plated tools on this item; matl: titanium alloy
01-097-7361
Aircraft Stiffener
Do not use cadmium plated tools on this item; matl:titanium alloy
01-097-7398
Structural Aircraft Plate
01-097-7399
Structural Aircraft Plate
01-097-7400
Structural Aircraft Plate
01-097-7429
Structural Aircraft Plate
6.000" overall length 6.000" overall width 0.100" material thickness
01-097-7445
Aircraft Skin
Used on c-135 airplane.. 48.000" overall length 48.000" overall width matt; clad, heat treat per T4, finish f-2.115
01-097-7446
Aircraft Skin
Used on b-52 bomber airplane.. 15.800" overall length 10.300" overall width matt; clad, finish f-2.16, heat treat per T3
01-097-7447
Aircraft Skin
Used on b-52 bomber airplane.. 20.800" overall length 10.200" overall width matt; clad, finish f-2.16, heat treat per T3
01-097-7448
Aircraft Skin
47.000" overall length 27.000" overall width
01-097-7449
Aircraft Spar
01-097-7450
Aircraft Spar
01-097-8434
Structural Aircraft Plate
Used on acft model f-16a belguim. titanium alloy per mil-t-9046, type 1, comp b, cond a; do not use cadmium plated tools on this item; located at fs 446.10 to fs 479.55; eff 6h 0014 9999; nha 16B6312-803; superseded p/n 16B6312-15 ni per ecn 83353; functional description:extension, shield
01-097-8910
Landing Gear Aircraft Fairing
01-097-9064
Structural Component Air Support
Used on aircraft fb-111.
01-097-9083
Aircraft Intercostal
9.000" overall length 7.000" overall width 0.032" material thickness
01-097-9084
Aircraft Frame
01-097-9761
Bleed Air Duct Assembly
Used on uh-60 black hawk. anodize surface treated
01-097-9762
Bleed Air Duct Assembly
Used on uh-60 blackhawk airframe. anodize surface treated
01-097-9822
Access Aircraft Door
01-097-9823
Access Aircraft Door
01-098-1163
Fluid Aircraft Manifold
01-098-1796
Structural Aircraft Plate
Used on acft model f4e. sheet steel A286 per ams 5525, 0.032 in.thk, 2.850 in.w, 16.000 in.lg, left hand, used on number 5 engine door, located from fs 447.05 to fs 493.0
01-098-2797
Structural Aircraft Panel
C/o insulation; trim cloth; tack strip; panel; insulation matl fiberglass; tack strip matl, plywood basswood; backing
01-098-3401
Structural Aircraft Plate
01-098-3412
Structural Aircraft Panel
21.000" overall length 16.000" overall width c/o strip
01-098-3425
Aircraft Former
Used on F-15.
01-098-3436
Aircraft Skin
33.030" overall length 21.200" overall width
01-098-4670
Bell Crank
0.7489" bore diameter
01-098-5029
Structural Aircraft Panel
01-098-5032
Structural Aircraft Panel
01-098-5033
Structural Aircraft Panel
01-098-5519
Aircraft Elevator
Used on aircraft model uh-in.
01-098-6543
Airfoil Rib
Used on acft model f-4j. stock is made from 32-11040-27f, left hand
01-098-8073
Aircraft Door
01-098-8074
Aircraft Door
01-098-8139
Structural Aircraft Plate
Used on acft model f4. do not use cadmium plated tools on this item, titanium 6al-4v per mil-t-9046 comp c cond annealed, 0.040 in.thk, 14.500 in.w, 15.000 in.lg, left hand, located from fs 303.62 to 359.66;
01-098-8159
Aircraft Skin
19.500" overall length 16.500" overall width cond 0
01-098-9520
Access Aircraft Door
Used on aircraft model a-10. located sta 276.70
01-098-9573
Structural Aircraft Plate
Located at ws 0.00, 23.00
01-098-9574
Structural Aircraft Plate
Located at ws 0.00, 23.00
01-098-9596
Aircraft Leading Edge
Used on F-15. retrofit
