00-015-9063
Structural Component Air Support
C/o 2 angle, 2 bracket, 2 screw, 2 nuts
00-016-0806
Airfoil Rib
U/a: rib assy; opp -020
00-016-0813
Airfoil Rib
Used on b-52 aircraft. u/a: rib assembly; opposite -41
00-016-1566
Thermal Insulation Pipe Covering
Half section, 0.440" min., 0.500" max. thk fiberglass, 0.0015" thk stainless steel foil inner cover, 0.003" thk stainless steel outer cover
00-016-1951
Access Aircraft Cover
Used on acft model c-141.
00-016-1967
Structural Aircraft Panel
With fabric
00-016-6341
Structural Component Air Support
Used on aircraft model uh1f. aluminum alloy, qq-a-367 comp 7079 cond T611, 3.280 in. o/a lg, 1.750 in. o/a w, 1.750 in. o/a h
00-017-0668
Aircraft Former
00-017-0669
Aircraft Former
00-017-0670
Aircraft Former
00-017-0671
Aircraft Skin
Used on f-4, phantom aircraft. matl class d
00-017-0672
Aircraft Former
00-017-0673
Aircraft Former
00-017-0675
Aircraft Former
00-017-0679
Aircraft Skin
6.150" overall length 4.300" overall width
00-017-0842
Aircraft Former
00-017-2408
Structural Component Air Support
Used on acft model h3. c/o bushing 2 ea p/n NAS537-4p-27, support 1 ea p/n S6140-61411-3
00-017-2622
Aircraft Floor
Birch
00-017-2624
Aircraft Floor
96.000" overall length 23.700" overall width birch 025 grade 1
00-017-2632
Structural Component Air Support
Used on acft model h3. alum alloy per qq-a-267 T3511, 0.750 in.w, 3.380 in.lg, used on air bottle utility system
00-017-2634
Structural Component Air Support
Used on acft model h3. phenolic ty fbm per mil-p-15035, 0.620 in.thk, 2.000 in.w, 3.120 in.lg
00-017-2643
Structural Component Air Support
7.120" overall length 1.000" overall width 1.000" material thickness
00-017-4279
Fuel Aircraft Tank
00-017-6078
Filler Opening Cap
4.250" outside diameter
00-017-7911
Airfoil Rib
U/a: rib assembly; opposite -40
00-017-7916
Airfoil Rib
U/a: rib assembly; opposite -39
00-017-7920
Stiffener Aircraft Rib
Used on b-52 aircraft.
00-017-7921
Stiffener Aircraft Rib
00-017-7925
Stiffener Aircraft Rib
00-017-8229
Structural Component Air Support
Aluminum alloy qq-a-250/12 7075-T6
00-017-8664
Cowling
0.025 in. thk outer skin
00-017-8665
Cowling
0.025 in. thk outer skin
00-017-9899
Aircraft Fairing
00-017-9901
Aircraft Fairing
00-017-9909
Access Aircraft Door
Used on c-5 aircraft.
00-017-9917
Access Aircraft Door
00-017-9976
Structural Component Air Support
Used on acft model c5. steel 17-4ph cres per ams 5355 annealed, 3.940 in.w, 4.345 in.lg, used on idler shaft, aft, engine control
00-017-9985
Structural Component Air Support
Used on acft model c5. steel 17-4ph cres per ams 5355 annealed, used on idler engine control
00-018-0670
Wing Dive Brake Flap
Used on aircraft model a7.
00-018-0672
Access Aircraft Door
Lh anodize surface treated
00-018-0674
Structural Component Air Support
Used on aircraft model a7a. consists of 1 fitting, aluminum alloy, qq-a-200/11 7075-T6, 2.620 in. lg, 1.880 in. w, 0.120 in. thk matl, 4 holes 0.191 in. dia, 2 holes 0.625 in. dia, 2 bushings
00-018-0718
Structural Component Air Bracket
2.000" overall length 1.600" overall width
00-018-0732
Aircraft Hinge
00-018-0757
Structural Component Air Support
00-018-0758
Structural Component Air Support
00-018-0774
Aircraft Skin
Used on f-111 aircraft.
00-018-0824
Structural Component Air Fitting
00-018-2328
Structural Aircraft Panel
Used on t-39 aircraft.
