00-827-3393
Aircraft Window Panel
00-827-4035
Aircraft Skin
46.000" overall length 38.300" overall width matl MMS155 class i cond 0
00-827-4059
Fluid Aircraft Manifold
2.430" overall length 1.900" overall width
00-827-4061
Aircraft Skin
16.500" overall length 11.100" overall width
00-827-4062
Aircraft Former
00-827-4447
Aircraft Fairing
00-827-4477
Aircraft Fairing
00-827-4497
Structural Aircraft Panel
00-827-4503
Structural Aircraft Plate
19.360" overall length 17.000" overall width
00-827-4504
Structural Aircraft Panel
00-827-7629
Pressure Fuel Servicing Adapter
00-827-7722
Aircraft Fairing
Ht T42
00-827-8674
Structural Aircraft Plate
1.000" overall length 1.000" overall width 0.025" material thickness
00-827-8688
Aircraft Fairing
00-827-8694
Structural Component Air Support
00-828-3290
Aircraft Fairing
Used on ch-47 series helicopters.
00-828-3333
Structural Aircraft Panel
Used on uh-1e,th-1l,uh-1l and uh-1m.
00-828-3334
Aircraft Fairing
Used on ch-47, chinook helicopter.
00-828-4444
Aircraft Skin
00-828-5339
Structural Aircraft Panel
With core
00-828-5340
Structural Aircraft Panel
With core
00-828-8138
Access Aircraft Door
Oxide film or primer zinc chromate surface treated
00-828-8140
Aircraft Floor
Aluminum alloy
00-828-8142
Aircraft Floor
Aluminum alloy
00-829-2074
Structural Component Air Support
00-829-2176
Aircraft Fairing
00-829-4327
Fuselage Section
20.500" overall length 17.000" overall width 0.030" material thickness manufacture suggested name: ejector-aft fuselage; sheet hastelloy; c/o: -5 stiffeners
00-829-4716
Aircraft Former
00-829-4717
Aircraft Former
00-829-5418
Outer Wing Section
P/o lh wing, appl to a-3 acft;
00-829-5423
Outer Wing Section
P/o wing, appl to a-3 acft;
00-829-6048
Aircraft Former
00-829-6049
Aircraft Former
00-829-6050
Aircraft Former
00-829-6051
Aircraft Former
00-829-6052
Aircraft Former
00-829-6053
Aircraft Former
00-829-6054
Structural Component Air Support
Used on acft model b-52. aluminum alloy, qq-a-250/12, 3.410 in. lg, 0.570 in. w, 2 mtg HOLES0.218 in. dia
00-829-6055
Structural Component Air Support
Used on acft model b-52. aluminum alloy, qq-a-250/12, 3.410 in. lg, 0.750 in. w, 2 mtg HOLES0.218 in. dia
00-829-6846
Fluid Aircraft Manifold
Used on next higher assy nsn: 1615-01-014-6006. magnesium alloy, qq-m-56, 0.276 in. min, 0.283 in. max dia mounting hole thru 2 places, boss fitting for 0.275 in. od tube 1 place, boss fitting for 0.250 in. od tube 1 place
00-829-7027
Access Aircraft Door
00-829-7028
Access Aircraft Door
00-829-7159
Access Aircraft Cover
00-829-7646
Trim Aircraft Tab
73.000" overall length
00-829-7648
Exhaust Pipe
Used on acft model c-7a.
00-829-7651
Exhaust Pipe
Used on acft model c-7a.
00-829-7652
Exhaust Pipe
Steel, corrosion resistant, ams 5526
00-829-7653
Exhaust Pipe
Used on acft model c-7a. cres steel per AMS5526; 21.370 in. lg, 0.050 in thk
00-829-7654
Exhaust Pipe
Used on acft model c-7a.
00-829-9389
Structural Component Air Fitting
Matl: nylon fabric
