00-756-5090
Aircraft Leading Edge
00-756-5091
Aircraft Leading Edge
00-756-5092
Aircraft Leading Edge
00-756-5093
Aircraft Leading Edge
0.032" material thickness
00-756-5094
Aircraft Leading Edge
0.032" material thickness
00-756-5477
Aircraft Windshield Panel
Used on helicopter,ch-47. 38.000" overall length
00-756-5478
Aircraft Windshield Panel
Used on helicopter,ch-47. 38.000" overall length
00-756-5887
Aircraft Leading Edge
0.032" material thickness
00-756-5888
Aircraft Leading Edge
0.032" material thickness
00-756-5889
Aircraft Leading Edge
00-756-5890
Aircraft Leading Edge
00-756-5912
Access Aircraft Cover
00-756-5913
Access Aircraft Cover
00-756-5925
Structural Component Air Support
Used on acft model c-141. aluminum alloy cast per qq-a-596 composition 8
00-756-8250
Aircraft Fairing
00-756-9915
Thermal Special Purpo Insulation
U/o: f-4 aircraft; matl: rag felt RF600, titanium affixed sh, mil-s-9046 featgmatl:rag felt RF600, titanium afixed sheet both sides
00-757-1429
Structural Aircraft Panel
00-757-1430
Structural Aircraft Panel
00-757-1431
Structural Aircraft Panel
00-757-1443
Structural Component Air Support
Used on acft model c-135. aluminum alloy per 2024-T4 qq-a-268, 2.400 in. lg, 3.500 in. dia, used on air intake, rudder boost
00-757-2120
Structural Component Air Support
2.500" overall length 1.500" overall width 0.063" material thickness
00-757-2134
Structural Component Air Support
Used on acft model c-135. c/o support p/n 65-14667, support p/n 66-14667-1, support p/n 65-14667-2, support p/n 65-14667-3, support p/n 66-14667-4, nut plate clipon p/n bac-N10fx-1, nut plate p/n nas 1068-C3
00-757-2135
Structural Component Air Support
Used on acft model c-135. c/o support p/n 65-14667-5, support p/n 65-14667-11, nut plate p/n NAS1068-C3
00-757-2136
Structural Component Air Support
Used on acft model c-135. c/o support p/n 65-14S661-6, support p/n 60-14661-10, support p/n 65-14667-12, support p/n 65-14667-6, support p/n 65-14667-17, support p/n 65-12783-24, nut plate clipon p/n bac-N10fx-1, nut plate p/n NAS1068-C3
00-757-2505
Structural Component Air Support
Used on b-52 aircraft. used as fitting-paratroop static line support, upper, fuselage station 1278; matl-7075-T651 qq-a-283 temp T651; dimensions-8.800 in. lg, 2.500 in. thk
00-757-2868
Structural Component Air Support
Used on aircraft model uh1.
00-757-3888
Aircraft Door
00-757-5742
Aircraft Skin
00-757-5747
Aircraft Former
Used on aircraft,a-7.
00-757-6040
Structural Component Air Support
Used on acft model c-141. made from lockheed stock LS6528-2, finish f-1-29; 16.900 in. lg, 1.640 in. o/a w, 0.500 in. h; c/o support 1 ea, recepticale (fastener) 4 ea; located at water line 225, fuselage stations 978 to 998
00-757-7118
Cowling
Used on aircraft model uh-1. aluminum alloy, qq-a-250/5 T3, qq-a-250/8 H34;
00-757-7130
Cowling
Used on aircraft model uh-1. aluminum alloy, qq-a-250/5 T3, qq-a-250/8 H34;
00-757-7481
Structural Component Air Support
Used on acft model c-5. pmade from al alloy casting A356-T6 per mil-a-21180, class 10; 1.860 in. lg, 1.320 in. w, 1.100 in. h; 2 0.210 in. dia mounting holes in base; 2 in line holes 0.200 in. dia, 1 in each vertical plates, 0.700 in. above base
00-757-7482
Structural Component Air Support
Used on acft model c-5. al alloy 7075-T651 per qq-a-250/12, temper-T651; triangular shaped; 23.000 in. lg, 17.000 in. o/a w, 3.000 in. o/a thk; c/o support 1 ea, bushing 2 ea
00-757-7484
Structural Component Air Support
Used on acft model c-5. al alloy 7075-T651 per qq-a-250/12, temper-T651; triangular shaped; 23.000 in. lg, 17.000 in. o/a w, 3.000 in. o/a thk; c/o support 1 ea, bushing 2 ea
00-757-7911
Access Aircraft Door
Used on p-3a acft.
00-757-8042
Access Aircraft Door
00-757-8905
Structural Component Air Support
Used on acft model c-135. steel per A151 301 mil-s-5059 1/4 hard sur. cond. 2d, opt aisi 302 per mil-s-5059 annealed, 1.450 in. lg, 1.100 in. w, 0.063 in. thk
00-757-8914
Structural Component Air Support
2 in line 0.561 in. dia w/1.687 in. w gap, spotfaced 1.440 in. dia
00-758-1094
Structural Aircraft Plate
00-758-1095
Aircraft Fairing
00-758-1407
Access Aircraft Door
00-758-1426
Structural Component Air Support
Used on aircraft model uh1f. magnesium alloy, qq-m-56 comp AZ91c cond T6, 3.400 in. o/a lg, 2.680 in. o/a w, 2 mtg holes 0.190 in. min, 0.196 in. max dia, 2 mtg holes 0.208 in. min, 0.214 in. max dia
00-758-1518
Aircraft Door
Used on F-5.
00-758-1526
Access Aircraft Cover
0.191" hole diameter
00-758-1579
Structural Aircraft Panel
Laminated figerglass
00-758-1807
Aircraft Fairing
Cond T3
00-758-1810
Access Aircraft Door
