01-189-1485
Aircraft Fairing
01-189-1488
Structural Component Air Support
Used on acft model c/kc-135. al alloy bar 2024-T4 per qq-a-268; T4 temper; finish srf-2.30; 3.660 in. o/a lg, 1.530 in. o/a w, 0.624 in. o/a thk; nha 65-10505
01-189-1489
Structural Component Air Support
Used on acft model b-52. machined from 7075-T411 forged block per BMS7-186; heat treated to cond T73; finish f-255 except bolt
01-189-1493
Structural Component Air Support
Used on acft model a-10a. made from 160D414017-1
01-189-1494
Structural Component Air Support
Used on acft model a-10a. aluminum alloy per qq-a-250/12 7075-T35
01-189-1495
Structural Component Air Support
Used on acft model a-10a. c/o support p/n 160D891703-13, 2 ea. washer p/n 160D891703-25, as required adhesive
01-189-1497
Structural Component Air Support
Used on c-130 acft. aluminum 2024-T3, qq-a-362
01-189-1498
Structural Component Air Support
Used on c-141 acft. tank seal, lower outboard, intermediate beam
01-189-1501
Structural Aircraft Panel
C/o: -118a core (1) size 0.524 x 21 x 49, matl 5052 alum alloy per qq-a-250/8, core to be mil-c-7438, class 2, 5.73/166-20n.5052 mil.519 max.529 thk; -112a & 116a doubler (2) size .032X4X24 matl 7075-T6 alclad per qq-a-250/13; -110a& -114a doubler (2) size .032X5.4X44 matl 7075-T6 per qq-a-250/13; -108a inner skin (1) size .013X21X45, matl 7075-T6 alclad per qq-a-250/13; -106a outer skin (1) size .016X24X50, matl 7075-T6 alclad per qq-a-250/13
01-189-1503
Structural Aircraft Panel
01-189-1504
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1418 to 1453
01-189-1505
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1418 to 1453
01-189-1506
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1383 to 1418
01-189-1508
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1383 to 1399
01-189-1509
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1383 to 1399
01-189-1510
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1418 to 1453
01-189-1515
Aircraft Former
40.000" overall length 4.750" overall width 0.071" material thickness
01-189-1516
Aircraft Former
40.000" overall length 4.750" overall width 0.071" material thickness
01-189-1517
Aircraft Former
44.000" overall length 4.750" overall width 0.071" material thickness
01-189-1518
Aircraft Former
44.000" overall length 4.750" overall width 0.071" material thickness
01-189-1519
Aircraft Former
40.000" overall length 4.750" overall width 0.071" material thickness
01-189-1520
Aircraft Former
40.000" overall length 4.750" overall width 0.071" material thickness
01-189-1522
Aircraft Former
7.880" overall length 2.640" overall width
01-189-1523
Aircraft Former
Used on c-130 acft.
01-189-1524
Aircraft Former
Used on c-130 acft.
01-189-1525
Aircraft Former
Used on c-130 acft.
01-189-1612
Thermal Insulation Pipe Covering
Acft c-130
01-189-2562
Access Aircraft Cover
Used on acft model b-1b. used as wing outer panel fuel salvage pump access cover
01-189-2581
Structural Component Air Bracket
Make -009 per PH13-8mo; nha L1201050
01-189-2582
Structural Component Air Bracket
Make -009 per PH13-8mo; opp -017; nha L1201050
01-189-2583
Structural Component Air Bracket
Make -009 per PH13.8mo; opp -017; nha L1201050
01-189-2584
Structural Component Air Bracket
Make from -009 per PH13-8mo; opp -018; nha L1201050
01-189-2585
Structural Component Air Bracket
Make from -009 per PH13-8mo; opp -018; nha L1201050
01-189-2586
Structural Component Air Bracket
Make from -009 per PH13-8mo; opp -017; nha L1201050
01-189-2616
Structural Aircraft Plate
C/o 1 plate, 1 flourosilicone rubber gasket; nha L1203369; opp -002
01-189-2617
Structural Aircraft Plate
14.400" overall length 7.650" overall width 1.200" material thickness c/o 1 plate, 1 florosilicone gasket seal, 10 helicoil inserts; nha L1203369; opposite -002
01-189-2812
Access Aircraft Door
Used on acft model b-1b.
01-189-2901
Structural Aircraft Plate
7.700" overall length 3.000" overall width 0.063" material thickness repair of 53-3-1022 cadmium surface treated
01-189-2905
Structural Component Air Support
19.05 in extended
01-189-2906
Structural Component Air Support
Used on acft model b-1b. 2024
01-189-2907
Structural Component Air Support
Used on acft model a-10a. aluminum alloy per qq-a-367, heat treat to t-73 per mil-h-6088, made FROM160D116007f-11
01-189-2913
Wing Aircraft Spoiler
Nha L1600000; opposite -011
01-189-4247
Structural Aircraft Plate
7.590" overall length 5.120" overall width 0.125" material thickness repair of 53-3-1022
01-189-4255
Structural Component Air Support
Used on acft model a-10a. made from 160D116022-11f, steel forging per mil-s-5000, 4340 condition d
01-189-4256
Structural Component Air Support
Used on acft model a-10a. aluminum alloy bar per qq-a-235/9 7075-7351, 7.800 in. lg, 1.500 in. w, 1.500 in. lg
01-189-4264
Aircraft Skin
Used on F-4. 48.000" overall length 35.000" overall width per mac ps 15534; part of -12, -57, -107, -109 door assy, no. 4 engine access
01-189-5637
Structural Component Air Support
01-189-5920
Access Aircraft Cover
Used on acft model b-1b. opposite p/n -002
01-189-5922
Access Aircraft Door
Used on acft model b-1b.
01-189-5923
Access Aircraft Door
Used on acft model b-1b.
