01-128-7492
Structural Component Air Support
Used on acft model t-39a. aluminum alloy per qq-a-347, 9.166 in. lg. o/a, 6.424 in. w. o/a
01-128-7493
Structural Component Air Support
Used on acft model f111. aluminum alloy per qq-a-225/6, 2024 T6, 11.000 in. lg, 4.000 in. w, 0.250 in. thk
01-128-7494
Structural Component Air Support
9.000" overall length 8.000" overall width 5.000" material thickness
01-128-7495
Structural Component Air Support
Used on f-15 acft. function-support for wing tip antenna
01-128-7496
Bleed Air Duct Assembly
Used on acft model f-16.
01-128-7497
Bleed Air Duct Assembly
C/o 1 bracket, 2 bushing, 1 support, 1 boss, 2 doubler, 2 tube, 7 standoff, integral insulation, misc hdwar
01-128-7498
Bleed Air Duct Assembly
C/o 1 support, 1 bracket, 1 doubler, 2 tube, 5 standoff, integral insulation
01-128-7507
Aircraft Former
01-128-7508
Aircraft Former
7.500" overall length 2.500" overall width
01-128-7510
Aircraft Former
7.500" overall length 2.500" overall width 0.190" material thickness
01-128-7511
Aircraft Former
22.900" overall length 2.400" overall width 0.190" material thickness
01-128-7512
Aircraft Former
22.900" overall length 2.400" overall width 0.190" material thickness
01-128-7513
Aircraft Former
1.000" overall length 1.000" overall width 0.312" material thickness
01-128-7517
Airfoil Rib
16.405" overall length opposite pn 3W33075-110
01-128-7518
Airfoil Rib
16.405" overall length opposite pn 3W33075-109
01-128-7519
Airfoil Rib
23.000" overall length 4.900" overall width 0.051" material thickness
01-128-7520
Aircraft Skin
Used on C-135. 59.000" overall length 28.000" overall width
01-128-7521
Aircraft Skin
Used on F-111.
01-128-7522
Aircraft Skin
Used on F-111.
01-128-7534
Aircraft Trailing Edge
Spar assembly p/n 160D612512-3, core p/n 160D612512-15, rub strip p/n 160D612512-17, laminate build-up
01-128-7845
Structural Component Air Fitting
01-128-7946
Aircraft Fairing
01-128-7949
Aircraft Fairing
01-128-8407
Structural Aircraft Plate
0.125 in. thick; 3.500 in. wide; 6.700 in. long; aluminum alloy 2024, qq-a-250/5, temp T3
01-128-8411
Structural Aircraft Plate
Used on rf-4c/b aircraft. i.r. power supply, aft cockpit; matl-7075-T651 mms 152; dim.-16.140 in.lg, 10.490 in. w, 1.000 in. thk
01-128-8419
Aircraft Skin
35.000" overall length 15.000" overall width
01-128-8420
Aircraft Skin
48.000" overall length 25.500" overall width
01-128-8421
Aircraft Skin
20.000" overall length 15.000" overall width
01-129-1059
Aircraft Fairing
01-129-1067
Structural Component Air Support
Used on acft model f-16. alt matl al alloy per qq-a-250/12, c/o rail 1 ea p/n C9673-1, used on ejection seat, right hand, 48.180 in.lg
01-129-1068
Structural Component Air Support
Used on acft model f-16. alt matl al alloy per qq-a-250/12, c/o rail 1 ea p/n C9673-1, used on ejection seat, left hand, 48.180 in.lg
01-129-1069
Structural Component Air Support
Used on f-15 acft. function-support for wing tip antenna
01-129-1074
Aircraft Pylon
Superceded -839 ow; c/o hardware, harness instl, bracket instl, 1 rib, 2 closure, bracket assy, 1 rib assy, 2 pylon assy, trailing edge, panel assys, beam, door, pouch; nha 16S500-855; eff on 67 OO11 9999
01-129-1075
Aircraft Pylon
01-129-1290
Structural Aircraft Panel
Used on UH-1. navy:cap bulkhead sta 25.00
01-129-1661
Access Aircraft Door
01-129-1764
Structural Component Air Support
01-129-1775
Aircraft Frame
0.050 in. thk; 18.000 in. wide; 88.000 in. lg; aluminum alloy qq-a-250
01-129-1778
Aircraft Bulkhead
0.20 in. thk; 11.500 in. wide; 75.000 in. lg; 7075 al aly qq-a-250/13 temp 0 T6
01-129-1807
Access Aircraft Door
Used on F-16. lh main landing gear
01-129-1828
Structural Aircraft Plate
1.000" overall length 0.500" overall width 0.750" material thickness
01-129-1830
Bleed Air Duct Assembly
C/o 1 tube, 1 bracket, 2 bushing, 1 support, 2 washer, 3 standoff, nameplate, joint linked, 2 flange
01-129-1857
Aircraft Skin
52.300" overall length 23.400" overall width
01-129-1858
Aircraft Skin
52.300" overall length 23.400" overall width
01-129-1859
Aircraft Skin
50.000" overall length 23.400" overall width
01-129-1860
Aircraft Skin
50.000" overall length 23.400" overall width
01-129-1863
Aircraft Skin
Used on F-111. 97.000" overall length 61.000" overall width
01-129-1992
Aircraft Elevator
Used on aircraft model s-3.
01-129-1993
Horizontal Stabilizer
Used on aircraft s-3. cognizant service:navy;
01-129-2903
Structural Component Air Fitting
