01-231-3959
Structural Component Air Support
Used on f100-pw-220.
01-231-4068
Structural Component Air Support
Used on acft model 1f-111. material K10A57T3511, 3.300 in. lg
01-231-4071
Structural Aircraft Panel
01-231-4072
Structural Aircraft Panel
01-231-4073
Structural Aircraft Panel
01-231-4074
Structural Aircraft Panel
01-231-4080
Aircraft Skin
65.000" overall length 40.000" overall width
01-231-4655
Structural Aircraft Plate
01-231-4656
Structural Aircraft Plate
01-231-4657
Structural Aircraft Plate
P/o acft floor-aft; aluminum alloy 7075-0 per qq-a-250/13 cond-T6
01-231-4658
Structural Component Air Support
Used on f-15 acft. cap-upper outboard, former, side panel; fuselage station 651.060
01-231-4659
Structural Component Air Support
Used on f-15 acft. cap-upper outboard, former, side panel fuselage; station 651.060
01-231-4660
Structural Component Air Support
Used on f-15 acft. support, hinge-canopy
01-231-4661
Structural Component Air Support
Used on f-15 acft. support, hinge-canopy
01-231-4662
Structural Component Air Support
Used on f-15 acft. support, handle-canopy jettison, aft
01-231-4663
Structural Aircraft Panel
Panel assy-jet fuel starter exhaust
01-231-4665
Aircraft Pylon
Pylon, aircraft centerline suu-73/a
01-231-4841
Aircraft Skin
Used on aircraft model f-18a.
01-231-5080
Structural Component Air Support
01-231-5406
Structural Component Air Fitting
01-231-6343
Structural Aircraft Plate
01-231-6344
Structural Component Air Support
Used on acft model b-52g/h. 20145-T6 die forging per spec qq-a-367, comp 5; finish f-2.30; stock size 1.04 in.; located at wing section 922.39; nha 34-1037
01-231-6345
Structural Component Air Support
Used on acft model b-52g/h. 20145-T6 die forging per spec qq-a-367, comp 5; finish f-2.30; stock size by 1.06 in.; located at wing station 960.46 to 1000.16; nha 4-3231
01-231-6349
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -105a panel (1) , -111a panel (1) ; part of -109a panel assembly-headliner, fus sta 769.50 to 827.00, bl 28.50 to bl 66.25
01-231-6372
Aircraft Skin
56.000" overall length 29.000" overall width form, fit, function
01-231-8114
Radome
Used on b-52g/h aircraft. matl; pre-impregnated glass fabric per D675-20262-1; nha: 675-22769
01-231-8115
Radome
Used on b-52g/h. matl: pre-impregnated glass fabric per D675-20262-1; nha: 675-22734
01-231-9431
Structural Aircraft Plate
01-231-9433
Structural Component Air Support
01-231-9436
Flap Wing Landing Rib
01-231-9437
Flap Wing Landing Rib
01-231-9440
Flap Wing Landing Rib
01-231-9677
Access Aircraft Cover
01-231-9796
Structural Aircraft Plate
2.300" overall length 1.900" overall width 0.050" material thickness
01-231-9816
Thermal Special Purpo Insulation
01-232-0696
Structural Aircraft Plate
01-232-1727
Aircraft Former
01-232-2944
Structural Aircraft Plate
Plate, adapter-air duct to bulkhead
01-232-3262
Structural Aircraft Plate
C/o former p/n 160D611521-38, doubler p/n 160D611521-82, filler p/n 160D611521-84, bracket p/n 160D345441-43
01-232-3264
Structural Aircraft Plate
01-232-3266
Structural Component Air Support
Used on acft model a-10a. aluminum alloy per qq-a-200/11 7075-0, 64.000 in. lg
01-232-3268
Structural Component Air Support
Used on f-15 acft. p/o former-sidepanel fuselage station 693.500
01-232-3269
Structural Component Air Support
Used on f-15 acft. p/o former-sidepanel fuselage station 693.500
01-232-3275
Aircraft Former
01-232-3276
Aircraft Former
01-232-3277
Aircraft Former
01-232-3571
Structural Component Air Support
Used on a-7e aircraft. 14.110" overall length 7.125" overall width 0.250" material thickness
01-232-3572
Structural Component Air Support
Used on a-7e aircraft. 14.110" overall length 7.125" overall width 0.250" material thickness
01-232-3775
Structural Component Air Bracket
Used on sentry f22 aircraft. bracket assembly
