01-132-2475
Aircraft Former
9.800" overall length 2.000" overall width 0.080" material thickness
01-132-2476
Aircraft Former
2.100" overall length 1.000" overall width 0.080" material thickness
01-132-2477
Aircraft Former
5.000" overall length 1.000" overall width 0.070" material thickness
01-132-2478
Aircraft Former
8.000" overall length 1.000" overall width 0.070" material thickness
01-132-2479
Aircraft Former
01-132-2480
Aircraft Skin
33.000" overall length 4.000" overall width
01-132-2481
Aircraft Skin
20.070" overall length 16.500" overall width
01-132-3677
Structural Component Air Support
Used on acft model b52. used on rear spar, left hand
01-132-4158
Aircraft Skin
Used on f-16 acft. acft rudder island
01-132-5831
Vertical Stabilizer
01-132-5832
Vertical Stabilizer
01-132-5969
Pressure Fuel Servicing Adapter
01-132-6429
Access Aircraft Cover
Used on acft model b-52. used on wing pylon adapter kit
01-132-6718
Structural Component Air Support
Used on c-130 acft. function-upper fitting, strut, left forward inbd; location fuselage station 737.0; matl-7075-T651 aluminum alloy per qq-a-283 temp-T651
01-132-6719
Structural Component Air Support
Used on wc-130h acft. function-right forward outboard fitting; matl-aluminum alloy 7075-T651 per qq-a-283 temp-651
01-132-6720
Structural Component Air Support
Used on wc-130h acft. function-left forward outboard fitting; location-fuselage station-737; matl-7075-T651 aluminum alloy per qq-a-283 temp-651
01-132-6730
Exhaust Pipe
Used on acft model c135. used on thrust reverser
01-132-6732
Aircraft Stringer
12.400" overall length ht T4; alter BAC1493-237
01-132-7095
Access Aircraft Door
01-132-7096
Access Aircraft Door
Used on c-141 aircraft.
01-132-7286
Access Aircraft Cover
Rh upper strake center fuselage
01-132-7287
Aircraft Fairing
19.000" overall length 7.200" overall width 0.040" material thickness
01-132-7291
Structural Component Air Support
Used on wc-130h acft. function-right forward inboard brace; location-lower strut fuselage station 737; matl-aluminum alloy 7075-T651 per qq-a-283 temp-651
01-132-7299
Aircraft Former
Used on T-39. cond 0, bare sheet, LB0170-124
01-132-7305
Airfoil Rib
7.800" overall length 6.100" overall width 0.040" material thickness heat treat to cond T42, age to cond T62
01-132-7306
Airfoil Rib
7.800" overall length 6.100" overall width 0.040" material thickness heat treat to cond T42, age to cond T62
01-132-7307
Airfoil Rib
7.600" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7308
Airfoil Rib
7.600" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7310
Airfoil Rib
8.200" overall length 6.200" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7311
Airfoil Rib
7.900" overall length 6.100" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7314
Aircraft Skin
Used on F-111. c/o skin installation p/n 12B13226M2-4, modified skin assembly 12B10901-14
01-132-7318
Fuel Aircraft Tank
Used on F-15.
01-132-7319
Fuel Aircraft Tank
Used on F-15.
01-132-7321
Fuel Aircraft Tank
Used on F-15.
01-132-7322
Fuel Aircraft Tank
Used on F-15.
01-132-7323
Fuel Aircraft Tank
Used on F-15.
01-132-7324
Fuel Aircraft Tank
Used on F-15.
01-132-7811
Structural Aircraft Plate
5.500" overall length 3.000" overall width 1.000" material thickness c/o plate 1 ea p/n CV15-564575-13, bushing 1 ea p/n NAS537B6P76, bushing 2 ea p/n NAS537-4P19; used on main landing gear door
01-132-7815
Aircraft Former
Used on T-39. matl 7075-T7351 al alloy plate, .750 x 8.75 X56.75, qq-a-250/12' machined per rockwell spec LA0103-004; 125.0microinch all machined surfaces
01-132-7817
Airfoil Rib
7.900" overall length 6.100" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7818
Airfoil Rib
7.500" overall length 5.800" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7819
Airfoil Rib
7.500" overall length 5.800" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7820
Airfoil Rib
8.100" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7821
Airfoil Rib
8.100" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7822
Airfoil Rib
8.200" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7823
Airfoil Rib
8.200" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7824
Airfoil Rib
8.100" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-132-7825
Aircraft Skin
C/o panel assembly p/n 160D213014-30, bracket doubler angle p/n 160D213014-R270, cover p/n 160D213014-200, 2 ea. gasket, 3 ea. rib, 2 ea. rib
01-132-7920
Fluid Aircraft Manifold
23.250" overall length 10.750" overall width
01-133-1831
Aircraft Frame
