01-152-6595
Aircraft Stringer
39.000" overall length 5.100" overall width 0.040" material thickness u/a: stringer-hat section; matl: clad sht, 0 temper; opposite -538
01-152-6596
Aircraft Stringer
39.000" overall length 5.100" overall width 0.040" material thickness u/a: stringer-hat section; matl: clad sht; 0 temp; opposite -537
01-152-6606
Thermal Special Purpo Insulation
Insulation material johns manville rf number 600 or equiv.encased in aisi 321 cres foil covering; left hand, used on tension regulator shroud; end item identification:aircraft, model B52
01-152-6609
Aircraft Door
Used on B-52.
01-152-6826
Wing Parts Kit
Used on f-15 aircraft. right hand side retrofit, intermadiate spar
01-152-7311
Structural Component Aircraf Web
16.000" overall length 0.032" material thickness
01-152-7312
Aircraft Intercostal
5.300" overall length 3.500" overall width 0.063" material thickness used on trailing edge fairing, inboard nacelle; steel sheet, annealed decard per AMS6350
01-152-7313
Aircraft Intercostal
5.200" overall length 3.500" overall width 0.071" material thickness used on trailing edge fairing, inboard nacelle; steel sheet, annealed decard per AMS6350
01-152-7314
Aircraft Intercostal
5.100" overall length 3.800" overall width 0.071" material thickness used on trailing edge fairing, inborad nacelle; steel sheet, annealed decard per ams 6350
01-152-7315
Aircraft Intercostal
5.800" overall length 5.300" overall width 0.071" material thickness used on trailing edge fairing, inboard nacelle; steel sheet, annealed decarb per AMS6350
01-152-7316
Aircraft Intercostal
5.400" overall length 3.500" overall width 0.071" material thickness used on trailing edge fairing, inboard nacelle; steel sheet, annealed decard per AMS6350
01-152-7317
Structural Aircraft Plate
7.000" overall length 1.700" overall width 0.125" material thickness
01-152-7318
Structural Aircraft Plate
8.500" overall length 1.600" overall width 0.125" material thickness matl: clad; T3 temper
01-152-7319
Structural Aircraft Plate
7.800" overall length 1.600" overall width 0.125" material thickness matl: cres stl sht type 301 comp, full hard surface cond 2d
01-152-7338
Structural Aircraft Plate
Used on b-52 aircraft. used as cap tee outer on frame installation station 70.00, canted nose cowl; opposite p/n 35-8642-113
01-152-7339
Structural Aircraft Plate
Used on B-52. BAC1506-1347 x 82.800
01-152-7340
Structural Aircraft Plate
Used on B-52. opp 35-8642-13
01-152-7341
Structural Aircraft Plate
4.700" overall length 1.700" overall width 0.020" material thickness
01-152-7342
Structural Aircraft Plate
2.700" overall length 1.100" overall width 0.020" material thickness
01-152-7343
Structural Aircraft Plate
6.900" overall length 1.000" overall width 0.020" material thickness
01-152-7344
Structural Aircraft Plate
2.700" overall length 2.000" overall width 0.020" material thickness
01-152-7345
Structural Aircraft Plate
14.000" overall length 4.500" overall width 0.071" material thickness
01-152-7346
Structural Aircraft Plate
Used on B-52. opp pn 35-8642-15
01-152-7347
Structural Aircraft Plate
14.000" overall length 4.500" overall width 0.071" material thickness
01-152-7348
Structural Aircraft Plate
Used on B-52. opp pn 35-8642-17
01-152-7349
Structural Aircraft Plate
6.000" overall length 2.100" overall width 0.025" material thickness
01-152-7350
Structural Aircraft Plate
3.900" overall length 1.500" overall width 0.025" material thickness opposite 35-8227-139
01-152-7351
Structural Aircraft Plate
2.000" overall length 1.300" overall width 0.025" material thickness
01-152-7352
Structural Aircraft Plate
6.900" overall length 1.000" overall width 0.020" material thickness
01-152-7353
Structural Aircraft Plate
8.000" overall length 1.500" overall width 0.023" material thickness
01-152-7354
Structural Aircraft Plate
24.970" overall length 11.000" overall width 0.016" material thickness
01-152-7355
Structural Aircraft Plate
5.000" overall length 4.500" overall width 0.020" material thickness
01-152-7356
Structural Aircraft Plate
0.700" overall length 0.600" overall width 0.080" material thickness
01-152-7358
Structural Component Air Support
7.600" overall length 3.300" overall width 0.063" material thickness opp 35-15322-29; used as intercostal, lower cowl body panel
01-152-7359
Structural Component Air Support
7.700" overall length 4.300" overall width 0.063" material thickness opp 35-15322-32; used as intercostal, lower cowl body panel
01-152-7360
Structural Component Air Support
7.700" overall length 4.300" overall width 0.063" material thickness opp 35-15322-31; used as intercostal, lower cowl body panel
01-152-7361
Structural Component Air Support
7.700" overall length 4.800" overall width 0.063" material thickness opp 35-15322-34; used as intercostal-intermediate
01-152-7362
Structural Component Air Support
7.700" overall length 4.800" overall width 0.063" material thickness opp 35-15322-33; used as intercostal-intermediate
01-152-7363
Structural Component Air Support
7.700" overall length 4.300" overall width 0.063" material thickness opp 35-15322-35; used as intercostal-intermediate
01-152-7364
Structural Component Air Support
7.500" overall length 4.200" overall width 0.063" material thickness opp 35-15322-38; used as intercostal-intermediate
01-152-7365
Structural Component Air Support
7.500" overall length 4.200" overall width 0.063" material thickness opp 35-15322-37; used as intercostal-intermediate
01-152-7366
Structural Component Air Support
11.300" overall length 4.300" overall width 0.063" material thickness opp 35-15322-40; used as intercostal 45 deg.splice fire seal
01-152-7367
Structural Component Air Support
11.300" overall length 4.300" overall width 0.063" material thickness opp 35-15322-39; used as intercostal 45 deg splice fire seal
01-152-7368
Structural Component Air Support
7.300" overall length 4.300" overall width 0.063" material thickness opp 35-15322-42; used as intercostal 45 deg skin splice
01-152-7369
Structural Component Air Support
7.300" overall length 4.300" overall width 0.063" material thickness opp 35-15322-41; used as intercostal 45 deg skin splice
01-152-7370
Structural Component Air Support
C/o 1 web, 1 pad
01-152-7371
Structural Component Air Support
2.990" overall length 0.850" overall width c/o 2 pad, 1 web
01-152-7387
Aircraft Former
Used on B-52. function gang channel
01-152-7388
Aircraft Former
8.300" overall length 8.300" overall width 0.016" material thickness
01-152-7389
Aircraft Former
8.300" overall length 8.300" overall width 0.016" material thickness opposite 35-8227-193
