01-152-5193
Structural Component Air Fitting
16.500" overall length 11.000" overall width 9.000 " material thickness dim are stock material; machine from PH13-8M0 cres bar per AMS5629, type 1, sol treated; ht per H1000 per AMS2759; -503 opposite -504
01-152-5194
Structural Component Air Support
C/o: cap 1 ea 35-8234-29, web 1 ea 35-8234-34
01-152-5195
Structural Component Air Support
C/o: cap 1 ea 35-8234-30, web 1 ea 35-8234-38
01-152-5196
Structural Component Air Support
C/o: cap 1 ea 35-8234-31, web 1 ea 35-8234-32
01-152-5199
Aircraft Former
Used on b-52 aircraft. used as stiffener
01-152-6043
Aircraft Former
Used on aircraft b-52.
01-152-6044
Aircraft Former
Used on aircraft,b52.
01-152-6318
Aircraft Fairing
16.800" overall length 1.000" overall width 0.032" material thickness
01-152-6319
Structural Aircraft Plate
6.000" overall length 2.900" overall width 0.040" material thickness
01-152-6320
Structural Aircraft Plate
Used on B-52. opposite pn 35-20704-41
01-152-6321
Aircraft Stiffener
17.000" overall length 4.000" overall width 0.063" material thickness
01-152-6322
Aircraft Former
Used on acft model b-52.
01-152-6323
Aircraft Former
Used on acft model b-52.
01-152-6324
Structural Aircraft Plate
Used on B-52.
01-152-6325
Aircraft Former
Used on b-52 acft.
01-152-6326
Aircraft Former
Used on b-52 acft.
01-152-6328
Structural Aircraft Plate
Used on B-52.
01-152-6329
Aircraft Fairing
01-152-6330
Structural Aircraft Plate
Used on B-52.
01-152-6331
Structural Aircraft Plate
Used on B-52.
01-152-6332
Structural Aircraft Panel
Used on B-52.
01-152-6333
Structural Aircraft Panel
Used on B-52.
01-152-6334
Structural Aircraft Panel
Used on B-52.
01-152-6335
Structural Aircraft Panel
Used on B-52.
01-152-6336
Structural Component Air Support
39.000" overall length 8.600" overall width finish F2.115; heat treat T4
01-152-6340
Aircraft Fairing
39.000" overall length 2.500" overall width 0.012" material thickness
01-152-6341
Structural Component Air Support
44.000" overall length 2.600" overall width 0.080" material thickness
01-152-6342
Structural Aircraft Plate
10.400" overall length 2.600" overall width 0.080" material thickness part of 35-8642-1
01-152-6343
Structural Aircraft Plate
10.400" overall length 2.600" overall width 0.080" material thickness part of 35-8642-2
01-152-6344
Aircraft Channel
9.800" overall length 5.200" overall width 0.063" material thickness matl: clad al aly sht, 0 temp, ht T4; fin F2.115; opp -100
01-152-6345
Structural Component Air Bracket
86.000" overall length 1.200" overall width 0.050" material thickness
01-152-6346
Structural Component Air Bracket
86.000" overall length 1.200" overall width 0.050" material thickness opposite 35-8697-23 angle
01-152-6347
Structural Aircraft Plate
0.800" overall length 0.700" overall width 0.063" material thickness
01-152-6348
Structural Aircraft Plate
0.900" overall length 0.700" overall width 0.063" material thickness
01-152-6349
Structural Component Air Bracket
75.000" overall length 4.000" overall width 0.050" material thickness
01-152-6350
Structural Component Aircraf Web
01-152-6351
Structural Component Aircraf Web
33.600" overall length 24.000" overall width 0.032" material thickness opposite 35-8697-509
01-152-6352
Structural Component Air Bracket
96.000" overall length 2.000" overall width 0.063" material thickness
01-152-6353
Structural Component Air Bracket
96.000" overall length 2.000" overall width 0.063" material thickness opposite 35-8697-801
01-152-6355
Aircraft Fairing
01-152-6356
Structural Aircraft Plate
Used on B-52.
01-152-6365
Aircraft Skin
Used on B-52.
01-152-6366
Aircraft Former
7.500" overall length 2.000" overall width 0.050" material thickness opp 35-10703-1; 0 temper; heat treat T4; finish f-2.115
01-152-6367
Aircraft Former
7.500" overall length 2.000" overall width 0.050" material thickness opp 35-10703-2; 0 temper; heat treat T4; finish f-2.115
01-152-6368
Structural Aircraft Plate
16.000" overall length 0.070" overall width 0.040" material thickness finish f-2.115, heat treat T4
01-152-6369
Structural Aircraft Plate
6.000" overall length 0.700" overall width 0.040" material thickness finish f-2.115; heat treat T4
01-152-6370
Aircraft Former
16.000" overall length 0.700" overall width 0.040" material thickness opp 35-10703-1; 0 temper; finish f-2.115; heat treat T4
01-152-6371
Structural Aircraft Plate
16.000" overall length 0.700" overall width 0.040" material thickness finish f-2.115; heat treat T4
01-152-6372
Structural Aircraft Plate
16.000" overall length 0.700" overall width 0.040" material thickness finish f-2.115; heat treat T4
01-152-6373
Structural Aircraft Plate
16.000" overall length 0.700" overall width 0.040" material thickness heat treat T4
