01-152-6443
Structural Component Air Support
7.500" overall length 4.400" overall width 0.063" material thickness opp 35-15322-16; used as intercoastal
01-152-6444
Structural Component Air Support
7.500" overall length 4.400" overall width 0.063" material thickness opp 35-15322-15; used as intercoastal
01-152-6445
Structural Component Air Support
7.500" overall length 4.400" overall width 0.063" material thickness opp 35-15322-18; used as intercoastal
01-152-6446
Structural Component Air Support
7.500" overall length 4.400" overall width 0.063" material thickness opposite -17
01-152-6447
Structural Component Air Support
7.300" overall length 4.400" overall width 0.063" material thickness
01-152-6448
Structural Component Air Support
10.000" overall length 3.900" overall width 0.063" material thickness
01-152-6449
Structural Component Air Support
12.500" overall length 4.500" overall width 0.063" material thickness opposite -22
01-152-6450
Structural Component Air Support
12.500" overall length 4.500" overall width 0.063" material thickness opposite -21
01-152-6451
Structural Component Air Support
7.500" overall length 4.500" overall width 0.063" material thickness opposite -24
01-152-6452
Structural Component Air Support
7.500" overall length 4.500" overall width 0.063" material thickness opposite -23
01-152-6453
Structural Component Air Support
7.500" overall length 4.500" overall width 0.063" material thickness opposite -26
01-152-6454
Structural Component Air Support
16.500" overall length 9.000" overall width dim are stock material; machine from PH13-8M0 cres bar per AMS5629, type 1, sol treated; ht per H1000 per AMS2759; -503 opposite -504
01-152-6455
Structural Component Air Support
01-152-6456
Structural Component Air Support
01-152-6457
Structural Component Air Support
01-152-6458
Structural Component Air Support
Opp -39
01-152-6459
Aircraft Frame
U/a: frame assy; opposite -512
01-152-6460
Aircraft Frame
U/a: frame assy; opposite -511
01-152-6461
Aircraft Frame
U/a: frame assy; opposite -514
01-152-6462
Aircraft Frame
U/a: frame assy; opposite -513
01-152-6463
Structural Component Air Support
7.500" overall length 4.500" overall width 0.063" material thickness opp 35-15322-25; used as intercostal-intermediate
01-152-6464
Structural Component Air Support
7.500" overall length 4.500" overall width 0.063" material thickness opp 35-15322-28; used as intercoastal, intermediate
01-152-6465
Structural Component Air Support
7.500" overall length 4.500" overall width 0.063" material thickness opp 35-15322-27; used as intercoastal, intermediate
01-152-6466
Structural Component Air Support
7.600" overall length 3.300" overall width 0.063" material thickness opp 35-15322-30; used as intercoastal, intermediate
01-152-6467
Structural Component Air Support
Used on acft model c/kc-135. corrosion resistant steel forged block 15-5ph per ams 5659; heat treated to 180-200 ksi per bac 5619; c/o 1 fitting, 2 bushings
01-152-6469
Structural Component Air Support
Used on acft model c/kc-135. corrosion resistant steel forging 15-5ph per ams 5659; finish f-8.07; heat treated to 155-170 ksi per BAC5619; c/o 1 fitting, 1 bearing; opposite p/n -2
01-152-6470
Aircraft Channel
70.000" overall length 2.900" overall width 0.040" material thickness u/a: frame channel; opp -530; matl: clad sht; 0 temper
01-152-6471
Aircraft Channel
70.000" overall length 2.900" overall width 0.040" material thickness u/a: frame channel; opp -529; matl:clad sht; 0 temper
01-152-6472
Aircraft Channel
70.000" overall length 2.900" overall width 0.040" material thickness u/a: frame channel; matl: clad sht; 0 temper; opposite -532
01-152-6473
Aircraft Channel
70.000" overall length 2.900" overall width 0.040" material thickness u/a:frame channel; matl: clad sht, 0 temper; opposite -531
01-152-6474
Structural Component Air Support
01-152-6475
Structural Component Air Support
01-152-6476
Structural Component Air Support
01-152-6477
Structural Component Air Support
Used on acft model c/kc-135. corrosion resistant steel forging 15-5ph per AMS5659; heat treated to 155-170 ksi per BAC5619; finish f-8.07; opposite p/n -1
01-152-6480
Structural Component Air Support
Used on acft model b52. used on inboard
01-152-6481
Structural Component Air Support
Stl 4340 per bms 7-28, used on aft firewall tension latch
01-152-6482
Structural Component Air Support
Stl 4340 per bms 7-28; used on aft firewall latch tension
01-152-6483
Structural Component Air Support
6.900" overall length 5.500" overall width 5.000" material thickness used on aft firewall tension latch; matl 4340 per BMS7-28
01-152-6484
Structural Component Air Support
6.900" overall length 5.500" overall width 5.000" material thickness used on aft firewall tension latch; matl 4340 per BMS7-28
01-152-6485
Structural Component Air Support
Used on nose cowl split, weldment; c/o: bracket 39-11727-1, tube 39-11727-2
01-152-6487
Structural Component Air Support
Used on acft model c/kc-135. aluminum die forging 7075-T73 per BMS7-186; finish f-2.47 except omit primer in housing bore; 3.300 in. lg, 3.000 in. w, 1.680 in. thk; made from -3 forging
01-152-6489
Structural Component Air Support
01-152-6527
Aircraft Former
1.700" overall length 1.400" overall width 0.032" material thickness temper 0; heat treat T4; finish f-2.115; opp -834
01-152-6528
Aircraft Former
4.900" overall length 1.100" overall width 0.040" material thickness
01-152-6529
Aircraft Former
Opposite 35-10704-59
01-152-6530
Aircraft Former
6.300" overall length 2.200" overall width 0.040" material thickness
01-152-6531
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 -99
01-152-6532
Aircraft Former
8.100" overall length 4.600" overall width 0.063" material thickness
01-152-6533
Aircraft Channel
8.100" overall length 4.600" overall width 0.063" material thickness matl; clad al aly sht, o temp, ht T4; fin: F2.115; opp -101
01-152-6534
Aircraft Former
39.000" overall length 8.000" overall width manufacturer suggested name: angle; opp -93; matl: BAC1490-39X8.0, clad al aly sht, o temp, ht T4; fin F2.115
