01-151-6713
Aircraft Former
10.500" overall length 10.200" overall width 0.025" material thickness opposite -51; used on -516, -522.and -545
01-151-6714
Aircraft Former
1.100" overall length 0.700" overall width 0.100" material thickness tempered T3; finish f-2.115
01-151-6715
Aircraft Former
44.500" overall length 11.000" overall width 0.040" material thickness heat treat T4; finish f-2.115
01-151-6716
Aircraft Former
30.000" overall length 2.000" overall width 0.040" material thickness used on -516, -522
01-151-6717
Structural Component Air Bracket
01-151-6718
Aircraft Former
39.900" overall length 1.400" overall width 0.025" material thickness finish f-10.10
01-151-6719
Structural Component Air Bracket
01-151-6720
Structural Component Air Bracket
01-151-6721
Aircraft Former
3.000" overall length 2.800" overall width 0.063" material thickness used on -516, -522
01-151-6722
Aircraft Former
3.000" overall length 0.900" overall width 0.063" material thickness opposite -835; used on -516, -522
01-151-6723
Aircraft Former
25.000" overall length 0.500" overall width 0.032" material thickness
01-151-6724
Aircraft Former
24.000" overall length 2.000" overall width 0.050" material thickness
01-151-6725
Aircraft Former
30.500" overall length make from BAC1493-550
01-151-6726
Aircraft Former
16.300" overall length make from BAC1493-218
01-151-6727
Aircraft Former
Used on acft model b-52.
01-151-6729
Longeron
Used on B-52. heat treated to 180, 000 to 200, 000 psi; c/o 1 forward
01-151-6730
Airfoil Rib
C/o 1 angle, 1 doubler, 1 rib; opposite -3013
01-151-6731
Airfoil Rib
14.900" overall length opposite -1
01-151-6733
Aircraft Skin
Used on b-52 aircraft. used as fillet skin on fairing installation fillet, inboard strut; matl-titanium per spec ams 4901 optional spec BMS7-7c; dimensions-57.000 in. lg, 17.500 in. w, 0.025 in. thk
01-151-6734
Aircraft Skin
Used on b-52 aircraft. used as fillet skin on fairing installation, fillet, inboard strut; opposite p/n 25-2345-51
01-151-6735
Aircraft Skin
Used on B-52. 34.000" overall length 24.000" overall width
01-151-6736
Aircraft Skin
Used on B-52. 19.000" overall length 17.000" overall width
01-151-6737
Aircraft Skin
Used on B-52. 12.000" overall length 8.500" overall width
01-151-7677
Aircraft Bulkhead
28.000" overall length 24.000" overall width 0.025" material thickness pure titanium ams 4900, annealed
01-151-7687
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy clad 2024-0 qq-a-250/5, 17.500 in. lg, 1.800 in. w, 0.063 in. thk
01-151-7688
Structural Aircraft Plate
36.000" overall length 1.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -232
01-151-7689
Structural Aircraft Plate
36.000" overall length 1.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -231
01-151-7690
Structural Aircraft Plate
66.000" overall length 10.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -234
01-151-7691
Structural Aircraft Plate
66.000" overall length 10.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -233
01-151-7692
Structural Aircraft Plate
Used on B-52.
01-151-7694
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy clad 2024-0 qq-a-250/5, 2.000 in. lg, 2.000 in. w, 0.032 in. thk
01-151-7698
Aircraft Former
3.500" overall length 3.000" overall width 0.050" material thickness heat treat 180, 000-200, 000 psi; finish f-8.05
01-151-7699
Aircraft Former
2.000" overall length 1.500" overall width 0.063" material thickness
01-151-7703
Aircraft Skin
Used on acft model b-52. steel cres sheet per aisi 302 mil-s-5059 comp 302 surf cond 2d annealed, 29.000 in. lg, 2.000 in. w, 0.032 in. thk
01-151-8413
Aircraft Spar
01-151-8414
Structural Component Aircraf Web
01-151-8417
Structural Component Air Support
2.200" overall length 2.200" overall width 0.050" material thickness
01-151-8418
Structural Component Air Support
2.300" overall length 2.200" overall width 0.050" material thickness
01-151-8420
Aircraft Fairing
12.500" overall length 3.500" overall width 0.032" material thickness
01-151-8421
Aircraft Fairing
12.500" overall length 3.500" overall width 0.032" material thickness
01-151-8425
Structural Aircraft Panel
Used on B-52. 35.400" overall length 24.400" overall width
01-151-8426
Structural Aircraft Panel
Used on B-52.
01-151-8427
Structural Aircraft Panel
Opposite 35-10704-1
01-151-8428
Structural Aircraft Plate
Used on B-52.
01-151-8429
Structural Aircraft Plate
Used on B-52.
01-151-8430
Structural Aircraft Plate
24.000" overall length 6.000" overall width 0.040" material thickness
01-151-8431
Structural Aircraft Plate
24.000" overall length 6.000" overall width 0.040" material thickness
01-151-8432
Structural Aircraft Plate
22.000" overall length 6.500" overall width 0.040" material thickness
01-151-8433
Structural Aircraft Plate
22.000" overall length 6.500" overall width 0.040" material thickness
01-151-8434
Structural Aircraft Plate
6.500" overall length 6.300" overall width 0.100" material thickness
