01-150-2558
Aircraft Skin
Used on B-52. 54.000" overall length 20.000" overall width
01-150-2559
Aircraft Skin
Used on B-52. 54.000" overall length 20.000" overall width
01-150-2560
Aircraft Skin
Used on B-52. 9.000" overall length 7.000" overall width
01-150-2561
Aircraft Skin
Used on B-52. 1/2 hard surface condition 2b
01-150-2562
Aircraft Skin
Used on B-52. 1/2 hard surface condition 2b
01-150-2938
Rotary Rudder Boom
01-150-4134
Aircraft Skin
Used on b-52 aircraft. location-tail fairing installation, right hand inboard strut
01-150-5152
Structural Component Air Bracket
2.300" overall length 1.300" overall width u/o -516, -522, -545
01-150-5153
Structural Component Air Bracket
2.300" overall length 1.300" overall width u/o -516, -522, -545
01-150-5170
Structural Aircraft Plate
50.000" overall length 19.800" overall width 0.016" material thickness used on- -516, -522
01-150-5171
Structural Aircraft Plate
12.000" overall length 4.000" overall width 0.050" material thickness
01-150-5172
Structural Aircraft Plate
82.000" overall length 2.500" overall width 0.016" material thickness finish f-10.10; opposite pn -38
01-150-5173
Structural Aircraft Plate
82.000" overall length 2.500" overall width 0.016" material thickness ffinish f-10.10; opp pn -37
01-150-5174
Structural Aircraft Plate
1.800" overall length 1.300" overall width 0.032" material thickness finish f-10.10
01-150-5175
Structural Aircraft Plate
6.100" overall length 1.800" overall width 0.063" material thickness finish f-2.115
01-150-5176
Structural Aircraft Plate
4.600" overall length 1.100" overall width 0.040" material thickness decarb limit per ams 6350; heat treated 180, 000 to 200, 000; opposite pn -510; annealed
01-150-5177
Structural Aircraft Plate
82.000" overall length 2.500" overall width 0.016" material thickness finish f-10.10; opposite pn -524
01-150-5178
Structural Aircraft Plate
47.000" overall length 2.500" overall width 0.016" material thickness finish f-10.10; opposite pn-526
01-150-5179
Structural Aircraft Plate
47.000" overall length 2.500" overall width 0.016" material thickness finish f-10.10; opposite pn -525
01-150-5180
Structural Aircraft Plate
82.000" overall length 2.500" overall width 0.012" material thickness finish f-8.05; opposite pn -528
01-150-5181
Structural Aircraft Plate
47.000" overall length 2.500" overall width 0.012" material thickness finish f-8.05; opposite pn -530
01-150-5182
Structural Aircraft Plate
47.000" overall length 2.500" overall width 0.012" material thickness finish f-8.05; opposite pn -529
01-150-5184
Structural Component Air Support
6.500" overall length 4.200" overall width 0.050" material thickness bracket; used on -516, -522, & -545; finish f-2.115
01-150-5185
Structural Component Air Support
3.000" overall length 2.400" overall width 0.040" material thickness
01-150-5190
Aircraft Former
5.600" overall length 1.600" overall width 0.032" material thickness channel; finish f-2.115; used on -516, -522 & -545; heat treated to T4; clad
01-150-5191
Aircraft Former
4.600" overall length 2.500" overall width 0.063" material thickness opposite -842; used on -516, -522
01-150-5192
Aircraft Former
4.600" overall length 2.500" overall width 0.063" material thickness opposite -841; used on -516, -522, and -545; finish f-2.10; heat treated to T4; channel
01-150-5193
Structural Component Air Bracket
01-150-5194
Structural Component Air Bracket
01-150-5195
Structural Component Air Bracket
01-150-5196
Aircraft Former
5.600" overall length 1.100" overall width 0.071" material thickness
01-150-5197
Aircraft Former
20.000" overall length 1.400" overall width 0.040" material thickness annealed; decarb limit, ams 6350; heat treated 180, 000 to 200, 000; opposite p/n -503
01-150-5198
Aircraft Former
49.600" overall length 2.100" overall width 0.040" material thickness annealed; decarb limit, ams 6350; heat treated 180, 000 to 200, 000; opposite p/n -506
01-150-5199
Aircraft Former
49.600" overall length 2.100" overall width 0.040" material thickness annealed; decarb limit, ams 6350; heat treated 180, 000 to 200, 000; opposite p/n -505
01-150-5200
Aircraft Former
26.000" overall length 2.800" overall width 0.040" material thickness annealed; decarb limit, ams 6350; heat treated 180, 000 to 200, 000; opposite p/n -508
01-150-5201
Aircraft Former
26.000" overall length 2.800" overall width 0.040" material thickness annealed; decarb limit, ams 6350; heat treated 180, 000 to 200, 000; opposite p/n -507
01-150-5202
Aircraft Former
30.000" overall length 1.100" overall width 0.040" material thickness annealed; decarb limit, ams 6350; heat treated 180, 000 to 200, 000; opposite p/n -512
01-150-5203
Aircraft Former
30.000" overall length 1.100" overall width 0.040" material thickness annealed; decarb limit, ams 6350; heat treated 180, 000 to 200, 000; opposite p/n -511
01-150-5204
Aircraft Former
2.600" overall length 2.400" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -518
01-150-5205
Aircraft Former
2.600" overall length 2.400" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -517
01-150-5206
Aircraft Former
2.000" overall length 2.000" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -520
01-150-5207
Aircraft Former
2.000" overall length 2.000" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -519
01-150-5208
Longeron
42.000" overall length 6.000" overall width 0.040" material thickness commercially pure sheet; finish f-10.15; opposite pn -514
01-150-5209
Longeron
42.000" overall length 6.000" overall width 0.040" material thickness commercially pure sheet; finish f-10.15; opposite pn -513
01-150-5210
Longeron
55.000" overall length 6.000" overall width 0.040" material thickness commercially pure sheet, finish f-10.15; opposite pn -516
01-150-5211
Longeron
55.000" overall length 6.000" overall width 0.040" material thickness commercially pure sheet; finish f-10.15; opposite pn -515
01-150-5212
Aircraft Skin
Used on B-52.
01-150-5213
Aircraft Skin
Used on B-52. 85.000" overall length 15.000" overall width 1/2 hard surface condition 2b
01-150-5214
Aircraft Skin
Used on B-52. 85.000" overall length 15.000" overall width 1/2 hard surface condition 2b
01-150-5215
Aircraft Skin
Used on B-52. 25.000" overall length 11.000" overall width
