01-150-7336
Structural Aircraft Plate
3.000" overall length 1.300" overall width 0.100" material thickness comp 4335
01-150-7337
Structural Aircraft Plate
11.660" overall length 1.170" overall width 0.550" material thickness laminated phenolic sheet hh-p-256 type 2 grade c, natural color
01-150-7338
Structural Aircraft Plate
Used on B-52. 11.700" overall length 1.350" overall width 0.500" material thickness laminated phenolic, sheet hh-p-256, type 2, grade c, natural color
01-150-7339
Structural Aircraft Plate
Used on acft model b52. do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.025 in.thk, 1.800 in.w, 18.800 in.lg, used on tail fairing, left hand, inboard strut
01-150-7340
Structural Aircraft Plate
23.000" overall length 10.000" overall width 0.020" material thickness do not use cadmium plated tools on this item; optional ams 4900 anld
01-150-7341
Structural Aircraft Plate
13.900" overall length 3.000" overall width 0.036" material thickness optional aisi 17-7ph per bms 7-12a; comp 350
01-150-7342
Structural Aircraft Plate
13.900" overall length 3.000" overall width 0.036" material thickness optional aisi 17-7ph per bms 7-12a; comp 350
01-150-7343
Structural Aircraft Plate
3.000" overall length 7.500" overall width 0.020" material thickness finish f-10.10
01-150-7344
Structural Aircraft Plate
2.000" overall length 8.500" overall width 0.020" material thickness finish f-10.10
01-150-7345
Structural Aircraft Plate
7.400" overall length 2.700" overall width 0.040" material thickness
01-150-7346
Structural Aircraft Plate
25.000" overall length 3.000" overall width 0.030" material thickness
01-150-7350
Structural Component Air Support
C/o 2 pad, 1 web
01-150-7351
Structural Component Air Support
C/o 2 pad, 1 web
01-150-7352
Structural Component Air Support
6.300" overall length 2.100" overall width 0.032" material thickness pure titanium mil-t-9046c, class 6, finish f-10.10; opposite -532
01-150-7353
Structural Component Air Support
6.300" overall length 2.100" overall width 0.032" material thickness pure titanium mil-t-9046c, class 6; finish f-10.10; opposite -531
01-150-7354
Structural Component Air Support
5.700" overall length 2.600" overall width 0.032" material thickness pure titanium per mil-t-9046c, class 6; finish f-10.10; opposite -534
01-150-7355
Structural Component Air Support
5.700" overall length 2.600" overall width 0.032" material thickness pure titanium per mil-t-9046c, class 6; finish f-10.10; opposite -533
01-150-7356
Structural Component Air Support
C/o 1 pad, 1 web
01-150-7357
Structural Component Air Support
4.600" overall length 1.600" overall width 0.040" material thickness cres st 4130 jper an-qq-s-685
01-150-7358
Structural Component Air Support
C/o 4 web
01-150-7359
Structural Component Air Support
4.600" overall length 1.600" overall width 0.040" material thickness stl 4130 per an-qq-s-685
01-150-7360
Structural Component Air Support
3.560" overall length 1.000" overall width c/o 1 angle, 2 gusset
01-150-7361
Structural Component Air Support
3.560" overall length 1.000" overall width c/o 1 angle, 2 gusset
01-150-7362
Structural Component Air Support
Stl 4130 per qq-s-685; c/o 1 web, 1 cap
01-150-7363
Structural Component Air Support
Stl 4130 per an-qq-s-685; c/o 1 web
01-150-7364
Structural Component Air Support
C/o 1 web, 1 strap
01-150-7365
Structural Component Air Support
C/o 1 web, 1 strap
01-150-7366
Structural Component Air Support
C/o 1 web, 2 pad
01-150-7367
Structural Component Air Support
C/o 1 web, 2 pad
01-150-7368
Structural Component Air Support
10.880" overall length 4.280" overall width
01-150-7369
Structural Component Air Support
5.100" overall length 3.300" overall width 0.125" material thickness plastic, phenolic laminate cotton-fabric base mil-p-15035
01-150-7370
Structural Component Air Support
8.700" overall length 3.000" overall width 1.000" material thickness stl 4340 per mil-s-5000
01-150-7371
Structural Component Air Support
C/o 1 strap, 1 web; make from stl 4130 per an-qq-s-685 debarb limit
01-150-7372
Structural Component Air Support
2.500" overall length 2.400" overall width 0.090" material thickness
01-150-7386
Aircraft Former
3.600" overall length 3.4000" overall width 0.032" material thickness heat treated 180, 000 to 200, 000 psi; opposite p/n -535; finish f-8.05
01-150-7387
Aircraft Former
Extrusion
01-150-7388
Aircraft Former
64.000" overall length alter basic 1515-514 extr.
01-150-7389
Aircraft Former
Used on B-52. opposite p/n 25-2321-503
01-150-7390
Aircraft Former
20.000" overall length
01-150-7391
Aircraft Former
Used on B-52. opposite p/n 25-2322-5
01-150-7392
Aircraft Former
28.500" overall length 3.200" overall width 0.032" material thickness opposite p/n 35-8229-104
01-150-7393
Aircraft Former
28.500" overall length 3.200" overall width 0.032" material thickness opposite p/n 35-8229-103
01-150-7394
Aircraft Former
12.400" overall length 2.600" overall width 0.050" material thickness
01-150-7395
Aircraft Former
33.000" overall length 31.000" overall width 0.050" material thickness
01-150-7396
Aircraft Former
30.000" overall length 16.000" overall width 0.050" material thickness
01-150-7397
Aircraft Former
24.000" overall length 5.000" overall width 0.040" material thickness
01-150-7400
Aircraft Former
Used on B-52. opposite 25-2322-507
01-150-7401
Aircraft Former
30.000" overall length 16.000" overall width 0.050" material thickness
01-150-7402
Aircraft Former
01-150-7403
Aircraft Former
Used on b-52 acft. opposite 35-8229-111
