01-152-6374
Structural Aircraft Plate
16.000" overall length 0.700" overall width 0.040" material thickness heat treat T4
01-152-6375
Structural Aircraft Plate
16.000" overall length 0.700" overall width 0.400" material thickness heat treat T4
01-152-6376
Structural Aircraft Plate
16.000" overall length 0.700" overall width 0.040" material thickness heat treat T4
01-152-6377
Structural Aircraft Plate
16.000" overall length 0.700" overall width 0.040" material thickness heat treat T4
01-152-6387
Structural Aircraft Panel
Used on C-141. c/o cowl door assy, p/n 3P21602-379; fire detector instl, p/n 6681-2
01-152-6388
Structural Aircraft Panel
Used on C-14. c/o cowl door assy, p/n 3P21602-379; fire detector instl, p/n 6681-2
01-152-6389
Structural Aircraft Panel
Used on C-141. c/o cowl door assy, p/n 3P21702-171; fire detector instl, p/n 6680-2
01-152-6390
Structural Aircraft Panel
Used on C-141. c/o cowl door assy, p/n 3P21701-169; fire detector instl, p/n 6680-1
01-152-6399
Structural Aircraft Panel
Used on B-52.
01-152-6400
Structural Aircraft Panel
Used on B-52.
01-152-6401
Structural Aircraft Plate
Opposite to p/n 35-10720-138; used as angle extrusion, support installation
01-152-6402
Structural Aircraft Plate
11.200" overall length 0.750" overall width 0.068" material thickness 4130 steel per ams 6350
01-152-6403
Structural Aircraft Plate
38.000" overall length 1.200" overall width 0.020" material thickness used as seal on panel-engine wrap cowl, lower
01-152-6404
Structural Aircraft Plate
Used as seal on panel-engine wrap cowl, lower; opposite p/n 35-10704-5 5
01-152-6405
Structural Aircraft Plate
2.200" overall length 1.700" overall width 0.040" material thickness used as gusset on panel-engine wrap cowl, lower
01-152-6406
Structural Aircraft Plate
2.200" overall length 1.100" overall width 0.375" material thickness used as filler tapered on frame installation station 70.00, canted nose cowl
01-152-6407
Structural Aircraft Plate
Used as filler on frame installation station 70.00, canted nose cowl, opposite p/n 35-8642-107
01-152-6408
Structural Aircraft Plate
28.000" overall length 10.400" overall width 0.071" material thickness used as web on frame installation station 70.000, canted nose cowl
01-152-6409
Structural Aircraft Plate
16.000" overall length 6.000" overall width 0.020" material thickness cres stl 321 or 347
01-152-6410
Structural Aircraft Plate
19.400" overall length 1.300" overall width 0.016" material thickness used on-516, -522, and -545
01-152-6411
Structural Aircraft Plate
35.000" overall length 2.500" overall width 0.050" material thickness tempered to T3; finish f-2.115
01-152-6412
Structural Aircraft Plate
34.300" overall length 23.200" overall width 0.020" material thickness
01-152-6413
Structural Aircraft Plate
23.400" overall length 1.500" overall width 0.025" material thickness
01-152-6414
Structural Aircraft Plate
6.000" overall length 0.500" overall width 0.020" material thickness do not use cadmium plated tools on this item
01-152-6415
Structural Aircraft Plate
Used on B-52. 0.032" material thickness 17-7ph, annealed
01-152-6416
Structural Aircraft Plate
Used on B-52.
01-152-6417
Structural Aircraft Plate
89.400" overall length bac 1506-1347
01-152-6418
Structural Aircraft Plate
Used on B-52. pposite pn 35-8642-115
01-152-6419
Structural Aircraft Plate
Used on B-52. opposite pn 35-8462-11; used as web
01-152-6420
Structural Aircraft Plate
12.300" overall length 4.500" overall width 0.080" material thickness
01-152-6421
Structural Aircraft Plate
5.500" overall length 2.500" overall width 0.040" material thickness
01-152-6422
Structural Aircraft Plate
6.200" overall length 3.000" overall width 0.040" material thickness
01-152-6423
Structural Aircraft Plate
Used on B-52.
01-152-6424
Structural Aircraft Plate
Used on B-52.
01-152-6425
Structural Aircraft Plate
23.100" overall length 1.600" overall width 0.025" material thickness
01-152-6426
Structural Aircraft Plate
Used on B-52.
01-152-6427
Structural Aircraft Plate
Used on B-52. 2.500" overall length 2.500" overall width 0.400" material thickness laminated thermo-setting sheet, asbestos, phenolic resin
01-152-6428
Structural Aircraft Plate
Used on B-52. c/o web 1 ea p/n 35-8289-801, pad 2 ea
01-152-6429
Structural Aircraft Plate
Used on B-52. 2.100" overall length 2.100" overall width 0.200" material thickness laminated thermo-setting sheet, asbestos, phenolic resin
01-152-6430
Structural Aircraft Plate
84.000" overall length 3.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finihs f-8.05; opposite pn -124
01-152-6433
Structural Component Air Support
Used as intercostal aft on panel-engine wrap cowl, lower; opp 35-10704-53
01-152-6434
Structural Component Air Support
14.000" overall length 2.000" overall width 0.063" material thickness used as angle support on panel-engine wrap cowl, lower
01-152-6435
Structural Component Air Support
Opp -57
01-152-6436
Structural Component Air Support
01-152-6437
Structural Component Air Support
01-152-6438
Structural Component Air Support
7.700" overall length 4.200" overall width 0.063" material thickness
01-152-6439
Structural Component Air Support
7.500" overall length 4.200" overall width 0.063" material thickness opp 35-15322-12; used as intercoastal
01-152-6440
Structural Component Air Support
7.500" overall length 4.200" overall width 0.063" material thickness opp 35-15322-11; used as intercoastal
01-152-6441
Structural Component Air Support
7.500" overall length 4.400" overall width 0.063" material thickness opp 35-15322-14; used as intercoastal
01-152-6442
Structural Component Air Support
7.500" overall length 4.400" overall width 0.063" material thickness opp 35-15322-13; used as intercoastal
