01-149-0391
Structural Aircraft Plate
6.300" overall length 2.200" overall width 0.080" material thickness finish f-2.115; opposite p/n -19
01-149-0392
Structural Aircraft Plate
6.400" overall length 2.200" overall width 0.080" material thickness finish f-2.115; opposite p/n -22
01-149-0393
Structural Aircraft Plate
6.400" overall length 2.200" overall width 0.080" material thickness finish f-2.115; opposite p/n -21
01-149-0394
Structural Aircraft Plate
5.200" overall length 2.000" overall width 0.080" material thickness finish f-2.115;
01-149-0395
Structural Aircraft Plate
40.500" overall length 7.500" overall width 0.080" material thickness finish f-2.115
01-149-0396
Structural Aircraft Plate
40.500" overall length 7.500" overall width 0.085" material thickness finish f-2.115
01-149-0397
Structural Aircraft Plate
40.500" overall length 7.500" overall width 0.085" material thickness finish f-2.115
01-149-0400
Structural Aircraft Plate
Used on acft model b-52. used on tail fairing installation left hand inboard strut
01-149-0401
Structural Aircraft Plate
Matl al alloy extruded; opposite p/n 25-2600-17; used as angle
01-149-0402
Structural Aircraft Plate
Matl al alloy extruded; used as angle
01-149-0403
Structural Aircraft Plate
Matl al alloy extruded; opposite p/n 25-2600-6; used as tee
01-149-0404
Structural Aircraft Plate
Matl al alloy extruded; opposite p/n 25-2600-5; used as tee
01-149-0405
Structural Aircraft Plate
Matl al alloy extruded; opposite p/n 25-2600-8; used as angle
01-149-0406
Structural Aircraft Plate
Matl al alloy extruded; opposite p/n 25-2600-7; used as tee
01-149-0407
Structural Aircraft Plate
01-149-0408
Structural Aircraft Plate
01-149-0409
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy per 2024 qq-a-250/5, 8.500 in. lg, 1.800 in. w, 0.063 in. thk, located upper station 254.3
01-149-0410
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy per 2024-0 qq-a-250/5, 8.500 in. lg, 1.800 in. w, 0.063 in. thk, located upper station 254.3
01-149-0411
Structural Aircraft Plate
11.600" overall length 1.900" overall width 0.080" material thickness used as splice plate on firewall installation; matl 8630 steel
01-149-0412
Structural Aircraft Plate
Used on acft model b-52.
01-149-0414
Structural Aircraft Plate
5.000" overall length 2.000" overall width 0.063" material thickness
01-149-0415
Structural Aircraft Plate
23.000" overall length 7.700" overall width 0.032" material thickness
01-149-0416
Structural Aircraft Plate
8.700" overall length 8.700" overall width 0.063" material thickness
01-149-0417
Structural Aircraft Plate
Used on acft model b52. al clad 2024-0 per qq-a-250/5, 0.071 in.thk, 6.700 in.w, 8.200 in.lg, left hand, located station 287.81, tail fairing
01-149-0418
Structural Aircraft Plate
7.880" overall length 2.160" overall width
01-149-0419
Structural Aircraft Plate
7.880" overall length 2.160" overall width
01-149-0420
Structural Aircraft Plate
10.500" overall length 2.250" overall width 0.875" material thickness
01-149-0421
Structural Aircraft Plate
10.500" overall length 2.250" overall width 0.875" material thickness
01-149-0422
Structural Aircraft Plate
Used on acft model b52. steel 350, 0.040 in.thk, 7.200 in.w, 11.600 in.lg, used on forward engine mount
01-149-0424
Structural Aircraft Plate
Used on acft model b52. steel 350, c/o web 1 ea p/n 29-2448-2, clip 1 ea p/n 29-2448-5, nutplate 36 p/n MK2000-1032, left hand
01-149-0426
Structural Component Air Support
12.000" overall length 3.000" overall width 0.063" material thickness
01-149-0427
Structural Component Air Bracket
Clip make from bac-1503-100119 spec material; finish per F2.3
01-149-0428
Structural Component Air Support
17.000" overall length 16.000" overall width 0.040" material thickness
01-149-0429
Structural Component Air Bracket
2.200" overall length 1.500" overall width 0.071" material thickness 0 temper, heat treat T6; finish f-2.115; c/o 2 nutplate, 1 bracket; opp -2
01-149-0430
Structural Component Air Support
5.200" overall length 4.800" overall width 0.063" material thickness
01-149-0431
Structural Component Air Support
C/o 1 fitting, 1 pin
01-149-0455
Aircraft Former
10.600" overall length 3.000" overall width 0.063" material thickness
01-149-0456
Aircraft Former
11.400" overall length 0.660" overall width 0.100" material thickness
01-149-0457
Aircraft Former
1.500" overall length 0.500" overall width 0.028" material thickness
01-149-0458
Aircraft Former
1.700" overall length 1.000" overall width 0.032" material thickness finish f-2.115
01-149-0459
Aircraft Former
Used on B-52.
01-149-0460
Aircraft Former
Used on B-52.
01-149-0461
Aircraft Former
38.000" overall length 0.040" material thickness
01-149-0462
Aircraft Former
Used on B-52. opposite 25-2308-13
01-149-0463
Aircraft Former
6.700" overall length 1.300" overall width 0.020" material thickness opposite 25-2600-1
01-149-0464
Aircraft Former
6.350" overall length 1.150" overall width 0.032" material thickness opposite 25-2600-21
01-149-0465
Aircraft Former
6.350" overall length 1.150" overall width 0.032" material thickness opp 25-2600-20
01-149-0466
Aircraft Former
6.700" overall length 1.300" overall width 0.020" material thickness
01-149-0467
Aircraft Former
1.200" overall length 2.400" overall width 0.080" material thickness
01-149-0468
Aircraft Former
Extruded; opp 25-2600-10
