01-148-0519
Structural Aircraft Plate
2.500" overall length 0.600" overall width 0.032" material thickness
01-148-0520
Structural Aircraft Plate
20.100" overall length 18.500" overall width 0.100" material thickness
01-148-0521
Structural Aircraft Plate
Used as doubler
01-148-0522
Structural Aircraft Plate
3.600" overall length 1.250" overall width 0.040" material thickness aisi 17-7ph per bms 7-12a; heat treated to 180, 000 to 200, 000 psi
01-148-0523
Structural Aircraft Plate
10.200" overall length 3.700" overall width 0.016" material thickness
01-148-0524
Structural Aircraft Plate
01-148-0525
Structural Aircraft Plate
01-148-0526
Structural Aircraft Plate
52.800" overall length 38.500" overall width 0.016" material thickness
01-148-0527
Structural Aircraft Plate
48.400" overall length 37.100" overall width 0.016" material thickness
01-148-0528
Structural Aircraft Plate
1.750" overall length 1.080" overall width 0.062" material thickness matl BAC1524-6255
01-148-0529
Structural Aircraft Plate
2.400" overall length 1.600" overall width 0.025" material thickness
01-148-0530
Structural Aircraft Plate
6.000" overall length 4.300" overall width 0.030" material thickness
01-148-0531
Structural Aircraft Plate
6.000" overall length 4.300" overall width 0.030" material thickness
01-148-0532
Structural Aircraft Plate
12.600" overall length 3.300" overall width 0.063" material thickness function angle
01-148-0533
Structural Aircraft Plate
12.600" overall length 3.300" overall width 0.063" material thickness function angle
01-148-0534
Structural Aircraft Plate
11.800" overall length 10.000" overall width 0.320" material thickness aisi 17-7 ph per bms 7-12a; heat treated to 180, 000 to 200, 000 psi; finish f-8.05
01-148-0535
Structural Aircraft Plate
6.600" overall length 3.300" overall width 0.025" material thickness
01-148-0536
Structural Aircraft Plate
Used on b-52 aircraft. function-splice plate, right hand; material-2024-T3 clad aluminum per qq-a-250/5
01-148-0537
Structural Aircraft Plate
Used on b-52 aircraft. material-cres steel sheet aisi 301 mil-s-5059, comp d 1/4 hard, surf cond 2b; location-tail fairing installation-outboard strut
01-148-0538
Aircraft Fairing
C/o 1 bond assy, 5 seal retainers, 10 rubber seals, 1 retainer, 2 latch assemblys, misc hardware
01-148-0539
Aircraft Fairing
01-148-0540
Aircraft Fairing
01-148-0541
Aircraft Fairing
01-148-0542
Aircraft Fairing
01-148-0543
Aircraft Fairing
01-148-0544
Aircraft Fairing
27.000" overall length 6.600" overall width 0.080" material thickness
01-148-0545
Structural Component Air Support
Used on b-52 acft. matl al alloy, qq-a-364, 2024-0; matl size 0.063 by 1.000 by 1.600 in. lg; used as attachment angle on tail fairing lh inboard strut
01-148-0546
Structural Component Air Support
Used on b-52 acft. matl al alloy, qq-a-364, 2024-0 clad; matl size 0.063 by 1.200 by 1.300 in. lg; opposite to p/n 23-1605-2; used as attachment angle on tail fairing lh inboard strut station 280.65
01-148-0547
Structural Component Air Support
Used on b-52 acft. matl al alloy, qq-a-362, 2024-T3; matl size 0.063 by 4.250 by 6.100 in. lg; 0.625 in. dia hole; used as support pressure line
01-148-0548
Structural Component Air Support
Used on acft model b52. c/o tube 1 ea p/n 25-2323-1, fitting 2 ea p/n 25-2669, used to connect engine to wing
01-148-0549
Structural Component Air Support
C/o 1 tube, 2 fitting
01-148-0550
Structural Component Air Support
C/o 45 component parts
01-148-0551
Structural Component Air Support
C/o 52 compontent parts
01-148-0552
Structural Component Air Support
01-148-0553
Structural Component Air Support
54.500" overall length 17.200" overall width 0.063" material thickness
01-148-0554
Structural Component Air Support
01-148-0555
Structural Component Air Support
54.500" overall length 17.200" overall width 0.063" material thickness
01-148-0556
Structural Component Air Support
01-148-0557
Structural Component Air Support
6.100" overall length 2.800" overall width 0.028" material thickness
01-148-0558
Structural Component Air Support
6.100" overall length 2.800" overall width 0.028" material thickness
01-148-0559
Structural Component Air Support
Used on b-52 aircraft. function-attach tee; material-2024-T4 extruded per qq-a-200/3
01-148-0560
Structural Component Air Support
Used on b-52 aircraft. function-attach tee; material-2024-T4 extruded per qq-a-200/3
01-148-0584
Aircraft Former
3.400" overall length 0.500" overall width 0.150" material thickness
01-148-0585
Aircraft Former
7.400" overall length 2.400" overall width 0.030" material thickness
01-148-0586
Aircraft Former
7.400" overall length 2.400" overall width 0.030" material thickness
01-148-0587
Aircraft Former
6.800" overall length 3.000" overall width 0.030" material thickness
01-148-0588
Aircraft Former
6.800" overall length 3.000" overall width 0.030" material thickness
01-148-0589
Aircraft Former
6.400" overall length 3.000" overall width 0.030" material thickness
01-148-0590
Aircraft Former
6.400" overall length 3.000" overall width 0.030" material thickness
01-148-0591
Aircraft Former
7.000" overall length 2.900" overall width 0.030" material thickness
