01-159-3388
Elevator Balance Weight
01-159-3389
Elevator Balance Weight
01-159-3390
Elevator Balance Weight
01-159-3391
Elevator Balance Weight
01-159-3392
Elevator Balance Weight
01-159-3393
Elevator Balance Weight
01-159-3394
Elevator Balance Weight
01-159-3395
Elevator Balance Weight
01-159-3396
Elevator Balance Weight
01-159-3398
Elevator Balance Weight
01-159-3399
Elevator Balance Weight
01-159-3400
Elevator Balance Weight
01-159-3401
Elevator Balance Weight
Used on acft model c/kc-135. 1020 or 1025 steel bar per mil-s-7952; finish cadmium plate per qq-p-416; 16.100 in. lg, 5.500 in. w, 0.375 in. thk; weight 29.0-29.5; opposite p/n -3016; used as a balance weight on elevator panel
01-159-3402
Elevator Balance Weight
Used on acft model c/kc-135. 1020 or 1025 steel bar per mil-s-7952; finish cadmium plate per qq-p-416; 18.500 in. lg, 5.500 in. w, 0.375 in. thk; weight 29.5-30.0; opposite p/n -3017; used as balance weight on elevator panel
01-159-3409
Structural Aircraft Plate
Used on C-130.
01-159-3410
Thermal Special Purpo Insulation
C-130
01-159-3412
Structural Component Air Fitting
4.000" overall length 2.750" overall width 2.250 " material thickness
01-159-3413
Structural Component Air Fitting
4.000" overall length 2.750" overall width 2.250 " material thickness
01-159-3415
Structural Component Air Support
01-159-3419
Structural Component Air Support
01-159-3464
Structural Aircraft Panel
Used on b-1b aircraft. consist of six component parts
01-159-3465
Structural Aircraft Plate
Used on c/kc-135 aircraft. effective for acft with 64-1071-14 fairing splice deleted; material-2024-T3 clad al. sht. per qq-a-250/5
01-159-3466
Structural Aircraft Plate
21.000" overall length 12.000" overall width 0.040" material thickness 6A1-4v; opposite pn 25-2303-19
01-159-3467
Structural Aircraft Plate
20.000" overall length 8.000" overall width 6A1-4v; opposite pn 25-2303-20; used as doubler
01-159-3468
Structural Aircraft Plate
9.700" overall length 2.300" overall width 0.063" material thickness optional full hard, cond 2b
01-159-3469
Structural Aircraft Plate
9.000" overall length 7.500" overall width 0.020" material thickness optional full hard, cond 2b
01-159-3470
Structural Aircraft Plate
Used on B-52.
01-159-3471
Structural Aircraft Plate
7.700" overall length 3.200" overall width 0.063" material thickness optinal full hard, cond 2b
01-159-3472
Structural Aircraft Plate
Used on B-52.
01-159-3473
Structural Aircraft Plate
4.000" overall length 2.000" overall width 0.020" material thickness
01-159-3474
Structural Aircraft Plate
22.800" overall length 14.000" overall width 0.063" material thickness optional full hard, surface cond 2b
01-159-3475
Structural Aircraft Plate
27.300" overall length 2.500" overall width 0.020" material thickness
01-159-3484
Aircraft Former
8.300" overall length
01-159-3485
Aircraft Former
8.300" overall length
01-159-3489
Airfoil Rib
26.000" overall length 22.000" overall width 0.080" material thickness
01-159-3490
Airfoil Rib
26.000" overall length 22.000" overall width 0.080" material thickness
01-159-3492
Airfoil Rib
26.000" overall length 22.000" overall width 0.080" material thickness
01-159-3494
Airfoil Rib
32.000" overall length 6.000" overall width 1.125" material thickness
01-159-3495
Airfoil Rib
21.000" overall length 6.000" overall width 2.000" material thickness
01-159-3496
Airfoil Rib
21.000" overall length 6.000" overall width 2.000" material thickness
01-159-3497
Airfoil Rib
21.000" overall length 6.000" overall width 2.000" material thickness
01-159-3498
Airfoil Rib
21.000" overall length 6.000" overall width 2.000" material thickness
01-159-3499
Aircraft Skin
Used on B-52. 8.000" overall length 5.000" overall width
01-159-3500
Aircraft Skin
Used on B-52. 8.000" overall length 5.000" overall width opposite p/n 25-2303-809
01-159-3501
Aircraft Skin
Used on B-52. 35.000" overall length 8.000" overall width
01-159-4133
Access Aircraft Cover
Used on F-16. dorsal fairing access
01-159-4136
Access Aircraft Cover
Used on f-16 aircraft.
01-159-4190
Aircraft Fairing
0.120" material thickness dorsal tip fairing assembly
01-159-4260
Aircraft Former
7.000" overall length 2.000" overall width 0.071" material thickness used on -1
01-159-4443
Structural Component Air Bracket
