01-281-8573
Structural Aircraft Panel
Panel, lower-fwd equipment bay
01-281-8584
Aircraft Former
Used on KC-135. ht tr T4; finish f-2.115; bac 1490-2640 by 28.0 in. lg; opposite -1107; nha 5-71746
01-281-8585
Aircraft Former
Used on KC-135. ht tr T4; finish f-2.115; bac 1490-2640 by 28.0 in. lg; opposite -1106; nha 5-71746
01-281-8586
Aircraft Former
19.800" overall length 5.000" overall width 0.081" material thickness ht tr T4; finish f-2.115; nha 5-71741
01-281-8588
Airfoil Rib
5.400" overall length 5.000" overall width 0.051" material thickness 0 temper, heat treat T4; finish f-2.115; opp -18; nha 5.71741
01-281-8589
Aircraft Spar
01-281-8590
Aircraft Spar
01-281-8591
Aircraft Window Panel
Nuclear hardness critical item; consist of 1 shield assy, 1 wire harness, 2 bracket, 2 nutplate, 2 screw, 2 clamp, 2 washer; nha L5305301
01-281-8592
Aircraft Window Panel
Nuclear hardness critical item; consist of 1 shield, 3 seal, 4 washer, r t-knobs; nha L5305330
01-281-8593
Aircraft Window Panel
Nuclear hardness critical item; consist of 1 retainer, 1 glove, 4 seal, 4 receptacle, 6 nut, 2 pin, 2 washer, 1 shield, 1 doubler, 2 bulb seal; nha L5305301
01-281-8594
Aircraft Window Panel
Nuclear hardness critical item; consist of 1 retainer, 1 glove, 3 seal, 4 receptacle, 6 nut, 2 pin, 2 washer, 1 shield, 1 doubler; nha L5305301
01-281-8595
Aircraft Window Panel
Nuclear hardness critical item; consist of 1 retainer, 1 glove, 4 seal, 4 receptacle, 6 nut, 2 pin, 2 washer, 2 bulb seal, 1 shield, 1 doubler; nha L5305301
01-281-9179
Structural Component Air Support
01-281-9180
Structural Component Air Support
01-281-9249
Structural Component Air Support
3.550" overall width
01-281-9453
Structural Aircraft Plate
Used on F-15. T81
01-281-9882
Structural Aircraft Plate
Make from BAC1512-3404 by 1.9 in; heat treat T42; finish SRF2.30
01-281-9883
Structural Component Air Support
Used on acft model b-52.
01-281-9884
Aileron Balance Weight
Used on acft model kc-135. architectural bronze, revere 283 or equiv; chemical; CU56.5 ZN4.25 lead 2.25; finish f-4.30; 22.00 in lg, 2.35 in wd, 0.11 in thk; nha 3-96128; used on outboard aileron balance panel, balance weight
01-281-9887
Aircraft Leading Edge
Nuclear hardness critical item; c/o 1 skin, 2 stringer, 2 doubler, 1 leaading edge, 16 rib, 32 shim, 1 panel assy, 2 skin assy; nha L2300302
01-281-9888
Longeron
Used on f-16a aircraft. functional description:longeron, lower-FS158 to FS189;
01-281-9889
Aircraft Tip
C/o 1 clip, 1 support assy, 16 bracket, 2 nutplate, 1 frame, 2 door, misc hardwr; nuclear hardnes critical
01-281-9890
Aircraft Tip
Nuclear hardness critical item; c/o 2 filler, 3 shim, 1 leading edge tip assy, 1 cap, , 5 door, 10 frame, 11 clip, 2 gusset, 2 skin, 6 rib, 3 support, 3 retainer, 16 bracket, misc hardware
01-282-0093
Aircraft Windshield Panel
Bullet resistant; color to be green or clear
01-282-0288
Aircraft Fairing
01-282-0289
Structural Component Air Support
Used on f-16a aircraft.
01-282-0290
Structural Component Air Support
01-282-0291
Structural Component Air Support
Used on c-130 acft. channel p/o support beam assy-gasturbine compressor, int dr actuator
01-282-0298
Aircraft Skin
01-282-0640
Airframe Modification Kit
Used on uh-60 blackhawk airframe.
01-282-1028
Wing Dive Brake Flap
Flap, wing, leading edge
01-282-1029
Wing Dive Brake Flap
Flap, leading edge, wing
01-282-1610
Structural Component Air Fitting
Arresting hook fitting
01-282-2639
Metal Molding
01-282-2955
Aircraft Skin
01-282-3457
Access Aircraft Door
Item includes four snap rings; four grommets; four studs chromate surface treated
01-282-3569
Control Surface Aircraft Fairing
Used on aircraft model av-8. cognizant service:navy;
01-282-3570
Aircraft Fairing
01-282-3571
Pylon Aircraft Fairing
Used on aircraft model av-8. aluminum alloy per qq-a-250/11; 6.710 in.o/a lg; 1.118 in.nom o/a w; 3.250 in.nom o/a h;
01-282-3572
Structural Component Air Support
Consists of one doubler p/n 372335-4; one instruction plate p/n 361046-1; one access door assembly p/n 375992-1; one doubler p/n 375997-5; one web doubler p/n 375995-3; fourteen nuts p/n 22-1754-048; sixteen nuts p/n 22-1754-02bc; one web p/n 375995-9; twenty-eight washers p/n AN960-D416; fourteen bolts p/n 756021-1
01-282-3573
Structural Component Air Support
01-282-3575
Structural Aircraft Panel
01-282-3583
Aircraft Floor
Used on aircraft model av-8.
01-282-3694
Aircraft Former
2.550" overall length 1.650" overall width 0.071" material thickness opp -2012; ht tr T62, PS15534
01-282-3695
Longeron
7.200" overall length 1.000" overall width 0.071" material thickness nha 362535-1; heat treat T4
01-282-3838
Structural Component Air Support
01-282-4204
Aircraft Leading Edge
01-282-4219
Structural Aircraft Plate
Used on C-141. retainer, pin
01-282-4221
Structural Component Air Support
6.000" overall length 6.000" overall width 0.032" material thickness nha:3P61510; matl:cp titanium per ams 4901
01-282-4579
Wing Aircraft Fairing
Used on 1887613284101. material .032 sh 6061-0 al alloy per qq-a-250/11;
