01-160-9331
Aircraft Former
Opposite -2; nha 458-58066
01-160-9332
Aircraft Former
1.500" overall length make from BAC1506-403
01-160-9333
Aircraft Former
1.500" overall length make from BAC1506-403
01-160-9334
Aircraft Former
1.200" overall length make from BAC1506-1386
01-160-9335
Aircraft Former
1.200" overall length make from BAC1506-1386
01-160-9336
Aircraft Former
Used on acft model b52.
01-160-9340
Aircraft Skin
56.000" overall length 40.000" overall width finish A657; nha 16B4701-5, eff 5c 0001 9999; superseded p/n 16B4615-9 ow per ecn 2E879
01-160-9342
Horizontal Stabilizer
01-160-9343
Horizontal Stabilizer
01-160-9515
Access Aircraft Door
01-160-9548
Aircraft Fairing
Used on aircraft model f-18.
01-161-0449
Structural Aircraft Panel
01-161-0450
Structural Aircraft Panel
01-161-0460
Structural Aircraft Panel
01-161-0462
Structural Aircraft Panel
01-161-0463
Structural Aircraft Panel
01-161-0505
Structural Component Air Support
Used on c-141b acft. c/o tube.p/n 3F31162-103; fitting 2; collar, 2; miscellaneous hardware; 40.340 in. lg; tube dia. 1.633 in.; used on fuselage station 958 to 998
01-161-0516
Structural Aircraft Plate
11.200" overall length 8.200" overall width 0.080" material thickness
01-161-0517
Structural Aircraft Plate
Used on B-52. make from BAC1513-81 x 1.900 in.
01-161-0518
Structural Aircraft Plate
Used on B-52. make from BAC1513-81 x 1.900 in.
01-161-0519
Structural Aircraft Plate
Used on B-52. make from BAC1513-81
01-161-0520
Structural Aircraft Plate
Used on B-52. make from BAC1513-81
01-161-0521
Structural Aircraft Plate
3.600" overall length 1.900" overall width 0.050" material thickness
01-161-0522
Structural Aircraft Plate
3.600" overall length 1.900" overall width 0.050" material thickness
01-161-0523
Structural Aircraft Plate
6.500" overall length 3.800" overall width 0.050" material thickness
01-161-0524
Structural Aircraft Plate
Used on B-52.
01-161-0526
Structural Aircraft Plate
Used on acft model kc-135r. al alloy clad 2024-0 per qq-a-250/5; heat treated to cond T42; finish f-2.03; 3.000 in. lg, 2.000 in. w, 0.100 in. thk; nha 458-58067-4
01-161-0527
Structural Aircraft Plate
Used on acft model kc-135r. BAC1534-33 x 2.000 in. lg, 1.000 in. w; finish f-12.6582; located nacelle station 235.00; nha 458-58067-4
01-161-0528
Structural Aircraft Plate
Used on acft model kc-135r. al alloy clad 2024-T3 per qq-a-250/5; finish f-2.03; 3.000 in. lg, 0.750 in. w, 0.100 in. thk; located nacelle station 235.00; nha 458-58067-4
01-161-0533
Structural Aircraft Plate
10.000" overall length 4.400" overall width 0.080" material thickness
01-161-0538
Structural Aircraft Plate
Used on kc-135r tanker airplane. used opposite p/n 485-58304-3. nha p/n 458-58304-2
01-161-0539
Structural Aircraft Plate
C/o 2 seal retainer, 1 upper clip, 1 lwr clip, 2 seals, 1 end plate; opp -4; nha 458-58304-1
01-161-0541
Structural Aircraft Plate
11.200" overall length 8.200" overall width 0.080" material thickness
01-161-0543
Structural Aircraft Plate
13.200" overall length 7.800" overall width 0.080" material thickness
01-161-0548
Structural Aircraft Plate
2.990" overall length 1.820" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-0549
Structural Aircraft Plate
2.660" overall length 1.660" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-0550
Structural Aircraft Plate
2.990" overall length 1.820" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-0551
Structural Aircraft Plate
2.660" overall length 1.660" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-0552
Structural Aircraft Plate
2.990" overall length 1.820" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-0553
Structural Aircraft Plate
2.840" overall length 1.820" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-0554
Structural Aircraft Plate
2.840" overall length 1.690" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-0555
Structural Aircraft Plate
2.530" overall length 1.690" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-0556
Structural Aircraft Plate
Used on f-15 acft. function-spacer; location-wing inner torque box; matl-7075-T76 aluminum alloy per qq-a-250/24 cond T76; dim. 2.660 in. lg, 1.660 in. w, 0.250 in. thk; retrofit-spar beef-up
01-161-0557
Structural Component Air Support
Used on c-5 acft. c/o boot
01-161-0558
Structural Component Air Support
2.600" overall length 1.800" overall width 0.050" material thickness
01-161-0559
Structural Component Air Support
2.600" overall length 1.800" overall width 0.050" material thickness
01-161-0560
Structural Component Air Support
1.500" overall width make from BAC1512-3350
01-161-0561
Structural Component Air Support
1.500" overall width make from BAC1512-3350
01-161-0562
Structural Component Air Support
Used on acft model kc-135. 2024-T3511 extruded al per qq-a-200/3; finish f-2.03; AND10134-1407 x 4.900 in. lg; nha 458-58067-2
01-161-0563
Structural Component Air Support
Used on acft model kc-135r. al alloy extruded 2024-T3511 per qq-a-200/3; finish f-2.03; AND10134-1407 x 4.900 in. lg; located nacelle station 213.88; nha 458-58075-2
