01-221-8502
Aircraft Former
15.000" overall length 9.000" overall width 2.500" material thickness used edp corrected dcn p/l
01-221-8503
Aircraft Former
20.050" overall length 5.760" overall width 0.056" material thickness
01-221-8504
Aircraft Former
8.100" overall length 7.000" overall width 0.050" material thickness
01-221-8505
Aircraft Former
16.300" overall length 5.700" overall width 0.050" material thickness
01-221-8506
Aircraft Former
16.300" overall length 5.700" overall width 0.050" material thickness
01-221-8507
Aircraft Former
15.500" overall length 5.250" overall width 0.050" material thickness
01-221-8508
Aircraft Former
15.900" overall length 5.250" overall width 0.050" material thickness
01-221-8509
Aircraft Former
01-221-8510
Aircraft Former
16.600" overall length 10.800" overall width 1.350" material thickness
01-221-8511
Aircraft Former
12.600" overall length 11.800" overall width 1.250" material thickness
01-221-8512
Aircraft Former
4.900" overall length 4.400" overall width 0.063" material thickness
01-221-8513
Aircraft Former
4.900" overall length 4.400" overall width 0.063" material thickness
01-221-8514
Aircraft Former
44.700" overall length 15.100" overall width 0.063" material thickness material per mms-1203 6al-6v-2sn
01-221-8515
Aircraft Former
14.120" overall length 6.610" overall width 0.063" material thickness
01-221-8516
Aircraft Former
Material per 1MT360A01-10037 x 43.250 in. lg
01-221-8517
Aircraft Former
Material per 1MT360A01-10037 x 43.250 in. lg
01-221-8518
Aircraft Former
39.000" overall length 9.000" overall width 0.050" material thickness
01-221-8519
Aircraft Former
26.200" overall length 8.700" overall width 0.045" material thickness
01-221-8520
Aircraft Former
8.750" overall length 8.100" overall width 0.045" material thickness
01-221-8521
Aircraft Former
25.600" overall length 7.850" overall width 0.045" material thickness
01-221-8526
Longeron
Used on F-15. stock 1MT10041B01 x 49.000 in. lg; p/o longeron-lower
01-221-8527
Longeron
Used on F-15. stock 1MT10041B01 x 49.000 in. lg; p/o longeron-lower
01-221-8530
Aircraft Skin
Used on F-15. 103.000" overall length 36.000" overall width per 6al-6v-2sn mms 1203
01-221-8531
Aircraft Skin
Used on F-15. 103.000" overall length 36.000" overall width per 6al-6v-2sn mms 1023
01-221-8533
Aircraft Stringer
35.000" overall length material per 1MA10298-801
01-221-8536
Aircraft Stringer
76.000" overall length 5.000" overall width 0.160" material thickness material per mms 1203 6al-6v-2sn
01-221-8537
Aircraft Stringer
76.000" overall length 5.000" overall width 0.160" material thickness material per mms 1203 6al-6v-2sn
01-221-8538
Aircraft Stringer
22.000" overall length 6.000" overall width 0.125" material thickness material per mms 1203 6al-6v-2sn
01-221-8539
Aircraft Stringer
22.000" overall length 6.000" overall width 0.125" material thickness material per mms 1203 6al-6v-2sn
01-221-8540
Aircraft Stringer
14.000" overall length material per 1MT360B01-10001
01-221-8541
Aircraft Stringer
14.000" overall length material per 1MT360B01-10001
01-221-8542
Aircraft Stringer
35.000" overall length material 1MA10299-B01
01-221-8543
Aircraft Stringer
35.000" overall length material 1MA10299-B01
01-221-8769
Structural Component Air Support
01-221-8834
Aircraft Pylon
C/o apron assy, hydraulic system, 2 drain system, cable pulley pylon support, panel assy, pylon structure assy, overheat
01-221-9278
Aircraft Wing Assembly
01-221-9307
Structural Component Air Support
Used on c-5b aircraft. fitting assembly-hinge, square slot door, mlg fairing, fs 1411.31 & 1495.01; c/o: -107a fitting (1) , bearing (1) ; opposite -106a
01-221-9308
Structural Component Air Support
Used on c-5b aircraft. fitting assembly-hinge, square slot door, mlg fairing, fs 1411.31 & 1495.01; c/o: -108a fitting (1) , bearing (1) ; opposite -105a
01-221-9309
Structural Component Air Support
C/o 1 preformed flange, 1 insert, 1 clinch ring; superseded 320-4-45511-101 ow per ECP031/eco 2; eff 5c 0001 9999; nha 320-4-45550-103
01-221-9331
Structural Aircraft Panel
Used on acft model e-3a. c/o preimpregnated glass fabric, 1 door cushion, 1 semi-rigid vinyl, 1 decorative laminate, 1 protective facing, 2 inserts; nha 204-40165
01-221-9332
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 face sheet; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9333
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 face sheet, 4 insert; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9334
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 face sheet, 4 insert; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9335
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 face sheet, 4 insert; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9337
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel assy, 1 face sheet; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9339
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel assy, 1 face sheet; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9340
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel assy, 1 face sheet; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9341
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 face sheet, 2 insert; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9343
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel assy, 1 face sheet; rubber stamp p/n on non-decorative side of panel per BAC5307
01-221-9344
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 face sheet, 4 insert; rubber stamp p/n on non-decorative side of panel per BAC5307
