01-207-3283
Aircraft Former
01-207-3284
Aircraft Former
01-207-3285
Aircraft Former
01-207-3286
Aircraft Former
01-207-3287
Aircraft Former
01-207-3288
Aircraft Former
01-207-3289
Aircraft Former
01-207-3290
Aircraft Former
01-207-3291
Aircraft Former
01-207-3294
Longeron
Used on F-15.
01-207-3295
Longeron
Used on F-15.
01-207-3296
Longeron
Used on F-15.
01-207-3297
Airfoil Rib
Used on C-130.
01-207-3298
Aircraft Skin
Used on C-130.
01-207-3503
Access Aircraft Cover
01-207-5156
Access Aircraft Door
Used on acft model f-16c/d usaf. nha 16P009-1; superseded p/n 16P178-803 ow per ECN1H032; effective on 5C0001-9999; aerial refuel slipway
01-207-5267
Structural Aircraft Panel
Used on c-5a acft. trim panel; p/o flight station lower; fuselage station 408.460 to 443.000
01-207-5268
Structural Aircraft Plate
Nha 4N12014
01-207-5303
Aircraft Former
55.000" overall length 26.000" overall width 1.750" material thickness lower bulkhead
01-207-5340
Structural Component Air Fitting
01-207-5348
Structural Component Air Fitting
01-207-5357
Aircraft Former
55.000" overall length 26.000" overall width 1.750" material thickness FMS3002-T851; finish A403; nha 16B610-5; effective on 5c 0005-0177, 0179, 0181, 183, 187, 189, 191, 193, 195, 201, 203, 205, 207, 209, 211, 213, 215, 219, 221, 223, 225, 227, 232; superseded p/n 16B6207-37 ow per ecn 0H610
01-207-5358
Structural Aircraft Plate
01-207-5359
Structural Aircraft Plate
01-207-5361
Structural Component Air Support
01-207-5364
Structural Component Air Support
Used on c-5a acft. attach-support mechanism inboard logistics rail
01-207-5365
Structural Component Air Support
Used on acft model kc-135. consist of 2 bushing, 1 support fitting; nha 65-6404
01-207-5366
Structural Component Air Support
Used on acft model kc-135.
01-207-5367
Structural Component Air Support
Used on acft model kc-135.
01-207-5369
Structural Component Air Support
Used on f-15 acft. p/o former side panel; fuselage station 702.900
01-207-5370
Structural Component Air Support
Used on f-15 acft. p/o former; fuselage station 565.330
01-207-5373
Structural Aircraft Panel
01-207-5374
Structural Aircraft Panel
01-207-5375
Structural Aircraft Panel
Used on c-5a acft. trim; fuselage station 1844 to 1884 lefthand side
01-207-5377
Structural Aircraft Panel
24.000" overall length 17.000" overall width
01-207-5379
Structural Aircraft Panel
23.000" overall length 17.000" overall width
01-207-5381
Structural Aircraft Panel
C/o panel p/n 12B43670-13, nut p/n C064-048-1, 2 ea. insert p/n MS21209F4-15, rivet, ar
01-207-5383
Aircraft Former
P/o fuselage section-aft side wall
01-207-5384
Aircraft Leading Edge
01-207-5385
Aircraft Leading Edge
01-207-5387
Aircraft Pylon
01-207-5388
Aircraft Pylon
01-207-5390
Aircraft Skin
Used on f-5 acft. intake duct, outboard fs 402.550 T0 451.950
01-207-5391
Aircraft Skin
74.000" overall length 25.000" overall width nha 16B602-3; effective on 5c 0001-9999; superseded p/n 16B6308-28 ow per ECN4G212; finish A701
01-207-5392
Aircraft Skin
74.000" overall length 25.000" overall width nha 16B602-3; effective on 5c 0001-91, 93, 117, 119, 121, 123, 125, 127, 129, 135, 137, 177, 179, 181, 183, 189, 191, 193, 195, 201, 203, 205, 207, 209, 211, 213, 215, 217, 219, 221, 223, 225, 227, 232; superseded p/n 16B6308-29 ow per ECN4G212; fin A701
01-207-5393
Fuselage Stringer
Used on 1520-00-859-2670. 29.000" overall length 2.600" overall width 0.063" material thickness bow design; angle cross section; w/o rivet holes
01-207-5394
Fuselage Stringer
Used on 1520-00-859-2670. 10.000" overall length 2.600" overall width 0.050" material thickness bow design; angle CR0ss section; w/o rivet holes
01-207-5395
Fuselage Stringer
Used on 1520-00-859-2670. 29.000" overall length 2.500" overall width 0.050" material thickness bow design; angle cross section; w/o rivet holes
01-207-5396
Structural Aircraft Panel
23.000" overall length 17.000" overall width
