01-536-3492
Structural Component Air Support
Beam assembly used on beam-bow, fus sta 497, 537, 557, lower, assy of
01-536-3493
Structural Component Air Support
Beam assembly used on beam-bow, fus sta 497, 537, 557, lower, assy of
01-536-3494
Structural Component Air Support
Beam assembly used on beam-bow, fus sta 497, 537, 557, lower, assy of
01-536-3495
Structural Component Air Support
Beam assembly used on beam-bow, fus sta 497, 537, 557, lower, assy of
01-536-3528
Airfoil Rib
Rib
01-536-3612
Aircraft Channel
Dimensions 0.064 x 4.30 x 19.60
01-536-3620
Aircraft Channel
Dimensions 0.064 x 4.30 x 19.52
01-536-3646
Structural Component Air Support
Clip clip - brace instl -mlg wheel well panel
01-536-3648
Structural Component Air Support
Clip clip - brace instl -mlg wheel well panel
01-536-3667
Structural Aircraft Plate
16.860" overall length 5.530" overall width 1.000" material thickness splice
01-536-3669
Structural Aircraft Plate
13.000" overall length 6.000" overall width 0.125" material thickness doubler
01-536-3670
Structural Aircraft Plate
16.000" overall length 1.000" overall width 0.125" material thickness filler
01-536-3671
Structural Aircraft Plate
16.000" overall length 1.000" overall width 0.125" material thickness filler
01-536-3672
Structural Aircraft Plate
3.000" overall length 1.000" overall width 0.090" material thickness filler
01-536-3972
Structural Aircraft Panel
Panel assembly for identification volume 51, figure 4
01-536-3973
Structural Aircraft Panel
For identification volume 51, figure four
01-536-4039
Access Aircraft Door
Used on f/a-22 raptor.
01-536-4040
Access Aircraft Door
Used on f/a-22 raptor.
01-536-4119
Structural Component Aircraf Web
Used on C-135. 16.300" overall length 4.960" overall width 0.025" material thickness web finish 2.115; dimensions are stocksize; clad sht; heat treat 0
01-536-4122
Structural Component Air Support
Used on C-135. 16.400" overall length chord-lower heat treat T6; extrusion, bac 1506-1053; dimension are stocksize; finish 2.30
01-536-4129
Structural Component Air Support
Used on C-135. 16.400" overall length chord-upper heat treat T6; extrusion BAC1506-1053; dim. are stocksize; finish 2.30
01-536-4159
Structural Component Aircraf Web
Used on C-135. 27.000" overall length 7.500" overall width 0.040" material thickness web used on -1
01-536-4176
Structural Component Air Support
Used on C-135. 39.000" overall length 1.800" overall width 0.064" material thickness rib chord heat treat 0; finish f-2.30; dimensions are stocksize
01-536-4397
Structural Component Air Fitting
Used on f/a-22 raptor. fitting f-22 emd
01-536-4555
Aircraft Latch Assembly
Used on mh60s knighthawk. latch assembly, rh
01-536-4623
Structural Component Air Fitting
Used on B-52. fitting assembly, left wing opposite 35-9230-502
01-536-4644
Access Aircraft Cover
Used on av-8b aircraft. navy-cover-access, aircraft two way interchange with 75A320967-2015
01-536-5593
Aircraft Ramp Assembly
01-536-5677
Access Aircraft Door
Used on f/a-22 raptor. access-shank-arresting gear
01-536-5777
Aircraft Skin
Fairing
01-536-5879
Structural Component Aircraf Web
Used on C-135. 14.000" overall length 4.800" overall width 0.025" material thickness web clad sheet; heat treat 0; finish f-2.115; dimesnsions are stocksize
01-536-5884
Structural Component Aircraf Web
Used on C-135. 22.000" overall length 7.000" overall width 0.025" material thickness web clad sheet; heat treat 0; dimensions are stocksize; finish f-2.115
01-536-5885
Structural Component Air Support
8.500" overall length 2.100" overall width 0.050" material thickness angle stiffener-closure rib, elev. trailing edge heat treat T3
01-536-5889
Structural Component Aircraf Web
Used on C-135. 20.950" overall length 5.980" overall width 0.032" material thickness web used on -3001
01-536-6119
Structural Component Air Support
01-536-6169
Aircraft Skin
9.300" overall length 5.000" overall width door installation-access elev, sta 70.38-75.38 heat treat T3
01-536-6184
Structural Aircraft Plate
9.300" overall length 5.000" overall width 0.032" material thickness doubler heat treat T6
01-536-6205
Structural Component Air Support
264.000" overall length 3.000" overall width door installation-access elev, sta 70.38-75.38 heat treat T6; opp -8
01-536-6211
Structural Aircraft Plate
9.500" overall length 5.000" overall width 0.016" material thickness doubler heat treat T6
01-536-6295
Structural Component Air Support
3.000" overall length 2.000" overall width 0.250" material thickness filler nha 16W030; heat treat T851; opposite -23
01-536-6396
Structural Component Air Support
Used on combat aircraft f-18 hornet. 3.00 bar; material 6al-4v ti anl technical document A1-F18ac-srm-210
01-536-6402
Structural Component Air Support
01-536-6411
Structural Component Air Fitting
3.600" overall width mates with the following p/n, 75A732254, 75A32253, 75A732216, 75A732263, bearing, .6250" ref. dia.
01-536-6412
Structural Component Air Fitting
3.600" overall width mates with the following p/n, 75A732254, 75A32253, 75A732216, 75A732263, bearing, 1.1875 min., 1.1880 max., ref dia., csk 90 deg bye 1.308 dia. near
01-536-6478
Access Aircraft Door
Used on f/a-22 raptor. f/a-22 emd
01-536-6479
Access Aircraft Door
Used on f/a-22 raptor. f/a-22 emd
01-536-6555
Structural Component Air Fitting
Track-door mechanism, main entry
01-536-6607
Structural Component Air Bracket
Bracket
01-536-6618
Airfoil Rib
Rib installation interspar elevator sta 115.18
01-536-6876
Structural Component Air Bracket
Used on f-22a raptor. 7.000" overall length 5.000" overall width 0.071" material thickness bracket, assy dim. are stock material; c/o: -279 bracket, LK204F3 nut,
