00-137-0213
Wing Landing Flap
00-137-0214
Wing Landing Flap
00-137-1371
Structural Aircraft Plate
Used on f-4 phantom airplane. 7.220" overall length 6.000" overall width 0.032" material thickness condition; 1/2 hard
00-137-1379
Structural Component Air Support
00-137-1380
Structural Component Air Support
00-137-1382
Structural Component Air Support
00-137-1397
Structural Component Air Support
00-137-1415
Aircraft Skin
00-137-1457
Access Aircraft Door
Anodize surface treated
00-137-2372
Aircraft Floor
00-137-2373
Aircraft Floor
00-137-2374
Aircraft Floor
00-137-2377
Aircraft Floor
00-137-3774
Aircraft Spar
00-137-3775
Aircraft Spar
00-137-3776
Aircraft Spar
00-137-3777
Aircraft Spar
00-137-3778
Aircraft Spar
00-137-3785
Aircraft Spar
00-137-3787
Aircraft Spar
00-137-3788
Aircraft Spar
00-137-3789
Aircraft Spar
00-137-3790
Aircraft Spar
00-137-3791
Aircraft Spar
00-137-3793
Aircraft Spar
00-137-3795
Aircraft Spar
00-137-3796
Aircraft Spar
00-137-3990
Structural Component Air Support
00-137-3991
Structural Component Air Support
00-137-3992
Structural Component Air Support
00-137-3993
Structural Component Air Support
00-137-3994
Structural Component Air Support
00-137-3995
Structural Component Air Support
00-137-3996
Structural Component Air Support
00-137-3997
Structural Component Air Support
00-137-3998
Structural Component Air Support
00-137-3999
Structural Component Air Support
00-137-4000
Structural Component Air Support
00-137-4001
Structural Component Air Support
00-137-4002
Structural Component Air Support
00-137-4003
Structural Component Air Bracket
00-137-4004
Structural Component Air Support
Used on acft model f-111. 7c/o ar rivets p/n C089-6, ar rivets p/n C086-6, beam p/n 12B2968-9, stiffener p/n 12B2968-7; beam matl aluminum alloy qq-a-250/5-T62, 32.0 in. lg, 6.0 in. w, 0.071 in. thk; stiffener matl aluminum alloy qq-a-250/-5-T62, 22.0in. lg, 2.0 in. w, 0.100 in. thk
00-137-4006
Structural Aircraft Panel
00-137-4007
Structural Aircraft Panel
