00-973-3345
Access Aircraft Door
00-973-3346
Access Aircraft Door
00-973-7437
Movable Canopy
00-974-1188
Aircraft Fairing
Matl: magnesium alloy, AZ31b, H24, 38.090 in lg to cut out; 20.760 in wd o/a; 0.125 in thk, 2 steel plates, type M6, 0.014in thk
00-974-5271
Access Aircraft Door
00-974-6460
Bell Crank
0.886" bore diameter
00-974-8830
Aircraft Door
00-974-8831
Aircraft Door
00-974-8834
Aircraft Skin
107.000" overall length 7.600" overall width
00-974-8836
Aircraft Wing Assembly
00-974-8837
Aircraft Wing Assembly
00-974-8838
Aircraft Beam
00-975-1555
Access Aircraft Door
Used on p-3e acft.
00-975-4282
Aircraft Fairing
00-975-4578
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, qq-a-250/4, 1.530 in. lg, 0.840 in. w, 2 holes 0.195 in. dia, 1 hole 0.080 in. dia
00-975-4584
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, qq-a-250/4, 1.530 in. lg, 0.840 in. w, 2 holes 0.195 in. dia, 1 hole 0.080 in. dia
00-975-4602
Structural Aircraft Plate
0.100" material thickness u/a:plate, guide, track no.3; matl: alum bronze, 0.811in wd 1 end, 1.740in wd opposite end, 4 holes drilled thru on 31.069in radius 0.191in min, 0.196 max dia equally spaced 0.380 in. from side
00-975-4603
Structural Aircraft Plate
0.100" material thickness u/a:plate, guide, track no.3; matl: alum bronze, 0.811in wd 1 end, 1.740in wd opposite end, 4 holes drilled thru max dia equally spaced 0.380 in. from side
00-975-4781
Structural Aircraft Plate
4.600" overall length 2.840" overall width
00-975-5506
Structural Component Air Bracket
00-975-5560
Structural Component Air Bracket
2.740" overall length 0.068" overall width 0.040" material thickness
00-975-5614
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, qq-a-250/4, 3.000 in. lg, 2.730 in. w, 2.180 in. h
00-975-5692
Structural Component Air Support
Matl:alum alloy ams 4260, 356-T6; c/o:support (-7) , 3.070 in lg, 2.880in dia of bearing outer area, 2.000in lg of mounting area, 1.600in. wd of mntg area, 3 mounting holes
00-975-6075
Aircraft Door
Used on C-141.
00-975-6076
Aircraft Door
Used on C-141.
00-975-6460
Aircraft Door
00-975-6461
Aircraft Door
00-975-6463
Aircraft Door
00-975-6464
Aircraft Door
00-975-6465
Access Aircraft Door
00-975-6467
Structural Component Air Bracket
3.000" overall length 1.900" overall width 0.760" material thickness 4 mntg holes 0.193 in dia, 2 mntg holes 0.190 in dia
00-976-0474
Structural Aircraft Panel
Used on b-52 aircraft. material honeycomb core, hexcel type np 3/16-112-7.0 per mil-c-8073, class 1, type 1b
00-976-0475
Structural Aircraft Panel
Used on kc-135 aircraft. honeycomb core, hexcel type np 3/16-112-7.0 per mil-c-8073, class 1, type 1b
00-976-0476
Structural Aircraft Panel
Used on b-52 aircraft. material honeycomb core, hexcel type np 3/16-112-7.0 per mil-c-8073, class 1, type 1b
00-976-0477
Structural Aircraft Panel
Used on b-52 aircraft. material honeycomb core, hexcel type np 3/16-112-7.0 per mil-c-8073, class 1, type 1b
00-976-0478
Structural Aircraft Panel
Used on b-52 aircraft. material honeycomb core, hexcel type np 3/16-112-7.0 per mil-c-8073, class 1, type 1b
00-976-0479
Structural Aircraft Panel
Used on b-52 aircraft. material honeycomb core, hexcel type np 3/16-112-7.0 per mil-c-8073, class 1, type 1b
00-976-1899
Structural Component Air Support
Used on acft model f101. located at fs 281.0
00-976-1960
Access Aircraft Door
Used on aircraft model c-135a/b.
00-976-1961
Access Aircraft Door
Used on aircraft model c-135a/b.
00-976-1962
Access Aircraft Door
Used on aircraft model c-135a/b.
00-976-1963
Access Aircraft Door
Used on aircraft model c-135a/b.
00-976-1970
Structural Aircraft Panel
00-976-2014
Structural Component Air Bracket
00-976-2015
Structural Component Air Bracket
00-976-2020
Structural Component Air Support
Used on acft model c-135k. cres, AMS5643
