01-183-0128
Structural Aircraft Panel
01-183-0129
Structural Aircraft Panel
01-183-0139
Wing Landing Flap
C/o: doors, stringers, closeouts, intercostals, ribs, spars, trailing edge assys, skin, gussets, doublers, splices, clips, & hardware; opp -002
01-183-0140
Wing Landing Flap
C/o: doors, stringers, closeouts, intercostals, ribs, spars, trailing edge assys, skin, gussets, doublers, splices, clips, & hardware; opp -001
01-183-0141
Wing Landing Flap
C/o: spars, skin, trailing edges, doors, gussets, ribs, close-outs, doublers, intercostals, splices, & hardware; opposite -002
01-183-0142
Wing Landing Flap
C/o: spars, skin, trailing edges, doors, gussets, ribs, close-outs, doublers, intercostals, splices, & hardware; opposite -001
01-183-0143
Wing Landing Flap
Opp -002; c/o: stingers, ribs, spar, skin, t.e assy, doors, gussets, splices, doublers, intercostals, caps, & hardware
01-183-0144
Wing Landing Flap
Opposite -001; c/o: stringers, ribs, spar, skin, t.e assy, doors, gussets, splices, doublers, intercostals, caps, & hardware
01-183-0145
Wing Landing Flap
C/o 1 sub assy, 7 nutplate assy, 5 skin, 1 door, 1 cover, misc hardware; nha L1830000
01-183-0146
Wing Landing Flap
C/o 1 sub assy, 7 nutplate, 5 skin, 1 door, 1 cover, misc hardware; nha L1830000
01-183-0147
Aircraft Former
22.200" overall length 11.700" overall width 0.050" material thickness finish f-10.10
01-183-0148
Aircraft Former
7.700" overall length 1.100" overall width 0.050" material thickness
01-183-0149
Aircraft Former
2.300" overall length 1.300" overall width 0.050" material thickness
01-183-0150
Aircraft Former
1.500" overall length 0.800" overall width 0.050" material thickness
01-183-0159
Aircraft Former
Used on c-5 acft. temper T6
01-183-0163
Aircraft Former
4.500" overall length 4.200" overall width 0.040" material thickness
01-183-0165
Aircraft Former
01-183-0166
Aircraft Former
4.300" overall length 1.900" overall width 0.050" material thickness
01-183-0167
Aircraft Former
4.200" overall length 2.700" overall width 0.050" material thickness
01-183-0168
Aircraft Former
Used on acft model c/kc-135.
01-183-0169
Aircraft Former
59.000" overall length 3.000" overall width 0.016" material thickness
01-183-0184
Airfoil Rib
21.700" overall length 5.700" overall width 0.050" material thickness
01-183-0185
Airfoil Rib
21.700" overall length 5.700" overall width 0.050" material thickness
01-183-0186
Stiffener Aircraft Rib
27.000" overall length 22.000" overall width 0.040" material thickness
01-183-0187
Stiffener Aircraft Rib
3.700" overall length 7.700" overall width 0.050" material thickness
01-183-0188
Aircraft Skin
Used on acft model c/kc-135. aluminum alloy clad sheet per qq-a-250/5 2024-0, 13.000 in. lg, 10.000 in. w, 0.050 in. thk
01-183-0189
Aircraft Skin
Used on F-15.
01-183-0191
Aircraft Skin
Used on acft model c/kc-135. allminum alloy clad per qq-a-362 2024-0, 28.000 in. lg, 19.000 in. w, 0.032 in. thk
01-183-0192
Aircraft Skin
Used on acft model c/kc-135.
01-183-0193
Aircraft Skin
Used on acft model c/kc-135. commercially pure titanium per mil-t-9046 class 7 condition annealed, 22.000 in. lg, 19.000 in. w, 0.025 in. thk
01-183-0194
Aircraft Skin
Used on acft model c/kc-135. commercially pure titanium sheet per mil-t-9046 class 7 condition annealed, 148.000 in. lg, 140.000 in. w, 0.025 in thk
01-183-0195
Aircraft Skin
Used on acft model c/kc-135. al alloy clad sheet 2024-0 per qq-a-362, 0 temper; 95.0 in. long, 42.7 in. wide, 0.050 in. thick; finish srf-2.130
01-183-0196
Aircraft Skin
Used on acft model c/kc-135. al alloy clad sheet 2024-0 per qq-a-362, 0 temper; 95.0 in. long, 21.8 in. wide, 0.050 in. thick; finish srf-2.130
01-183-1842
Access Aircraft Door
Used on c-5b acft
01-183-1946
Aircraft Slat
01-183-1947
Aircraft Slat
01-183-1948
Aircraft Slat
01-183-1949
Aircraft Slat
01-183-1950
Aircraft Slat
Nha L1702000; opposite -022
01-183-1951
Aircraft Slat
Nha L1702000; opposite -032
01-183-1952
Aircraft Slat
Nha L1702000; opposite -022
01-183-1953
Aircraft Tip
Oppsite -032; nha L1202001
01-183-1954
Aircraft Slat
01-183-1955
Aircraft Slat
01-183-1956
Aircraft Slat
Nha L1702000; opposite -021
01-183-1957
Aircraft Slat
Nha L1702000; opposite -031
01-183-1958
Aircraft Slat
Nha L1702000; opposite -021
01-183-1959
Aircraft Slat
01-183-1960
Aircraft Tip
Opposite -031; nha L1202001
01-183-1976
Fuselage Section
