01-247-0800
Structural Aircraft Panel
Used on oh-58 a/c (kiowa warrior).
01-247-0986
Structural Component Air Support
01-247-1830
Structural Aircraft Plate
Alum aly 6061-T6 per qq-a-250/11 cond-T6; o/a 0.025 by 0.82 by 3.12 in.; 3 holes placed irregularly, 0.195 min
01-247-1831
Structural Component Air Support
Used on acft model a-10a. c/o support aluminum alloy clad sh per qq-a-250/5 2024-T3, 5.000 in. lg, 4.600 in. w, 0.063 in. thk, and attaching hardware
01-247-1832
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sheet per qq-a-250/13 7075-0, 13.800 in. lg, 2.000 in. w, 0.063 in. thk
01-247-1834
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 11.800 in. lg, 2.000 in. lg, 0.063 in. thk
01-247-1835
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 7.600 in. lg, 1.800 in. w, 0.050 in. thk
01-247-1836
Structural Component Air Bracket
Nha L5342999; same as -001
01-247-1854
Aircraft Former
14.100" overall length 8.200" overall width 0.063" material thickness
01-247-1855
Aircraft Former
9.200" overall length
01-247-1856
Aircraft Former
18.400" overall length
01-247-1857
Aircraft Former
22.400" overall length 1.600" overall width 0.063" material thickness
01-247-1858
Aircraft Former
12.900" overall length 1.300" overall width 0.050" material thickness
01-247-1859
Aircraft Former
14.100" overall length 8.200" overall width 0.063" material thickness
01-247-1860
Aircraft Former
43.000" overall length
01-247-1861
Aircraft Former
27.100" overall length 15.700" overall width 0.040" material thickness
01-247-1865
Wing Rib
9.750" overall length 7.203" overall width 0.032" material thickness
01-247-1883
Thermal Special Purpo Insulation
C/o facesheet 2; batt 1; id plate; grommet 6; located on apu compt YN216.5 to YN265.25; end item identification:aircraft, model b-1b; functional description:used on nac insulation blanket assembly
01-247-1884
Thermal Special Purpo Insulation
C/o facesheet 2; batt 1; plate 1; grommet 8; located on apu compt YN216.5 to YN265.25; end item identification:aircraft, model b-1b; functional description:used on nac insulation blanket assembly
01-247-1885
Thermal Special Purpo Insulation
C/o facesheet 2; batt 1; plate 1; grommet 18; located at apu compt YN216.5 to YN265.25; end item identification:aircraft, model b-1b; functional description:used on nac insulation blanket assembly
01-247-1886
Thermal Special Purpo Insulation
C/o facesheet 2; batt 1; plate 1; grommet 22; located on apu compt YN216.5 to YN265.25; end item identification:aircraft, model b-1b; functional description:used on nac insulation blanket assembly
01-247-1887
Thermal Special Purpo Insulation
Ac/o facesheet 2; batt 1; id plate 1; grommet 20; located on apu compt YN216.5 to yn 265.25; end item identification:aircraft, model b-1b; functional description:used on nac insulation blanket assembly
01-247-2175
Structural Aircraft Plate
Aluminum alloy 2024-0 qq-a-250-5, matl 0.125 in. thk by 11.000 in. w by 15.500 in. lg
01-247-3555
Structural Component Air Support
Aluminum alloy 2024-0 qq-a-250/5, matl 0.190 in. thk by 2.125 in. w by 7.750 in. lg
01-247-4194
Structural Component Air Fitting
01-247-4221
Structural Aircraft Plate
14.000" overall length 9.000" overall width 0.063" material thickness
01-247-4222
Structural Aircraft Plate
Used on F-15. doubler
01-247-4223
Structural Aircraft Plate
Used on F-15.
01-247-4224
Structural Aircraft Plate
Used on F-15. doubler
01-247-4225
Structural Aircraft Plate
Used on F-15. doubler
01-247-4226
Structural Aircraft Plate
Used on F-15.
01-247-4227
Structural Aircraft Plate
Used on F-15.
01-247-4228
Structural Aircraft Plate
Used on F-15.
01-247-4229
Structural Aircraft Plate
Used on F-15. 5.150" overall length 2.890" overall width 0.063" material thickness splice
01-247-4230
Structural Component Air Support
01-247-4233
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 4.500 in. lg, 2.500 in. w, 0.063 in. thk
01-247-4234
Structural Component Air Support
Used on acft model a-10a. aluminum alloy sh per qq-a-250/13 7075-0, 13.500 in. lg, 5.500 in. w, 0.050 in. thk
01-247-4235
Structural Component Air Support
Used on acft model a-10a. aluminum alloy sh per qq-a-250/13 7075-0, 13.500 in. lg, 6.000 in. w, 0.050 in. thk
01-247-4236
Structural Component Air Support
Used on acft model a-10a. aluminum alloy sh per qq-a-250/13 7075-0, 25.500 in. lg, 4.200 in. w, 0.050 in. thk
01-247-4238
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 9.000 in. lg, 3.500 in. w, 0.050 in. thk
01-247-4239
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 8.500 in. lg, 1.400 in. w, 0.050 in. thk
01-247-4241
Structural Component Air Support
Used on acft model a-10a. aluminum alloy shp per qq-a-200/3 2024-T3511, 20.000 in. lg
01-247-4245
Structural Component Air Support
Used on acft model f-111.
01-247-4246
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 17.500 in. lg, 6.600 in. w, 0.050 in. thk
01-247-4248
Structural Component Air Support
Used on acft model a-10a. aluminum alloy shp per qq-a-200/11 7075-T6, 59.000 in. lg
01-247-4251
Structural Component Air Support
Used on acft model a-10a. material aluminum hfgd qq-a-367 7075-T411, 18.000 long
01-247-4262
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/5 2024-T3, 15.400 in. lg, 15.000 in. w, 0.032 in. thk
01-247-4264
Structural Component Air Support
Used on acft model a-10a. aluminum alloy shp per qq-a-200/11 7075-T6511, 12.600 in. lg
01-247-4265
Structural Component Air Support
Used on acft model a-10a. aluminum alloy shp per qq-a-200/11 7075-T6511, 13.000 in. lg
01-247-4267
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 4.500 in. lg, 4.500 in. w, 0.050 in. thk
