01-246-8953
Structural Aircraft Plate
Used on C-130.
01-246-8955
Structural Aircraft Plate
Used on C-130.
01-246-8959
Structural Aircraft Plate
Used on F-15. 3.7500" overall length 2.600" overall width 0.100" material thickness opp -2002; nha 68A112221
01-246-8960
Structural Aircraft Plate
Used on F-15. 1MA160B04-10169 by 4.00 in.; nha 68A112267
01-246-8961
Structural Aircraft Plate
Used on F-15. 1MA160B04-10169 by 4.00 in.; nha 68A112267
01-246-8962
Structural Aircraft Plate
Used on F-15.
01-246-8963
Structural Aircraft Plate
Used on F-15.
01-246-8964
Structural Aircraft Plate
Used on F-15. 2.000" overall length 1.350" overall width 0.080" material thickness filler
01-246-8965
Aircraft Fairing
9.000" overall length 7.000" overall width 0.050" material thickness opposite p/n -1
01-246-8966
Aircraft Fairing
Nha 68A334004
01-246-8967
Aircraft Elevator
01-246-8975
Structural Component Air Support
01-246-8976
Structural Component Air Support
01-246-8977
Structural Component Air Support
01-246-8978
Structural Component Air Support
01-246-8979
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 4.200 in. lg, 3.200 in. w, 0.050 in. thk
01-246-8982
Structural Component Air Support
Used on acft model a-10a. aluminum hfgd qq-a-367 7075-T73, 18.500 in. lg, 8.000 in. w, 3.500 in. thk
01-246-8983
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per 7075-0 qq-a-250/13, 9.200 in. lg, 5.900 in. w, 0.063 in. thk
01-246-8988
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 13.000 in. lg, 5.200 in. w, 0.050 in. thk
01-246-8989
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 12.000 in. lg, 5.800 in w, 0.050 in. thk
01-246-8990
Structural Component Air Support
Used on acft model a-10a. aluminum forging per 7075-T73 qq-a-367
01-246-8993
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 15.400 in. lg, 3.000 in. w, 0.050 in. thk
01-246-8994
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 3.200 in. lg, 2.100 in. w, 0.050 in. thk
01-246-8996
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 7.000 in. lg, 3.400 in. w, 0.050 in. thk
01-246-8997
Structural Component Air Bracket
4.200" overall length 3.200" overall width 0.050" material thickness
01-246-9006
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 6.900 in. lg, 3.400 in. w, 0.080 in. thk
01-246-9010
Structural Component Air Support
Used on f-15 aircraft. size .040X4.63X11.58; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-9011
Structural Component Air Support
Used on f-15 aircraft. size .040X4.63X11.58; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-9012
Structural Component Air Support
Used on f-15 aircraft. size .040X3.84X13.89; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-9013
Structural Component Air Support
Used on f-15 aircraft. size .040X3.56X7.32; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-9016
Structural Component Air Support
Used on acft model f-15. 7075-T7351 per mms-159 cond T7351; 42.00 in. lg, 17.50 in. wd, 3.125 in. thk; located at fs 558.50 to fs 595.90
01-246-9017
Structural Component Air Support
Used on acft model f-15. 7075-T7351 per mms-159 cond T7351; 42.00 in. lg, 17.50 in. wd, 3.125 in. thk; located at fs 558.50 to fs 595.90
01-246-9024
Structural Aircraft Panel
Used on acft model b-1b. same as -011; nha L5351025
01-246-9025
Structural Aircraft Panel
43.000" overall length 30.000" overall width
01-246-9036
Aircraft Former
31.000" overall length 11.600" overall width 0.050" material thickness
01-246-9037
Aircraft Former
18.300" overall length 10.400" overall width 0.050" material thickness
01-246-9042
Aircraft Former
31.500" overall length 13.000" overall width 0.050" material thickness
01-246-9043
Aircraft Former
30.500" overall length 11.300" overall width 0.050" material thickness
01-246-9044
Aircraft Former
15.000" overall length 6.000" overall width 0.050" material thickness
01-246-9046
Aircraft Former
15.000" overall length 9.000" overall width 0.050" material thickness
01-246-9047
Aircraft Former
19.000" overall length 2.800" overall width 0.050" material thickness
01-246-9052
Aircraft Skin
01-246-9053
Aircraft Skin
01-246-9054
Aircraft Skin
01-246-9056
Aircraft Skin
30.000" overall length 25.000" overall width p/o skin INSTALLATI0n
01-246-9059
Aircraft Skin
21.500" overall length 17.000" overall width opposite p/n -2002; nha 68A335002
01-246-9060
Aircraft Skin
21.500" overall length 17.000" overall width opposite p/n -2001; nha 68A335002
01-246-9064
Thermal Special Purpo Insulation
Bc/o blanket 1; tab 4; pile tape 3; hook tape 3; safety cord 1; misc hardware; nha 520-10084; end item identification:aircraft, model b-52; functional description:used on bleed air duct insulation blanket
01-246-9772
Structural Component Air Support
01-247-0238
Aircraft Engine Build- Parts Kit
