01-253-1201
Structural Aircraft Plate
Used on F-15. 1MA160B04-10149 by 9.10 in.; opposite p/n -2046; used on -1001
01-253-1202
Structural Aircraft Plate
Used on F-15. 6.750" overall length 2.500" overall width 1.500" material thickness nha 68A110001
01-253-1203
Structural Aircraft Plate
7.450" overall length 4.150" overall width 0.032" material thickness opposite p/n -2026; make from -2O04
01-253-1204
Structural Aircraft Plate
Used on F-15.
01-253-1205
Structural Aircraft Plate
Used on F-15.
01-253-1207
Structural Aircraft Plate
Used on F-15.
01-253-1208
Structural Aircraft Plate
Used on F-15. 23.000" overall length 4.530" overall width 0.312" material thickness
01-253-1209
Structural Aircraft Plate
Used on F-15. cond 0, alclad
01-253-1210
Structural Aircraft Plate
Used on F-15. cond 0, alclad
01-253-1211
Structural Aircraft Plate
Used on F-15. cond 0, alclad
01-253-1212
Structural Aircraft Plate
Used on F-15. 24.400" overall length 7.500" overall width 0.050" material thickness opposite -2037; used on -1005
01-253-1213
Structural Aircraft Plate
Used on F-15. 18.000" overall length 0.625" overall width 0.063" material thickness
01-253-1214
Structural Aircraft Plate
Used on F-15. cond 0, alclad
01-253-1215
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 comp c annealed; bracket p/o tip 2.000 in. dia vertical stabilizer
01-253-1216
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-T851; tee u/o wing, trailing, forward
01-253-1217
Structural Component Air Support
01-253-1218
Structural Component Air Support
Used on acft model f-15. 7075-0 per qq-a-250/12 cond 0; 20.35 in. lg, 4.35 in. wd, 0.063 in. thk; used on -1002
01-253-1219
Structural Component Air Support
01-253-1220
Structural Component Air Support
Used on acft model f-15. 6al-4v per mil-t-9047; 3.20 in. lg, 2.75 in. wd, 1.00 in. thk; was -2001; nha 68A413400
01-253-1221
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-T851; tee u/o trailing edge, aft
01-253-1222
Structural Component Air Support
Used on f-15 acft.
01-253-1223
Structural Component Air Support
Used on f-15 acft. aluminum alloy 7075-T7351; fitting, splice-rib to rear spar; wing station 155.024
01-253-1224
Structural Component Air Support
Used on acft model f-15. 1MA122D05-10028 by 4.95 in; nha 68T050292; located on xw 63.866
01-253-1225
Structural Component Air Support
Used on acft model f-15. 2124-T851 per mms-149 cond T851; 6.15 in. lg, 4.40 in. wd, 2.25 in. thk; nha 68A113093
01-253-1226
Structural Component Air Support
Used on acft model f-15. 1MA122D05-10028 by 4.95 in; nha 68A1131148
01-253-1228
Structural Aircraft Panel
Liner, left hand side-forward crew station
01-253-1229
Structural Aircraft Panel
Thermoplastic sheet; liner, left hand side-forward crew station
01-253-1231
Aircraft Floor
Used on F-15. deck, pressure
01-253-1232
Aircraft Floor
Used on F-15. deck, pressure
01-253-1237
Airfoil Rib
10.620" overall length 9.760" overall width 0.071" material thickness opposite p/n -2027
01-253-1238
Airfoil Rib
10.000" overall length 8.080" overall width 0.071" material thickness used on -1001
01-253-1239
Airfoil Rib
23.200" overall length 8.950" overall width 0.050" material thickness opposite p/n -2032
01-253-1249
Airfoil Rib
68A113155-2001; nha 68A113156
01-253-1608
Access Aircraft Cover
01-253-2236
Fuel Aircraft Tank
01-253-2250
Aircraft Fairing
Nuclear hardness critical item; c/o 2 seal, 4 sub assy, 2 strip, 5 shoe, 1 panel, misc hardware; nha L3053601; opposite -002
01-253-2251
Aircraft Fairing
Nuclear hardness critical item; nha L3053601; c/o 2 seals, 4 subassy, 2 strips, 5 shoes, 1 panel, misc hardware; opposite pn -001
