01-360-1277
Aircraft Fairing
47.000" overall length 4.000" overall width 0.250" material thickness nuclear hardness critical item; nha DAA3150A640; used as fairing lower rudder blade seal
01-360-1280
Aircraft Fairing
10.000" overall length 8.000" overall width 0.190" material thickness nuclear hardness critical item; nha DAA3661B106; 6al-4v cond a; used as elevon fairing seal
01-360-1281
Aircraft Fairing
Nuclear hardness critical item, next assembly DAA3661B106
01-360-1282
Aircraft Fairing
Nuclear hardness critical item, next assembly DAA366AB106
01-360-1287
Structural Aircraft Panel
Nuclear hardness critical item & smoothness critical item; nha: DAA3114B103; fin: f-19.62
01-360-1288
Structural Aircraft Panel
01-360-1291
Aircraft Floor
01-360-1294
Structural Component Air Support
01-360-1295
Structural Component Air Support
01-360-1296
Structural Component Air Support
01-360-1310
Structural Component Air Fitting
01-360-1311
Structural Component Air Fitting
01-360-1313
Structural Component Air Fitting
01-360-1314
Structural Component Air Fitting
01-360-1315
Structural Component Air Fitting
4.750" overall length 1.062" overall width 0.375 " material thickness guide-lever; t.c.t.o.1a-10a-1215
01-360-1397
Aircraft Fairing
Used on pacer special. seal assy, aerodynamic - mid elevon; loci or locp must be evaluated for low observable impacts by the responsible engineering activity
01-360-1398
Aircraft Fairing
Used on pacer specail. seal assy, aerodynamic - mid elevon; loci or locp must be evaluated for low observable impacts by the responsible engineering activity
01-360-1399
Aircraft Fairing
Used on pacer special. seal assy, aerodynamic - mid elevon; loci or locp must be evaluated for low observable impacts by the responsible engineering activity
01-360-1794
Access Aircraft Door
Used on C-130.
01-360-1801
Structural Aircraft Plate
3.250" overall length
01-360-1802
Structural Aircraft Plate
3.000" overall length 2.000" overall width 0.090" material thickness
01-360-1803
Structural Aircraft Plate
4.000" overall length 2.500" overall width 0.500" material thickness u/o rudder thru bolt repair
01-360-1804
Structural Aircraft Plate
4.000" overall length 2.500" overall width 0.500" material thickness u/o rudder thru bolt repair
01-360-1805
Structural Aircraft Panel
01-360-1806
Structural Aircraft Panel
01-360-1807
Structural Component Air Support
Used on pacer special. nuclear hardness critical item
01-360-1808
Structural Component Air Bracket
01-360-1824
Aircraft Channel
Functional description:u/o formerfuselage FS402.17
01-360-2085
Structural Aircraft Plate
Cfracture critical category ii; c/O2 bungee assy, 2 bellcrank assy, 1 plate, 4 rivet, 2 pivot hook pin, 2 hook, 2 push rod assy, 12 washer, 8 pin, 4 bolt, 2 screw, 2 nutplate, 8 nut; nha daa 3510A140
01-360-2086
Fuel Aircraft Tank
Disassemblied external fuel tank with container
01-360-2574
Aircraft Fairing
Used on aircraft,hornet f/a-18.
01-360-2575
Aircraft Fairing
Used on aircraft,hornet f/a-18.
01-360-2576
Structural Component Air Support
Used on b-2 bomber (atb). 5.000" overall length 1.000" overall width
01-360-2577
Structural Component Air Fitting
01-360-3739
Structural Component Air Fitting
Used on aircraft model ch-46e.
01-360-3740
Structural Component Air Fitting
Used on aircraft model ch-46e.
01-360-3743
Structural Component Air Fitting
Used on aircraft model ch-46e.
01-360-4049
Aircraft Fairing
Used on pacer special. 45.000" overall length 2.200" overall width 0.063" material thickness smoothness critical item, opp-025material: 15-5 ph sheet per BMS7-240 type 1, solution tr, ht tr 150-170ksi per BAC5619
01-360-4051
Aircraft Fairing
Nuclear hardness critical item, next assembly DAA3661B106
01-360-4325
Access Aircraft Door
Used on t37c aircraft.
01-360-4390
Aircraft Floor
Used on aircraft,b-2. weight shall not exceed 15.900 lb
01-360-4393
Structural Component Air Support
Used on b-2 bomber (atb). 4.120" overall length 1.150" overall width glass fabric preimprenated high temperature resistant; stock 11 plies
01-360-4394
Structural Component Air Support
Used on b-2 bomber (atb). 5.830" overall length 2.870" overall width glass fabric preimpregnated high temperature resistant; stock 12 plies
01-360-4395
Structural Component Air Support
Used on b-2 bomber (atb). 6.400" overall length 4.270" overall width glass fabric preimpregnated high temperature resistant; stock 12 plies
01-360-4396
Structural Component Air Support
Used on b-2 bomber (atb). 4.630" overall length 1.150" overall width glass fabric preimpregnated high temperature resistant; stock 11 plies
01-360-4551
Thermal Special Purpo Insulation
Used on b-2 bomber. 13.300" overall length 7.000" overall width used on b-2 bomber
01-360-4552
Thermal Special Purpo Insulation
Used on b-2 bomber. 13.300" overall length 7.000" overall width used on b-2 bomber
01-360-4553
Thermal Special Purpo Insulation
Used on b-2 bomber. 16.000" overall length 13.300" overall width used on b-2 bomber
01-360-4554
Thermal Special Purpo Insulation
Used on b-2 bomber. 24.000" overall length 13.300" overall width used on b-2 bomber
01-360-4555
Thermal Special Purpo Insulation
Used on b-2 bomber. 13.300" overall length 7.500" overall width used on b-2 bomber
