00-837-2609
Thermal Special Purpo Insulation
00-837-2610
Thermal Special Purpo Insulation
00-837-3870
Access Aircraft Door
00-837-4841
Structural Component Air Support
Used on acft model c135. al alloy 7075-T6 per qq-a-367, comp 10; 7.340 in. lg, 6.955 in. w, 1.400 in. thk; vertical flap track support, wing station 615.00
00-837-4918
Access Aircraft Door
00-837-4921
Access Aircraft Door
00-837-4922
Access Aircraft Door
00-837-4924
Access Aircraft Door
00-837-9126
Fuel Aircraft Tank
00-838-2603
Wiring Harness
00-838-7992
Aircraft Fairing
19.210" overall length
00-839-3459
Access Aircraft Door
00-839-3483
Aircraft Fairing
8.960" overall width 0.040" material thickness
00-839-3491
Aircraft Former
0.050" material thickness
00-839-3492
Aircraft Former
0.050" material thickness
00-839-3493
Structural Aircraft Plate
Steel, A286, ams 5525, 5.900 in. l, 2.550 in. w, 0.050 in. thk
00-839-3494
Former
Titanium alloy, mil-t-9046 ty 1, comp a, annealed, 0.032 in.matl thk;
00-839-3500
Aircraft Former
0.032" material thickness
00-839-3501
Aircraft Former
0.032" material thickness
00-839-3503
Aircraft Former
0.032" material thickness
00-839-3504
Aircraft Former
0.036" material thickness
00-839-3510
Aircraft Former
0.036" material thickness
00-839-3512
Aircraft Former
0.025" material thickness
00-839-3516
Aircraft Former
0.025" material thickness
00-839-3517
Aircraft Skin
Matl 4138 cond n
00-839-3519
Structural Aircraft Plate
5.600 in. lg, 3.750 in. w, 0.032 in. thk, 19 holes
00-839-3521
Structural Aircraft Plate
Steel, A286, ams 5525, 5.600 in. l, 4.000 in. w, 0.036 in. thk
00-839-3522
Structural Aircraft Plate
Steel, A286, ams 5525, 5.600 in. l, 3.750 in. w, 0.032 in. thk
00-839-3523
Aircraft Former
0.032" material thickness
00-839-3526
Former
Titanium alloy, mil-t-9046 ty 1, comp a, annealed, 0.040 in.matl thk;
00-839-3541
Aircraft Former
00-839-3542
Aircraft Former
00-839-3907
Structural Component Air Support
00-839-4564
Structural Component Air Support
Used on acft model c5. al clad 2024-0 per qq-a-250/5, heat rreatment-T62; c/o support channel 1 ea p/n 4F24200-103a, mounting plate 1 ea p/n 4F24200-105a; used on main landing gear inner door gear box
00-839-4570
Structural Component Air Support
Used on acft model c5. al clad 2024-0 per qq-a-250/5, heat treatment-T62; c/o support channel 1 ea p/n 4F24200-104a, mounting plate 1 ea p/n 4724200-106a; used on main landing gear inner door gear box
00-839-4574
Aircraft Floor
Used on aircrafr model c-5a.
00-839-4585
Aircraft Floor
Used on aircraft model c-5a.
00-839-4588
Aircraft Windshield Panel
Used on aircraft,c-5a. flight safety critical
00-839-6663
Access Aircraft Door
00-839-6665
Aircraft Leading Edge
00-839-6736
Structural Component Air Fitting
11.500" overall length 1.500" overall width 0.750 " material thickness
00-839-6738
Structural Component Air Fitting
11.400" overall length 1.500" overall width 0.750 " material thickness
00-839-6744
Access Aircraft Door
Chromate zinc surface treated
00-839-9777
Movable Canopy
00-840-0040
Structural Component Air Support
Used on acft model f111. steel, 4.510 in.lg, 5 holes 0.191 in.min, 0.196 in.max dia;
00-840-0874
Aircraft Pylon
00-840-0879
Aircraft Pylon
00-840-0880
Aircraft Skin
134.000" overall length 29.500" overall width
00-840-1511
Access Aircraft Door
