00-014-6149
Structural Component Air Support
Used on aircraft model c5a.
00-014-6150
Access Aircraft Cover
Resilient member material is all metal
00-014-6162
Structural Component Air Bracket
5.160" overall length 3.290" overall width 0.920" material thickness
00-015-1394
Access Aircraft Door
Used on f-4 airplane. ppconsist of 1 door p/n 32-31220-43, 1 stiffener p/n 32-31220-39
00-015-1419
Access Aircraft Door
00-015-1422
Structural Component Air Support
Used on f-4 aircraft. support assy-frame
00-015-1423
Structural Component Air Support
Used on f-4 aircraft. support assy-frame
00-015-1460
Structural Component Air Support
Aluminum alloy qq-a-200/3 2024-T4
00-015-1461
Structural Component Air Support
Aluminum alloy qq-a-200/3 2024-T4
00-015-1462
Aircraft Skin
18.400" overall length 18.000" overall width
00-015-1463
Aircraft Skin
18.000" overall length 18.000" overall width
00-015-1466
Aircraft Fairing
Used on aircraft model sh-3.
00-015-2105
Structural Aircraft Plate
00-015-2145
Structural Aircraft Plate
00-015-2146
Structural Aircraft Plate
Used on kc-135 tanker airplane. 0.065" material thickness
00-015-2152
Structural Component Air Support
Used on acft model kc-135. aluminum alloy qq-a-601
00-015-2153
Aircraft Former
00-015-2237
Access Aircraft Cover
Used on f-86 aircraft. cover, fuel tank; 5.688 in lg, 0.193in dia hole 3 places, 0.040 in thk
00-015-2438
Structural Aircraft Panel
20.000" overall length 8.000" overall width
00-015-2451
Aircraft Fairing
0.375" material thickness core data 3.1-3/16-1 on 5052H39 per mil-c-7438
00-015-2452
Aircraft Fairing
0.375" material thickness core data 3.1-3/16-1 on 5052H39 per mil-c-7438
00-015-2453
Aircraft Fairing
0.375" material thickness core data 3.1-1/16-1 on 5052H39 per mil-c-7438
00-015-2454
Aircraft Fairing
0.375" material thickness core data 3.1-3/16-1 on 5052H39 per mil-c-7438
00-015-2462
Structural Aircraft Panel
00-015-2463
Structural Aircraft Panel
00-015-2467
Structural Aircraft Panel
46.600" overall length 14.260" overall width with aluminum honeycomb core per mil-c-7438
00-015-2469
Structural Aircraft Panel
00-015-2470
Structural Aircraft Panel
00-015-2471
Aircraft Trailing Edge
Dfabricate per lac 1451 using impregnated epoxy glass cloth per mil-r-9300, type 1 resin, mil-f-9084, type 8 fabric finish per mil-f-9118, cross laminate plies, finish per lac g-629 type 1 external only
00-015-4751
Structural Component Air Support
Used on acft model c141a. al alloy 7075-T6 per qq-a-282, 1.500 in.thk, 2.500 in.w, 4.000 in.lg, left hand, used on upper roller number 6 spoiler drive
00-015-4759
Structural Aircraft Panel
00-015-4779
Structural Aircraft Panel
Used on C-141.
00-015-4787
Access Aircraft Cover
00-015-4788
Access Aircraft Cover
00-015-4789
Access Aircraft Cover
00-015-4800
Structural Aircraft Panel
00-015-8434
Structural Aircraft Plate
00-015-8435
Aircraft Leading Edge
00-015-8500
Structural Component Air Support
Used on acft model kc-135. steel, 17-4ph cres, ams 5355
00-015-8501
Structural Aircraft Plate
00-015-8502
Aircraft Strut
00-015-8503
Aircraft Strut
00-015-8504
Aircraft Strut
00-015-8505
Exhaust Pipe
Used on KC-135.
00-015-8530
Structural Component Air Support
00-015-8531
Structural Component Air Support
Used on aircraft model kc135. magnesium alloy, qq-m-56
00-015-9023
Structural Aircraft Panel
With fabric, 4 plys
00-015-9024
Structural Aircraft Panel
With fabric
00-015-9045
Aircraft Fairing
Alum alloy/honeycomb core
00-015-9049
Aircraft Fairing
Alum alloy/honeycomb core
