01-133-1841
Structural Component Air Support
Used on f-4a/b aircraft. seal installation-wing fuselage int-inboard leading edge flap, matl-2024-o qq-a-250/5 cond o
01-133-1847
Airfoil Rib
8.100" overall length 5.700" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1848
Airfoil Rib
8.100" overall length 5.700" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1849
Airfoil Rib
8.100" overall length 5.600" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1850
Airfoil Rib
8.100" overall length 5.600" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1851
Airfoil Rib
7.900" overall length 5.500" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1852
Airfoil Rib
7.900" overall length 5.500" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1853
Airfoil Rib
7.800" overall length 5.400" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1854
Airfoil Rib
7.800" overall length 5.400" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1855
Airfoil Rib
7.800" overall length 5.400" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-1856
Airfoil Rib
7.400" overall length 5.100" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2307
Access Aircraft Door
01-133-2450
Airfoil Rib
7.900" overall length 5.600" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2451
Airfoil Rib
7.400" overall length 5.600" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2452
Airfoil Rib
7.500" overall length 5.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2453
Airfoil Rib
7.500" overall length 5.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2454
Airfoil Rib
8.200" overall length 5.900" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2455
Airfoil Rib
8.200" overall length 5.900" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2456
Airfoil Rib
8.100" overall length 5.800" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2457
Airfoil Rib
8.100" overall length 5.800" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2458
Airfoil Rib
7.900" overall length 5.800" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2459
Airfoil Rib
7.900" overall length 5.800" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2460
Airfoil Rib
7.700" overall length 5.500" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2461
Airfoil Rib
7.700" overall length 5.500" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2462
Airfoil Rib
8.100" overall length 5.700" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2463
Airfoil Rib
8.100" overall length 5.700" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2464
Airfoil Rib
8.100" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-2696
Structural Component Air Support
Used on uh-60a helicopter.
01-133-6012
Structural Aircraft Panel
C/o doubler, inner skin, outer skin
01-133-6023
Airfoil Rib
7.400" overall length 5.100" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-6024
Airfoil Rib
7.800" overall length 6.000" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-6026
Airfoil Rib
7.800" overall length 4.600" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-6027
Airfoil Rib
7.800" overall length 4.600" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-6028
Airfoil Rib
8.000" overall length 6.400" overall width 0.040" material thickness heat treat to cond T42; age to cond T62
01-133-6030
Aircraft Skin
Used on F-16.
01-133-6032
Aircraft Skin
Used on C-141. 145.000" overall length 60.000" overall width T761 clad both sides
01-133-6907
Access Aircraft Door
Used on f-14 acft.
01-133-8068
Structural Aircraft Plate
Used on f/a-18a aircraft. 10.250" overall length 0.008" material thickness
01-133-9388
Structural Aircraft Plate
01-133-9389
Structural Aircraft Plate
Used on uh-60a helicopter. aluminum alloy per qq-a-250-5
01-133-9390
Structural Aircraft Plate
01-133-9391
Structural Aircraft Plate
01-133-9392
Structural Aircraft Plate
01-133-9393
Structural Aircraft Plate
01-133-9394
Structural Aircraft Plate
01-133-9395
Structural Aircraft Plate
01-133-9396
Structural Aircraft Plate
01-133-9901
Structural Component Air Fitting
Function: attachment to aircraft conformal fuel tank; project fox
01-133-9902
Structural Component Air Fitting
Funct: attachment to acft conformal fuel tanks; project peace fox
01-133-9906
Structural Component Air Fitting
Funct: attachment to acft confromal fuel tanks; project peace fox
