01-216-0637
Airfoil Rib
Used on F-15.
01-216-0638
Airfoil Rib
Used on F-15.
01-216-0639
Airfoil Rib
Used on F-15.
01-216-0640
Airfoil Rib
Used on F-15.
01-216-0646
Aircraft Skin
Used on F-15. 36.000" overall length 8.500" overall width
01-216-0647
Aircraft Skin
Used on F-15. 13.000" overall length 7.500" overall width
01-216-0648
Aircraft Skin
Used on F-15. 36.000" overall length 8.500" overall width
01-216-0649
Aircraft Skin
Used on C-141.
01-216-0650
Aircraft Skin
Used on C-141.
01-216-0651
Aircraft Skin
01-216-0652
Aircraft Skin
Used on C-141.
01-216-0653
Aircraft Skin
01-216-0654
Aircraft Skin
Used on C-141.
01-216-0655
Aircraft Skin
Used on C-141.
01-216-0656
Aircraft Skin
Used on C-141.
01-216-0657
Aircraft Skin
Used on C-141.
01-216-0658
Aircraft Skin
Used on C-141.
01-216-0659
Aircraft Skin
Used on C-141.
01-216-0660
Aircraft Skin
01-216-0661
Aircraft Skin
Used on F-15.
01-216-0662
Aircraft Spar
01-216-0664
Aircraft Spar
01-216-2584
Structural Aircraft Panel
01-216-3125
Structural Aircraft Plate
01-216-3126
Wing Aircraft Fairing
01-216-3127
Wing Aircraft Fairing
01-216-3128
Structural Component Air Support
01-216-3129
Structural Component Air Support
01-216-3144
Aircraft Former
01-216-3145
Aircraft Former
Used on F-18. 13.000" overall length 0.900" overall width 0.012" material thickness one corner cut at a angle
01-216-3159
Airfoil Rib
Used on F-15.
01-216-3160
Aircraft Skin
01-216-4157
Aircraft Fairing
01-216-4158
Structural Component Air Support
01-216-4563
Thermal Special Purpo Insulation
01-216-4657
Access Aircraft Door
Used on acft model f-4. wc/o 5 clip, 2 shim, 1 inner skin, 3 channel, 1 beam, 1 receptacle, 1 lwr hinge, 1 name plate, 1 warning plate, 1 upper fitting assy, 1 tee, 2 skin, 1 clip, 1 plate, 1 zee, misc hardware; nha 53-32502; located at fs 493.00 to fs 515.00 flash well
01-216-4774
Fuselage Section
01-216-4775
Fuselage Section
01-216-4811
Structural Component Air Support
Used on acft model b-52g/h. make from 35-3185-529; opposite p/n -516; heat treat T73 per BAC5602; finish f-2.47; nha 35-35470
01-216-4814
Structural Aircraft Panel
Used on acft model b-52g/h. al alloy clad sheet 2024-T4 per qq-a-369; finish f-2.115; 22.30 in. lg, 9.30 in. w, 0.032 in. thk; nha 35-21732
01-216-4815
Structural Aircraft Panel
Used on acft model b-52g/h. al alloy clad sheet 2024-T4 per qq-a-362; finish f-2.115; 23.00 in. lg, 17.00 in. w, 0.032 in. thk; nha 35-21732
01-216-5658
Aircraft Windshield Panel
01-216-5659
Aircraft Windshield Panel
01-216-5839
Structural Component Air Bracket
57.000" overall length 12.000" overall width 2.000" material thickness
01-216-5840
Structural Component Air Bracket
57.000" overall length 12.000" overall width 2.000" material thickness
