01-268-1633
Structural Aircraft Plate
Used on C-141.
01-268-1634
Structural Aircraft Plate
Used on C-141. T6
01-268-1635
Structural Aircraft Plate
Used on C-141. T6
01-268-1638
Structural Aircraft Plate
Used on C-141.
01-268-1639
Structural Aircraft Plate
Used on C-141.
01-268-1640
Aircraft Fairing
Used on C-141.
01-268-1641
Structural Component Air Support
10.070" overall length 2.300" overall width
01-268-1642
Structural Component Air Support
01-268-1656
Longeron
Used on C-141. PH15-7M0
01-268-1657
Aircraft Skin
Used on C-141. T6 clad
01-268-1658
Aircraft Skin
Used on C-141. 48.000" overall length 21.000" overall width T6
01-268-1659
Aircraft Skin
Used on C-141. 44.000" overall length 18.000" overall width T6, cond 0
01-268-1660
Aircraft Skin
Used on C-141. 32.000" overall length 19.000" overall width T6
01-268-1661
Aircraft Skin
Used on C-141. 57.000" overall length 15.000" overall width T6
01-268-1662
Aircraft Skin
Used on C-141. 43.000" overall length 12.000" overall width T6
01-268-1663
Aircraft Skin
Used on C-141. T6 clad
01-268-1664
Aircraft Skin
Used on C-141. 60.000" overall length 8.000" overall width T6 clad
01-268-1665
Aircraft Stringer
9.000" overall length 5.000" overall width 0.050" material thickness
01-268-1956
Access Aircraft Door
Used on acft model f15. consist of 1 door, misc hardware; nha 68A330002; used on outbd thrust mount access door
01-268-2032
Structural Aircraft Plate
Used on c-5 galaxy airplane.... used in the fire detector system
01-268-2033
Structural Aircraft Plate
Used on C-141. T6, cond 0
01-268-2034
Structural Aircraft Plate
Used on C-141. 4.000" overall length 2.000" overall width 0.040" material thickness PH15-7mo
01-268-2035
Structural Aircraft Plate
Used on C-141. 42.000" overall length 9.000" overall width 0.071" material thickness cond 0 T6
01-268-2037
Structural Aircraft Plate
Used on F-15. 13.000" overall length 2.100" overall width 0.036" material thickness channel
01-268-2038
Structural Aircraft Plate
Used on F-15. 12.300" overall length 2.000" overall width 0.032" material thickness strap stabilization
01-268-2039
Structural Aircraft Plate
Used on F-15.
01-268-2040
Structural Aircraft Plate
Used on F-15. 64.800" overall length 4.620" overall width 0.125" material thickness
01-268-2041
Structural Aircraft Plate
Used on F-15. 64.800" overall length 4.620" overall width 0.125" material thickness
01-268-2042
Aircraft Fairing
01-268-2043
Aircraft Fairing
01-268-2045
Structural Component Air Support
Used on c-5 aircraft. used on fire detector system
01-268-2046
Structural Component Air Support
Used on acft model kc-135. consist of 2 foil marker, 1 pan, 2 clip, 1 rear cover, 2 side cover, 14 angle, 2 front cover, 4 bracket, misc hardware; nha 458-54956
01-268-2047
Structural Component Air Support
Used on acft model f-111.
01-268-2048
Structural Component Air Support
Used on c-141 acft. no.1 vane angle
01-268-2050
Structural Component Air Support
01-268-2051
Structural Component Air Support
01-268-2053
Structural Component Air Support
Used on c-141 acft. al alloy 2024-0, T6 clad; 0/a dim. 2.0 by 8.0 by 0.071 in.; angle u/o frame, aft cowl
01-268-2054
Structural Component Air Support
Used on f-15 acft. bracket, electrical support-missile launcher plug
01-268-2055
Structural Component Air Support
Used on f-15 acft. al alloy 2024-0; frame, leading edge-outer wing
01-268-2056
Structural Component Air Support
Used on f-15 acft. al alloy 2024-0; frame, leading edge-outer wing, removeable section
01-268-2057
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046, type 3, comp c, annealed; o/a dim. 10.000 by 5.400 by 0.750 in.; support-engine throttle sector box
01-268-2058
Structural Component Air Support
Used on f-15 acft. stiffener-aft missile launcher support, lower
01-268-2059
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046, type 3, comp c, annealed; o/a dim. 10.000 by 4.250 by 1.500 in.; u/o missile well skin
01-268-2064
Structural Aircraft Panel
16.100" overall length 8.000" overall width nha 68A112155
01-268-2065
Structural Aircraft Panel
16.100" overall length 8.000" overall width nha 68A112155
01-268-2086
Aircraft Former
8.000" overall length 2.000" overall width 0.071" material thickness ht tr T6; nha 3P21601
01-268-2088
Aircraft Former
Used on C-141.
01-268-2089
Aircraft Former
Used on C-141.
01-268-2090
Aircraft Former
Used on C-141. 0 clad
01-268-2091
Aircraft Former
65.000" overall length 3.000" overall width 0.071" material thickness nha 3P21602
