01-295-5901
Aircraft Former
Used on C-130. make from LS4224 by 23.00 in lg; nha -41r
01-295-5902
Aircraft Former
01-295-5903
Aircraft Former
Used on C-130.
01-295-5904
Aircraft Former
Used on C-130.
01-295-5905
Aircraft Former
Used on F-15. make from 68A315024-2001; nha 68A315004
01-295-5910
Aircraft Skin
Used on C-141. T3 clad
01-295-5912
Aircraft Skin
Used on C-141. 33.000" overall length 21.000" overall width T6
01-295-7708
Access Aircraft Door
Used on f-15 acft. access lower gun
01-295-7800
Structural Aircraft Plate
Filler
01-295-7801
Structural Aircraft Plate
6.000" overall length 5.000" overall width 0.050" material thickness T81 clad; mms 1410; NHA68A118002
01-295-7802
Aircraft Fairing
01-295-7804
Structural Component Air Support
Used on c-130 acft. angle u/o cargo door
01-295-7805
Structural Component Air Support
U/a: angle
01-295-7806
Structural Component Air Support
Used on c-130 acft. angle u/o aft cargo door
01-295-7807
Structural Component Air Support
Used on c-130 acft. al alloy 7075-0 clad; angle u/o cargo ramp pedestal
01-295-7808
Structural Component Air Support
01-295-7809
Structural Component Air Support
U/a: clip
01-295-7811
Structural Component Air Support
Used on acft model f-15. consist of 2 pin, 1 support, 2 adapter, misc hardware; nha -1001
01-295-7825
Aircraft Former
Used on C-130.
01-295-7826
Aircraft Former
Used on F-15.
01-295-7827
Aircraft Former
Used on C-130. consist of 1 ring segment, 2 filler; nha 373058-3
01-295-7830
Aircraft Former
Used on F-15. 1MA160B01-10300 by 100.00 in.
01-295-7831
Aircraft Former
Used on F-15. 1MA160801-10300 by 100.00 in.
01-295-7832
Aircraft Former
Used on F-15. 1MA160B01-10300 by 100.00
01-295-7833
Aircraft Former
Used on F-15. 1MA160B01-10300 by 100.00 in.
01-295-7834
Longeron
Used on C-130. make from LS5000 by 29.8 in; heat treat T6, lac 521; finish f-1; nha 372902-1
01-295-7835
Longeron
Used on C-130. make from LS5000 by 29.8 in; heat treat T6 LAC521; finish f-1; nha 372902-1
01-295-7837
Aircraft Skin
Used on F-16.
01-295-7838
Aircraft Skin
Used on C-130.
01-295-7839
Aircraft Stringer
01-295-8079
Structural Aircraft Plate
31.000" overall length 16.000" overall width 3.000" material thickness lwr; matl FMS3002-T851; NHA16B560-801
01-295-8080
Structural Aircraft Plate
7.000" overall length 1.000" overall width 0.050" material thickness NHA12K3369-4 skin assy, lwr frame-canopy hatch
01-295-8081
Structural Aircraft Plate
11.000" overall length 1.000" overall width 0.050" material thickness nha 12K3369-4 skin assy, lwr frame-canopy hatch
01-295-8082
Structural Aircraft Plate
T73 clad; guide-mpcd support
01-295-8083
Structural Component Air Support
Used on h-53 hel. angle-frame cap, fuselage sta 522
01-295-8084
Structural Component Air Support
Used on h-53 hel. angle-frame cap, fuselage sta 522
01-295-8085
Structural Component Air Support
Matl:al aly clad; temper T3; u/a support-bracket-fuel line
01-295-8086
Structural Component Air Support
Matl:al aly clad; temper T3; u/a support-channel-fuel line
01-295-8087
Structural Component Air Support
P/o: helicopter refueling mod
01-295-8088
Structural Component Air Support
Used on f-15 acft. al alloy 7075-T7351; support, brake pedal output-outboard
01-295-8089
Structural Component Air Support
Used on f-15 acft. stiffener-upper leading edge
01-295-8090
Structural Component Air Support
Used on f-15 acft. stiffener-upper leading edge
01-295-8091
Structural Component Air Support
Used on f-15 acft. stiffener-upper leading edge
01-295-8092
Structural Component Air Support
Used on f-15 acft. stiffener-upper leading edge
01-295-8093
Structural Component Air Support
Used on f-15 acft. stiffener-upper leading edge
01-295-8094
Structural Component Air Support
Used on f-15 acft. stiffener-upper leading edge
01-295-8095
Structural Component Air Support
Used on f-15 acft. al alloy 2024-0 clad; support-outboard instrument panel
01-295-8096
Structural Aircraft Panel
01-295-9550
Structural Component Air Support
82.000" overall length 5.000" overall width 0.063" material thickness wing root fairing support
01-295-9599
Aircraft Former
21.000" overall length 18.000" overall width 2.250" material thickness former-nacelle; NHA6-11450
