01-530-6313
Aircraft Skin
179.000" overall length 65.000" overall width
01-530-6314
Aircraft Skin
103.000" overall length 67.000" overall width replaces -118a
01-530-6315
Aircraft Skin
111.000" overall length 67.000" overall width replaces -117a
01-530-6317
Aircraft Skin
Used on c-5 model acft. 145.000" overall length 71.000" overall width skin heat treat T761
01-530-6400
Structural Component Air Support
Used on c-135 acft. 3.200" overall length 3.100" overall width 0.032" material thickness bulkhead tab spar, elevator heat treat 0; opp -23
01-530-6417
Structural Component Air Support
Used on c-135 acft. 3.200" overall length 3.100" overall width 0.032" material thickness bulkhead-tab spar, elevator heat treat 0; clad sheet
01-530-6439
Structural Aircraft Plate
01-530-6507
Structural Component Air Support
Used on e-8 joint stars. support next higher assy 525-11340
01-530-6510
Structural Component Air Support
Used on e-8 joint stars. support ext higher assy 525-11340
01-530-6712
Aircraft Door
Used on hh-3f helicopter. next higher assembly S6182-20108-063; door assembly
01-530-6713
Structural Aircraft Plate
Used on hh-3f,sikrosky,helicopter. ccnt panel ramp; next higher assembly S6192-61340-001
01-530-6729
Structural Aircraft Panel
Used on 70500-24003-046. rack assembly
01-530-6904
Aircraft Skin
Used on e-2c; skin-cont surf-rh inbd rudder. navy: cover assembly
01-530-6909
Structural Component Air Support
Used on c92a; support fus-mid sect-entrance door mechanism. 3.500" overall length 2.250" overall width navy; fitting assembly alodize surface treated
01-530-6942
Stiffener Aircraft Rib
Used on c-2a/e-2c; rib-power plant-oil cooler, exit flap. 10.000" overall length 5.000" overall width 0.050" material thickness navy: rib assembly next higher assembly=123P10315 anodize surface treated
01-530-6947
Structural Component Air Support
Used on c-2afus tail-sect cl car dr fs 659.557 wl 46 cyl atch. 6.500" overall length navy: fitting assembly nha=123B41207 anodize surface treated
01-530-6955
Access Aircraft Cover
Used on c-2a; cover assembly lh console cockpit. navy: cover assembly 5 mounting holes each side
01-530-6971
Structural Component Air Support
Used on c-2a;fus mid sect sta 265.500-266.469 wg fairing. 20.000" overall length 5.000" overall width 0.040" material thickness navy:support assembly nha=123B41256 anodize surface treated
01-530-7005
Aircraft Skin
Used on e-2a; cont surf stab . upr skin sta 54 and 148. 25.000" overall length 13.000" overall width navy: door assembly 123CS10141-5 is an interchanagable part per mil-i-8500 anodize surface treated
01-530-7012
Aircraft Skin
Used on e-2a; cont surf stab . upr skin sta 54 and 148. 25.000" overall length 13.000" overall width navy: door assembly 123CS10141-6 is an interchanagable part per mil-i-8500 anodize surface treated
01-530-7016
Stiffener Aircraft Rib
Used on c-2a: cont surf, rudder outbd, le. navy: rib assembly
01-530-7022
Stiffener Aircraft Rib
Used on c-2a: cont surf, rudder outbd, le. navy: rib assembly
01-530-7047
Aircraft Door
Used on e-2a; fairing-control surfaces-outbd rudder. 5.000" overall length 5.000" overall width navy: door assembly
01-530-7061
Aircraft Door
Used on e-2a; fairing- cont surf-outbd rudder. 5.000" overall length 5.000" overall width navy: door assembly
01-530-7063
Aircraft Trailing Edge
Used on kdc-10 aircraft. 54.000" overall length
01-530-7238
Bleed Air Duct Assembly
24.250" overall length 4.500" overall width duct nha 17P2N9004; u/o 17A001-34, 17T001 acft; dim. are stock matl.size; c/o 1 flange, 2 duct end, 1 duct
01-530-7239
Aircraft Skin
Used on c-5 aircraft. 187.000" overall length 65.000" overall width replaces -105a skins; dim. are stock matl; clad; heat treat cond-T761
01-530-7240
Bleed Air Duct Assembly
Duct u/o 17A001-034, 17T001 acft; nha 17P2N9004, sheet; c/o 1 flange, 1 ductend
01-530-7248
Structural Component Air Support
01-530-7251
Structural Component Air Bracket
01-530-7262
Structural Component Air Bracket
01-530-7300
Fastener Parts Kit
Used on f-16 acft.
01-530-7325
Structural Component Air Support
Used on f/a-18 e/f; support-swing joint, lever, main landing gear. navy: support, aircraft, ma
01-530-7332
Structural Component Air Support
Used on f/a-18 e/f; support-swing joint, lever, main landing gear. navy: support, aircraft, ma
01-530-7367
Aircraft Pylon
Used on tornado aircraft. strut assembly next higher assembly buddy-buddy refueling pod
01-530-7368
Aircraft Pylon
Used on tornado aircraft. strut assembly next higher assembly buddy-buddy refueling pod
01-530-7446
Cowling
Used on approach light system (als). stand-off
01-530-7548
Refueling Aircraft Tank
Used on tornado aircraft. store assembly, aerial buddy-buddy refueling
01-530-7559
Structural Component Air Support
01-530-7594
Structural Aircraft Panel
Used on f/a-22 raptor. finish assy c/o 1 ref panel assy 5HW82821-154, 2 coating appl, 6 ring, 1 label, 6 bolt
01-530-7595
Structural Aircraft Panel
Used on f/a-22 raptor. finish assy c/o 1 ref 5HW82821-149 panel assy, 2 coating appl, 6 ring, 1 label, 6 bolt
01-530-7596
Aircraft Skin
Used on c-5 acft. 86.000" overall length 67.000" overall width skin heat treat 0
01-530-7597
Structural Component Air Support
Used on c-17 globemaster iii. clevis next higher assembly 17P8D8504; a sub part may be made from 2X3X3 A280 cress per ams 5734 or from 2X3X3 A280 per ams 5737 by full annealing per dps 5.00 before machining
01-530-7802
Structural Component Air Support
01-530-7803
Structural Component Air Support
01-530-7804
Structural Component Air Support
01-530-7805
Structural Component Air Support
01-530-7806
Structural Component Air Support
01-530-7841
Movable Canopy
Used on f/a-22 raptor. canopy
01-530-7842
Structural Component Air Support
Used on f/22 raptor. support
