01-533-1751
Aircraft Skin
86.000" overall length 56.000" overall width dim. are stock material
01-533-1760
Aircraft Door
Used on c2a-2 aircraft. 4.500" overall length 4.750" overall width
01-533-1762
Aircraft Door
Used on c2a-2 aircraft. 5.500" overall length 6.000" overall width
01-533-1765
Aircraft Door
Used on c2a-2 aircraft. 4.562" overall length 6.187" overall width
01-533-1773
Aircraft Fairing
Used on e-2a aircraft; fairing assy, control surf-outbd rudder upper. 0.032" material thickness consists of aluminum stiffener (5" x 8.250")
01-533-1787
Seal Replacement Mecha Parts Kit
Used on f/a-18a/b/c/d acft. seal kit ehv face flight safety critical item,
01-533-1788
Aircraft Fairing
Used on c-2a aircraft; fairing assy, control surf-slab fin. consists of a fairing, 2 doublers,
01-533-1790
Seal Replacement Mecha Parts Kit
Used on f/a-18a/b/c/d acft.
01-533-1795
Stiffener Aircraft Rib
Used on c-2a/e-2a; control surface-rh inbd tab. rib assembly
01-533-1801
Aircraft Skin
Used on e-2c aircraft; skin, control surface-rh inbd rudder. 9.000" overall length 16.000" overall width anodize surface treated
01-533-1811
Stiffener Aircraft Rib
Used on c-2a/e-2c aircraft. 0.020" material thickness rib
01-533-1813
Structural Aircraft Plate
Used on e-2a aircraft. 10.000" overall length 35.000" overall width 0.050" material thickness doubler
01-533-1826
Aircraft Skin
Used on e-2a aircraft. skin assembly
01-533-1848
Aircraft Skin
84.000" overall length 31.000" overall width outboard accessary compartment door skin nacelle heat treat 0
01-533-1850
Aircraft Skin
86.000" overall length 56.000" overall width outboard accessary compartment door skin nacelle heat treat 0
01-533-1851
Aircraft Skin
82.000" overall length 56.000" overall width outboard accessary compartment door skin nacelle heat treat 0
01-533-1965
Aircraft Skin
Used on A-10A. 36.000" overall length 26.000" overall width skin heat treat T0; dim. are stocksize
01-533-1970
Aircraft Skin
Used on A-10A. 32.000" overall length 31.000" overall width skin heat treat 0; dim. are stocksize
01-533-1995
Access Aircraft Door
01-533-2008
Aircraft Latch Assembly
Used on f-22 raptor. latch, door
01-533-2056
Access Aircraft Door
Used on c-2a aircraft; door assy, fus-fwd sect-sta 49.120-56.813-taxi light. door assembly assembly consists of 1 door, 1 glass assembly, 1 zee, 4 angles, 2 clip, 1 half-hinge, 4 retainers, 1 seal, 1 fitting, 1 grommet, 16 screws, 16 nut plates, 1 cover, 1 strap, anodize surface treated
01-533-2123
Structural Component Air Fitting
Outboard hinge, fitting - fillet flap, assembly of opposite -5
01-533-2181
Structural Component Air Fitting
Fitting-hinge bracket, fwd-tip protection - gear wheel door assy of opposite of -516 1560-01-533-2192
01-533-2192
Structural Component Air Fitting
Fitting fitting hinge bracket; opposite of -515 1560-01-533-2181
01-533-2364
Structural Component Air Support
01-533-2365
Structural Component Air Support
01-533-2366
Structural Component Air Support
01-533-2367
Structural Component Air Support
01-533-2470
Structural Component Air Fitting
13.996" overall length 12.412" overall width
01-533-2473
Structural Component Air Fitting
14.162" overall length 12.412" overall width opposite of -025 1560-01-530-3146
01-533-2493
Structural Component Air Fitting
Used on B-52. 2.250" overall length forged block, ultrasonic inspect per mil-std-2154, class b; nha 675-22734; dimensions are stocksize; heat treat T73; finish f-2.47
01-533-2520
Structural Component Air Bracket
Used on B-52. clip
01-533-2772
Aircraft Tip
Opposite la-RE184-56r
01-533-2774
Structural Component Air Support
End cap
01-533-2827
Aircraft Hinge
Used on h46 helicopter. hinge half, engine aircraft
01-533-3037
Access Aircraft Cover
01-533-3038
Structural Component Air Fitting
01-533-3073
Aircraft Fairing
01-533-3245
Fuel Aircraft Tank
Used on f-18 e/f.
01-533-3248
Structural Component Air Fitting
4.250" overall length 1.000" overall width 0.125 " material thickness angle matl AMS5604 cress plate alloy 17-4ph cond H1025; dim are stock matl
01-533-3305
Structural Component Air Fitting
14.750" overall length 14.000" overall width 4.250 " material thickness fitting matl ams cress plate alloy 17-4ph cond h 1025; dim are stock matl
01-533-3335
Structural Aircraft Panel
Used on hercules aircraft, c-130j.
01-533-3594
Structural Aircraft Panel
01-533-3671
Structural Aircraft Plate
Used on B-1B. 5.690" overall length 5.100" overall width 0.560" material thickness nha L1600042; suitable for b-1b 83-0065 thru 86-0140 (acft 2 thru 100) ; heat treat T7351; plate alum; dim. are stocksize
01-533-3688
Structural Aircraft Plate
Used on B-1B. 6.910" overall length 5.010" overall width 0.530" material thickness nha L1600042; effective 83-0065 thru 86-0140 (acft 2 thru 100) ; heat treat T7351; alum. plate; dim. are stocksize
01-533-3693
Structural Aircraft Plate
Used on B-1B. 5.470" overall length 4.810" overall width 0.850" material thickness nha L1600042 suitable for b-1b 83-0065 thru 86-0140 (acft 2 thru 100) ; heat treat T7351; alum plate; dim. are stocksize
01-533-3913
Aircraft Hinge
Used on p3 orion transport aircraft. used on the main electrical load center enclosure
01-533-3920
Aircraft Fairing
Fairing
01-533-3929
Aircraft Fairing
Fairing
01-533-4006
Structural Aircraft Plate
Used on p67 tristar aircraft.
