01-510-2564
Structural Aircraft Panel
01-510-2679
Structural Aircraft Panel
01-510-2700
Structural Aircraft Panel
01-510-2725
Aircraft Stringer
01-510-2758
Structural Aircraft Panel
01-510-2773
Structural Component Air Support
01-510-2866
Structural Component Air Support
Used on f/a-22 raptor. 1.600" overall length 1.370" overall width bracket, assy of
01-510-2869
Structural Component Air Bracket
01-510-2872
Tubing Aircraft Support
01-510-2873
Tubing Aircraft Support
01-510-2884
Wing Landing Flap
Structural assy. inbrd flap NHA17N6P0624-513; c/o 1 fairing inst.
01-510-2885
Wing Landing Flap
Structural assy, inboard flap nha 17N6P0624-514; c/0 1 fairing inst
01-510-2892
Wing Landing Flap
Structural assy, outbrd flap rh; nha 17N60P0624-509; c/o 1 fairing instl
01-510-2893
Wing Landing Flap
Structural assy, outboard flap lh; nha 17N60P0624-510; c/o 1 fairing instl
01-510-3121
Bleed Air Duct Assembly
Duct
01-510-3207
Structural Aircraft Panel
01-510-3438
Structural Component Air Support
1.762" overall length 1.380" overall width 0.055" material thickness extruded h-clip corner 0.016; fillet 0.060
01-510-3443
Structural Component Air Support
1.422" overall length 1.380" overall width 0.040" material thickness extruded h-clip corner 0.016; fillet 0.060
01-510-3444
Structural Component Air Support
1.492" overall length 1.500" overall width 0.063" material thickness extruded h-clip corner 0.016; fillet 0.060
01-510-3445
Access Aircraft Cover
Cover stock size 0.080 x 6 x 7; 3 sharp corners, 1 rounded corner; 6 holes oneach side of long edge evenly spaced, 1 additional hole in center of one edge, 3 additional holes in evenly spaced on opposite edge; total of 16 holes
01-510-3446
Structural Component Air Support
Brace-upper tubing 2024-0 al aly tube; material size 0.049 x 1.00 od x 31; material spec ww-t-785 type i
01-510-3449
Structural Component Air Support
Used on lau-116/a and lau-116a/a aircraft guided missile launcher. support-trim aft, left nha 74A730302; to aw-394ac-750-010
01-510-3463
Structural Component Air Fitting
Used on c-130 aircraft. 0.375 " material thickness fiting
01-510-3466
Structural Aircraft Plate
0.188" material thickness gusset 6-3/16 dia lock bolt holes; 5-3/16 dia lockbolt holes; 2-1/4 dia lockbolt holes; 15-3/16 dia lockbolt holes; 5 holes 0.193 min 0.199 max dia
01-510-3482
Structural Aircraft Plate
Used on 1520-01-088-3669: t.m.1520-240-23p.
01-510-3484
Structural Component Air Support
Used on 1520-01-088-3669: t.m.1520-240-23p.
01-510-3488
Structural Component Air Support
Used on 1520-01-088-3669: t.m.1520-240-23p.
01-510-3495
Structural Component Air Support
Used on 1520-01-088-3669: t.m.1520-240-23p.
01-510-3505
Access Aircraft Cover
Cover assembly
01-510-3614
Aircraft Fairing
Upper, removable, nha 17P4T4003-1, effectivity 17A081-17A999; same as -507 except ecn chgs.; c/o 1 fairing, 42 nutplate, 1309 pin-rivet, 110 pin, 1522 collar
01-510-3615
Aircraft Fairing
Upper, removable; nha 17P4T4003-1; effectivity 17A081-17A999; same as -507except for ecn chgs; c/o 1 fairing, 42nutplates, 1309 pin-rivet, 110 pins, 1522 collars
01-510-3616
Aircraft Fireseal
10.600" overall length 5.000" overall width fire shield operational requirements include temp range of -65 deg to 1250 deg f anfire resistant to 2000 deg f for 5 mins, operating altitude of 45, 000 ft max, ambient temp -65 deg f to 250 deg f
01-510-3885
Structural Component Air Fitting
01-510-3900
Structural Component Air Fitting
01-510-3921
Window Aircraft Frame
Used on 1520-01-088-3669: t.m.1520-240-23p.
01-510-3947
Aircraft Ramp Assembly
Used on 1520-01-088-3669: t.m.1520-240-23p.
01-510-3951
Air Wing Fairing Inflatable Seal
Used on 1520-01-088-3669: t.m.1520-240-23p.
01-510-4067
Aircraft Engine Installation Kit
01-510-4444
Structural Component Air Fitting
Used on CH-60. track assy nha is tract inst sta 241-327, main rotor pylon
01-510-4449
Structural Component Air Fitting
Used on CH-60. track assy nha is tract inst sta 241-327, main rotor pylon
01-510-4554
Structural Component Air Bracket
01-510-4651
Structural Component Air Bracket
Nha 12W9931 translating track-outbd, flap no 5; all surfaces to be finished per fps-1006, code D021, except the electroless nickel plating to be 0.0015 P0.0005, M0.0000 thick, shot peen all surfaces except holes; prime all surfaces after nickle plating
01-510-4843
Structural Aircraft Plate
8.400" overall length 7.700" overall width 0.375" material thickness doubler finish f-29959, f-12.101, except use fed std 595 color no 37200, penetrantinspect per bac 5423; dim are stock matl
01-510-4990
Aircraft Engine Installation Kit
Used on c/kc-130f/r/t. engine nacelle, parts list name on nsn request = qeck assembly, aircraft
01-510-5391
Aircraft Fairing
01-510-5509
Structural Component Air Fitting
Used on helicopter,cargo transport. 1.750" overall length 1.350" overall width 0.100 " material thickness
01-510-5550
Aircraft Fairing
01-510-5563
Aircraft Fairing
01-510-5650
Structural Aircraft Plate
8.400" overall length 7.700" overall width 0.375" material thickness doubler finish f-29959, f-12.101, except use fed std 595 color no 37200, penetrant inspect per bac 5423; dim are stock matl
