01-449-5329
Structural Aircraft Plate
1.940" overall length 0.500" overall width 9.190" material thickness manufacturer suggested name-filler; u/o f-15s 1up
01-449-5330
Structural Component Air Support
U/o f-15s 13up, f-15i 1up; next higher assy 68A116128
01-449-5526
Aircraft Skin
Used on b-2 bomber. this item contains hardness critical processes lear effect (s) of thermal
01-449-5540
Aircraft Skin
Used on b-2 bomber. this item contains hardness critical processes (hcps) for the nuclear effect (s) of thermal
01-449-5693
Aircraft Fairing
Used on b-2 bomber. 7.550" overall length this item contains hardness critical processes (hcp) for the nuclear effect (s) of over pressure//thermal
01-449-5761
Aircraft Fairing
Used on sikorsky ch-3 helicopter.
01-449-5938
Structural Component Air Support
Used on the chinook helicopter
01-449-5963
Structural Aircraft Plate
Used on b-2 bomber.
01-449-6052
Structural Aircraft Panel
01-449-6080
Structural Aircraft Panel
Used on part number 75a800502. part name assigned by manufacturer panel
01-449-6180
Access Aircraft Door
Used on F-15S. u/o f-15s 1 to 24; next higher assy 68A333011
01-449-6192
Structural Component Air Support
U/o f-15s 13up, f-15i 1up; next higher assy 68A116128
01-449-6225
Aircraft Skin
Used on p-3 aircraft.
01-449-6228
Aircraft Skin
Used on p-3 aircraft.
01-449-6229
Aircraft Skin
Used on p-3 aircraft.
01-449-6233
Aircraft Skin
Used on p-3 aircraft.
01-449-6239
Aircraft Skin
Used on p-3 aircraft.
01-449-6243
Aircraft Skin
Used on p-3 aircraft.
01-449-6250
Structural Component Air Support
Used on the chinook helicopter
01-449-6256
Structural Component Air Support
Used on the chinook helicopter
01-449-6309
Aircraft Skin
Used on p-3 aircraft.
01-449-6328
Aircraft Skin
Used on p-3 aircraft.
01-449-6330
Aircraft Skin
Used on p-3 aircraft.
01-449-6338
Aircraft Skin
Used on p-3 aircraft.
01-449-6339
Aircraft Skin
Used on p-3 aircraft.
01-449-6341
Aircraft Skin
Used on p-3 aircraft.
01-449-6344
Aircraft Skin
Used on p-3 aircraft.
01-449-6345
Aircraft Skin
Used on p-3 aircraft.
01-449-6350
Aircraft Latch Assembly
Used on e-2c aircraft.
01-449-6355
Access Aircraft Cover
Used on e-2c aircraft.
01-449-6555
Aircraft Trailing Edge
01-449-6556
Aircraft Trailing Edge
01-449-6565
Structural Component Air Bracket
1.630" overall length 1.500" overall width 1.500" material thickness rmanufacturer suggested name-link attach-spring bungee clip; heat treat ph steel per ST0111LA0008 to condition: H1025 after machining; matl:AMS5643 cres bar alloy 17-4ph; n/a: L3223760; opposite -003; u/o acft 1 & subq
01-449-6566
Structural Aircraft Panel
21.700" overall length 13.000" overall width featgmanufacturer suggested name-panel, wedge, pivoting-underwing fairing; nha -001; finish 60ha & LA0108-038 on outer surface of -003; matl: class 301 temp 1/2h 301 cres sh; opposite -004
01-449-6567
Structural Aircraft Panel
21.500" overall length 12.500" overall width manufacturer suggested name-panel, pivoting-underwing fairing; nha -001 assy; heat treat to cond T62 per ST0111LA0009; fin 11AB02; matl:al clad sh; 0 temper; opposite -080
01-449-6568
Structural Aircraft Panel
21.700" overall length 13.000" overall width manufacturer suggested name-panel, wedge, pivoting-underwing fairing; nha: -002; matl: class 301 temp 1/2h 301 cres ch; opposite -003
01-449-6569
Aircraft Stiffener
1.050" overall length 0.030" overall width 0.063" material thickness manufacturer suggested name-fitting, bungee attach, shim; matl:comp 301 cond 1/2h, 301 cres sheet; nha -001
01-449-6570
Structural Aircraft Panel
15.700" overall length 8.000" overall width nnuclear hardness critical item; manufacturer suggested name-panel, wedge, pivoting-underwing faring; nha -001 assy; heat treat to cond T62 per ST0111LA0009; finish 11AB02; matl: al clad sh; 0 temper; opposite -078
01-449-6571
Structural Aircraft Panel
15.700" overall length 8.000" overall width pnuclear hardness critical item; manufacturer suggested name-panel, wedge, pivoting-underwing fairing; nha: -002 assy; heat treat to cond T62 per ST0111LA0009; finish 11AB02; matl: al clad sh; 0 temper; opposite -077
01-449-6572
Aircraft Stiffener
1.050" overall length 0.030" overall width 0.063" material thickness manufacturer suggested name-fitting, bungee attach, shim; matl:comp 301 cond 1/2h, 301 cres sheet; nha -002
01-449-6913
Radome
Used on kc-135 aircraft. manufacturer suggested name-radome assembly, nose, CMN2000 core, x-band
01-449-6922
Aircraft Spar
Made from 68A112132-2011 forging, 6al-4v mil-f-83142 composition 6 condition a; p/n 68A112107-2080 is the opposite configuration
01-449-6923
Aircraft Spar
Made from 68A112132-2012 forging, 6al-4v mil-f-83142 composition 6 condition a; p/n 68A112107-2079 is the opposite configuration
01-449-7304
Structural Component Air Bracket
6.750" overall length
01-449-7336
Fuel Aircraft Tank
01-449-7337
Fuel Aircraft Tank
01-449-7717
Structural Aircraft Panel
20.000" overall length 9.000" overall width manufacturer suggested name; panel, underwing pivoting wedge fairing assembly; opposite -7; heat treat T62 per ST0111LA0009
01-449-7718
Aircraft Channel
9.740" overall length 3.800" overall width 0.080" material thickness manufacture suggested name; panel, underwing pivoting wedge fairing assembly; opposite -019; heat treat T62 per ST0111LA0009
01-449-7719
Aircraft Channel
9.740" overall length 3.800" overall width 0.080" material thickness manufacturer suggested name; panel, underwing pivoting wedge fairing assembly; opposite -020; heat treat T62 per ST0111LA0009
01-449-7722
Structural Aircraft Panel
20.000" overall length 9.000" overall width manufacturer suggested name; panel, underwing pivoting wedge fairing assembly; heat treat T62 per ST0111LA0009; opposite -8
