Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
00-899-6443
Airfoil Rib
00-899-6446
Airfoil Rib
00-899-6453
Airfoil Rib
00-899-6454
Airfoil Rib
00-899-6458
Airfoil Rib
00-899-6503
Airfoil Rib
00-899-6504
Airfoil Rib
00-899-6720
Aircraft Fairing
0.028" material thickness
00-899-7351
Radome
00-899-7714
Aircraft Fairing
00-899-7785
Structural Component Air Support
00-900-4789
Wing Landing Flap
Used on aircraft model o-2. aluminum alloy, 2024 T42
00-900-4792
Wing Landing Flap
Used on aircraft model o-2. aluminum alloy, 2024 T42
00-900-5012
Access Aircraft Door
Spring loaded self-closing
00-900-5014
Cowling
Aluminum alloy;
00-900-5015
Cowling
Aluminum alloy;
00-901-1083
Structural Component Air Support
Used on a-37a/b acft. includes 48 holes, 0.218 in. dia that match engine front frame; used as strap, engine forward
00-901-1385
Access Aircraft Door
00-901-1389
Aircraft Window Panel
00-901-4861
Airfoil Rib
Used on o-2a aircraft.
00-901-4871
Wing Landing Flap
Used on aircraft model o-2. aluminum alloy, 2024 T42
00-901-5134
Aircraft Window Panel
Plastic, acrylic sheet, 28.400 in. lg, 21.100 in. w, 0.187 in. thk,
00-901-5271
Access Aircraft Door
Spring loaded self-closing
00-901-5294
Cowling
Used on aircraft model o-2.
00-901-5299
Aircraft Skin
Aluminum, 2024-T42 clad, 32.000 in. lg, 30.000 in. w, 0.032 in. thk
00-901-5304
Aircraft Skin
00-901-5305
Fuselage Section
00-901-5330
Structural Component Air Support
Used on acft model 02a. steel per mil-s-18729
00-901-5337
Structural Component Air Support
Used on acft model 02a. aluminum alloy 6061 T6, used on blast tube
00-901-5391
Structural Component Air Support
Used on acft model 02a. aluminum alloy 2024, 9.000 in. lg, 8.600 in. w, 0.040 in. thk
00-901-5930
Structural Component Air Support
7.000" overall length
00-901-6254
Aircraft Window Panel
Used on ov-10 airplane.
00-901-6389
Aileron
00-901-6404
Aileron
00-901-6540
Aircraft Window Panel
Plastic, sheet acrylic, 27.400 in. lg, 14.200 in. w, 0.188 in. thk
00-901-6845
Aircraft Floor
Used on aircraft model o2a. aluminum alloy, qq-a-250/5
00-901-8183
Aircraft Spar
94.520" overall length 4.020" overall width 3.900" material thickness
00-901-8185
Aircraft Spar
94.520" overall length 4.020" overall width 3.900" material thickness
00-901-8343
Aircraft Skin
Alluminum alloy, qq&a&250/5, 2024-0 clad, heat treat T4
00-901-8344
Aircraft Skin
Aluminum alloy, qq&a&250/5, 2024-0 clad, heat treat T4
00-901-8633
Access Aircraft Door
2.250" outside diameter primer surface treated
00-901-8660
Bleed Air Duct Assembly
Used on acft model f111. used on engine bleed right hand firewall
00-902-3095
Aircraft Floor
Used on C-130. 121.424" overall length 9.000" overall width
00-902-4822
Fuel Aircraft Tank
Used on u-21a,u-21g,ru-21a,ru-21d,ru-21h,ru-21b and ru-21c.
00-902-4828
Fuel Aircraft Tank
Used on u-21a,u-21g,ru-21a,ru-21d,ru-21h,u-21b and ru-21c.
00-902-4833
Fuel Aircraft Tank
Used on u-21a,u-21g,ru-21a,ru-21d and ru-21h.
00-902-9367
Aircraft Skin
Used on aircraft o-2a.
00-902-9433
Airfoil Rib
Used on o-2a observation airplane. material type T42
00-902-9465
Airfoil Rib
0.020" material thickness material type T42
00-902-9470
Airfoil Rib
0.020" material thickness material type T42
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