Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
00-202-5364
Supplemental Small Arms-fr Armor
Steel mil-a-46099
00-202-5414
Bleed Air Duct Assembly
Steel, mil-s-8840
00-202-5420
Bleed Air Duct Assembly
Steel, mil-s-8840
00-202-5455
Aircraft Floor
00-202-5456
Aircraft Floor
00-202-5489
Access Aircraft Door
00-202-5490
Access Aircraft Door
00-202-6131
Structural Aircraft Plate
19.950" overall length 3.750" overall width 0.032" material thickness strip
00-203-1100
Fuselage Section
Glass fabric per 299-947-012, type viii, fscm 97499, aluminum ALLOY5052 honeycomb, titanium alloy, mil-t-9046
00-203-1135
Fuselage Section
Titanium alloy, mil-t-9046, composition b, type i, aluminum alloy honeycomb per 299-947-059 type 2 fscm 97499, and glass fabric per 299-947-057 type c fscm 97499;
00-203-1144
Fuselage Section
Aluminum alloy honeycomb per 299-947-059 type 2 fscm 97499, glass fabric per 299-947-057 type c fscm 97499, titanium alloy, mil-t-9046, type 3 composition c, and type i composition b
00-203-1168
Aircraft Floor
Titanium alloy mil-t-9046 type i composition b, aluminum alloyhoneycomb composition b per 299-947-059 type 2 fscm 97499, glass fabric PER299-947-057 type c fscm 97499
00-203-1178
Aircraft Floor
Titanium alloy mil-t-9046 type i composition b, aluminum alloyhoneycomb composition b per 299-947-059 type 2 fscm 97499, glass fabric PER299-947-057 type c fscm 97499
00-203-8421
Bell Crank
00-203-8422
Bell Crank
00-203-8436
Structural Component Air Fitting
00-204-3702
Aircraft Window Panel
Used on c-141 acft. matl acrylic plastic, mil-p-25690; 10.900 in. lg; 8.300 in. w; 0.530 in. min to 0.710 in. max thk; 0.228 min. in. to 0.248 max in. dia 7 places; used for main landing gear inspection
00-204-4494
Aircraft Fairing
Used on a-7e aircraft. 0.040" material thickness
00-204-4497
Aircraft Fairing
Used on a-7e aircraft. 0.040" material thickness
00-204-4635
Aircraft Fairing
Used on a-7e aircraft. 0.040" material thickness
00-204-4636
Aircraft Fairing
Used on a-7e aircraft. 0.040" material thickness
00-204-5801
Aircraft Door
00-204-5804
Aircraft Door
00-204-5830
Fluid Aircraft Manifold
17.750" overall length 9.900" overall width
00-204-5909
Fluid Aircraft Manifold
27.250" overall length
00-204-5912
Fluid Aircraft Manifold
59.680" overall length
00-204-5915
Fluid Aircraft Manifold
00-204-5934
Fluid Aircraft Manifold
00-204-6262
Aircraft Leading Edge
00-204-6274
Fuselage Section
00-204-6781
Pressure Fuel Servicing Adapter
00-204-6885
Structural Component Air Support
Make from 327 annealed steel
00-204-6897
Structural Component Air Fitting
2.270" overall length u/a: spoiler drive tube fitting; temper T651; matl:2.860in dia
00-205-2188
Aircraft Floor
Used on helicopter model rh-53d.
00-205-2252
Aircraft Fairing
Used on a-7e aircraft. 0.040" material thickness
00-205-2327
Structural Aircraft Plate
6.380" overall length 1.700" overall width 0.190" material thickness
00-205-2328
Structural Aircraft Plate
6.380" overall length 1.700" overall width 0.190" material thickness
00-205-6526
Fluid Aircraft Manifold
00-205-7145
Access Aircraft Door
00-205-7174
Radome
Used on model b52h.
00-205-7191
Aircraft Fairing
00-205-8414
Aircraft Bulkhead
Used on aircraft model c130.
00-207-4927
Aircraft Skin
31.000" overall length 17.000" overall width
00-208-3241
Structural Component Air Support
7.460" overall length
00-208-3278
Aircraft Beam
00-208-3330
Aircraft Skin
Used on aircraft,f-4.
00-208-3376
Aircraft Latch Assembly
Used on 15603404202. c/o 1 pin, 1 spring, 1 handle assembly, 1 actuator, 1 housing
00-208-3689
Aircraft Skin
00-208-3690
Aircraft Skin
00-208-3692
Aircraft Window Panel
12.500" overall length 6.680" overall width
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