Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
00-518-5444
Access Aircraft Door
00-518-6647
Airfoil Rib
00-518-6663
Airfoil Rib
00-518-6678
Fluid Aircraft Manifold
00-518-6679
Fluid Aircraft Manifold
53.770" overall length
00-518-6685
Structural Aircraft Plate
0.360" overall length 0.032" material thickness
00-518-6720
Structural Aircraft Plate
80.000" overall length 1.000" overall width
00-518-6721
Structural Aircraft Plate
Used on acft model kc-135. aluminum alloy, qq-a-200/3, alloy 2024, 1.000 in. w, 100.000 in. lg
00-518-6726
Structural Aircraft Plate
Used on acft model kc-135. aluminum alloy, qq-a-200/3, alloy 2024, 1.000 in. w, 80.000 in. lg
00-518-6727
Structural Aircraft Plate
Used on acft model kc-135. aluminum alloy, qq-a-200/3, alloy 2024, 1.000 in. w, 100.000 in. lg
00-518-6844
Structural Component Air Support
Aluminum alloy, AMS4260, alloy 356, T6
00-518-6880
Aircraft Window Panel
Used on uh-1f iroquois helicopter.
00-518-6889
Aileron
00-518-7824
Structural Component Air Support
5.180" overall length 5.000" overall width 0.063" material thickness
00-518-7880
Structural Component Air Support
Used on acft model f4c. c/o tube p/n 53-830073, flange p/n 53-830073-5, located fuselage station 333.35 upper
00-518-8271
Aircraft Skin
78.000" overall length 53.000" overall width function-aileron closure, lower
00-518-8274
Aircraft Skin
78.000" overall length 53.000" overall width
00-518-8447
Structural Component Air Fitting
00-518-8774
Aircraft Skin
Used on F-4. 12.300" overall length 1.900" overall width function-upper leading edge closure, c.s.w.; matl class d
00-518-8775
Aircraft Skin
Used on F-4. 12.300" overall length 1.900" overall width function-upper leading edge closure, c.s.w.; matl class d
00-518-8890
Aircraft Trailing Edge
115.000" overall length 7.500" overall width 1.250" material thickness
00-518-8894
Aircraft Trailing Edge
00-520-0734
Aircraft Tip
Aluminum alloy
00-520-0735
Aircraft Tip
Aluminum alloy
00-520-0904
Aircraft Fireseal
00-520-0942
Aircraft Fairing
00-520-0943
Aircraft Fairing
00-520-0949
Fuel Aircraft Tank
00-520-0950
Fuel Aircraft Tank
This item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition
00-520-0951
Fuel Aircraft Tank
00-520-0952
Fuel Aircraft Tank
00-520-1810
Access Aircraft Door
00-520-2730
Structural Component Air Support
00-520-2732
Structural Component Air Support
00-520-2734
Structural Component Air Support
Used on C-5A.
00-520-2735
Access Aircraft Cover
00-520-3615
Aircraft Stringer
00-520-3769
Fluid Aircraft Manifold
4.440" overall length 3.190" overall width
00-520-3828
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, AMS4260
00-520-3842
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, qq-a-225/6, 2.444 in. lg, 1.500 in. w, 1.130 in. h, 3 holes 0.093 in. dia
00-520-3844
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, qq-a-200/3, 2.260 in. lg, 2.010 in. w, 2.238 in. h, 2 holes 0.500 in. dia, 3 holes 0.132 in. dia
00-520-3845
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, qq-a-200/3, 2.312 in. lg, 1.718 in. w, 2.000 in. h, 2 holes 0.500 in. dia, 4 holes 0.132 in. dia
00-520-4513
Aircraft Window Panel
00-520-4538
Structural Component Air Support
Used on acft model b57. steel per mil-s-6721 composition T6, 5.625 in. lg, 2.375 in. w, 0.044 in. thk
00-520-4842
Structural Component Air Bracket
00-520-5078
Aircraft Floor
Used on C-130. 23.000" overall width 1.700 height
00-520-5080
Aircraft Floor
Used on C-130. 23.000" overall width 1.700 in. o/a height
00-520-5086
Aircraft Floor
Used on aircraft model c-130. 42.480" overall length 32.540" overall width
00-520-5098
Aircraft Fairing
00-520-5100
Aircraft Tip
Heat treat T3
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