Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-398-1906
Structural Component Air Support
01-398-1908
Structural Component Air Fitting
01-398-1909
Structural Component Air Support
01-398-1922
Structural Component Air Fitting
Used on b-52 stratofortress aircraft. 16.000" overall length 6.560" overall width adapter fitting-stub pylon; forged block 7075-01 heat treat t-73;
01-398-1923
Structural Component Air Fitting
Used on b-52 stratofortress aircraft. 16.000" overall length 6.560" overall width adapter fitting-stub pylon; forged block 7075-01 heat treat t-73;
01-398-1960
Thermal Special Purpo Insulation
Used on f-14 aircraft
01-398-2569
Aircraft Stiffener
Used on tmk10 aircraft.
01-398-2722
Structural Aircraft Panel
Used on c-130 hercules aircraft. 9.000" overall length 5.750" overall width panel-filler
01-398-3814
Structural Component Air Fitting
Used on sh60b helo mark iii.
01-398-4135
Aircraft Fairing
Used on mc-130h aircraft. 1.000" material thickness fairing-fuselage cooling provision;
01-398-4137
Aircraft Skin
Used on mc-130h aircraft. skin-fairing assy-ram air;
01-398-4186
Structural Component Air Support
01-398-4918
Aircraft Latch Assembly
Used on tmk10 aircraft.
01-398-4919
Aircraft Latch Assembly
Used on tmk10 aircraft.
01-398-4920
Aircraft Latch Assembly
Used on tmk10 aircraft.
01-398-4932
Aircraft Skin
01-398-5139
Structural Component Aircraf Web
01-398-5140
Structural Component Air Support
3.110" overall length 2.660" overall width 0.063" material thickness material:6al-4v; u/o 68A331013-1003 on f-15a CUM15, 17 & up, f-15b CUM3 & up, f-15c/d CUM1 & up, f-15e CUM1
01-398-5141
Aircraft Stiffener
9.220" overall length 4.000" overall width 0.063" material thickness material:6al-6v-2sn, MMS1203
01-398-5142
Aircraft Stiffener
18.000" overall length 2.490" overall width 1.000" material thickness
01-398-5143
Aircraft Stiffener
18.000" overall length 2.490" overall width 1.000" material thickness
01-398-5147
Aircraft Skin
01-398-5842
Aircraft Latch Assembly
Used on c-17 cargo aircraft. unit package quantity:1; component document origin:industrial; document source:88277; end item source:88277; end item name:c-17a aircraft
01-398-5853
Aircraft Skin
Used on b-52 stratofortress aircraft. PS240.000 to PS270.000; engine pylon fairing skin;
01-398-5856
Structural Component Air Bracket
01-398-5858
Structural Component Air Bracket
01-398-5859
Structural Component Air Bracket
01-398-5860
Structural Component Air Bracket
01-398-5861
Structural Component Air Bracket
01-398-5865
Aircraft Fairing
Used on mc-130h aircraft. skin-fairing assy;
01-398-5866
Aircraft Fairing
Used on mc-130h aircraft. core-fairing; fabricate per tps 2-408;
01-398-5868
Aircraft Fairing
Used on mc-130h aircraft. vane-fairing ram air; phenolic;
01-398-5904
Aircraft Stiffener
01-398-5905
Aircraft Stiffener
01-398-5972
Airfoil Rib
01-398-5973
Airfoil Rib
01-398-5974
Structural Aircraft Plate
4.950" overall length
01-398-5975
Airfoil Rib
01-398-5976
Structural Aircraft Plate
4.590" overall length
01-398-5977
Aircraft Skin
01-398-5978
Aircraft Skin
01-398-5979
Aircraft Skin
01-398-5980
Aircraft Skin
01-398-5981
Aircraft Skin
01-398-5982
Aircraft Skin
01-398-5983
Airfoil Rib
01-398-5984
Aircraft Skin
01-398-5985
Airfoil Rib
01-398-6004
Aircraft Window Panel
01-398-6011
Structural Aircraft Plate
Used on f-14dr tomcat aircraft. 0.062" material thickness pan assy-water separator;