Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-361-4380
Structural Component Air Bracket
3.800" overall length 3.760" overall width 0.063" material thickness inboard leading edge rib clip
01-361-4381
Structural Component Air Bracket
3.800" overall length 3.760" overall width 0.063" material thickness inboard leading edge rib clip
01-361-4627
Access Aircraft Door
01-361-4737
Aircraft Fairing
Used on c-17a airlifter airplane.
01-361-4738
Aircraft Fairing
Used on c-17a airlifter airplane.
01-361-4739
Aircraft Strut
Used on aircraft,viking s-3a. consist of following parts, one lanyard p/n LS9981-1-1-8; two tube fillers p/n LS1669-38D48; one pin p/n NAS1333S3S03; two sleeves p/n 28-1-c
01-361-4755
Fuel Tank Parts Kit
01-361-4801
Thermal Special Purpo Insulation
01-361-4948
Aircraft Intercostal
14.300" overall length 6.200" overall width 0.063" material thickness heat treated to 2024-T62; used on next assy 68A111232-1003 on the f-15e cum 6-44
01-361-4949
Aircraft Intercostal
14.300" overall length 6.200" overall width 0.063" material thickness heat treated to 2024-T62; used on next assy 68A111232-1004 on the f-15e cum 6-44
01-361-4950
Aircraft Intercostal
14.300" overall length 6.230" overall width 0.063" material thickness heat treated to 2024-T62; used on next assy 68A111232-1003 on the f-15e cum 45
01-361-4951
Aircraft Intercostal
14.300" overall length 6.230" overall width 0.063" material thickness heat treated to 2024-T62; used on next assy 68A111232-1004 on the f-15e cum 45
01-361-4952
Structural Component Air Bracket
4.000" overall length 1.900" overall width 0.063" material thickness heat treated to 2024-T81
01-361-5118
Structural Component Air Support
3.650" overall length support for c-130 glareshield
01-361-5119
Structural Component Air Support
Used on b-2 bomber.
01-361-5198
Thermal Special Purpo Insulation
Aircraft, airlifter c-17a
01-361-5757
Structural Aircraft Panel
Panel assembly, aileron actuating bay wing, lh
01-361-5758
Structural Aircraft Panel
Panel assembly, aileron actuating bay wing; rh
01-361-5886
Structural Component Air Support
Used on helicopter observation (ahip),oh-58d.
01-361-5887
Structural Component Air Support
01-361-5888
Structural Component Air Fitting
Used on helicopter observation (ahip),oh-58d.
01-361-6075
Airfoil Rib
11.680" overall length 6.760" overall width 0.063" material thickness
01-361-6076
Aircraft Fairing
9.900" overall length 1.800" overall width 0.063" material thickness nuclear hardness critical item, opposite -002, part of outlet door seal, matl: 15-5ph sht, per BMS7-240, type 1, solution treated, heat treat 150-170 ksi per BAC5619
01-361-6077
Aircraft Fairing
9.900" overall length 1.800" overall width 0.063" material thickness nuclear hardness critical item, opp -001, part of outlet door seal, material: 15-5ph sht, per bms 7-240, type 1, solution treated, heat treat 150-170 ksi per bac 5619
01-361-6078
Aircraft Fairing
8.600" overall length 1.800" overall width 0.063" material thickness nuclear hardness critical item, opp -004, part of outlet door seal, material: 15-5ph sht, per bms 7-240, type 1, solution treated, heat treat 150-170 ksi per bac 5619
01-361-6079
Aircraft Fairing
6.300" overall length 1.800" overall width 0.063" material thickness nuclear hardness critical item, opp -006, part of outlet door seal, material: 15-5ph sht, per bms 7-240, type 1, solution treated, heat treat 150-170 ksi per bac 5619
01-361-6080
Aircraft Fairing
6.300" overall length 1.800" overall width 0.063" material thickness make from 15-5ph sht; opposite -005; nuclear hardness critical item
01-361-6082
Aircraft Fairing
6.300" overall length 1.800" overall width 0.063" material thickness make from 15-5ph sht; opposite -010; nuclear hardness critical item
01-361-6083
Aircraft Fairing
6.300" overall length 1.800" overall width 0.063" material thickness make from 15-5ph sht; opposite -009; nuclear hardness critical item
01-361-6084
Aircraft Fairing
6.200" overall length 1.800" overall width 0.063" material thickness nuclear hardness critical item, opp -011, part of outlet door seal, material: 15-5ph sht, per bms 7-240, type 1, solution treated, heat treat 150-170 ksi per bac 5619
01-361-6697
Structural Aircraft Plate
01-361-6698
Structural Aircraft Plate
01-361-7177
Access Aircraft Cover
Used on b-2 pacer special. access panel assy; sta 221.5
01-361-7295
Structural Aircraft Plate
Sci-smoothness critical item
01-361-7296
Structural Aircraft Plate
Sci-smoohtness critical item
01-361-7297
Structural Aircraft Plate
Sci-smoothness critical item
01-361-7298
Structural Aircraft Plate
5.570" overall length anodize surface treated
01-361-7299
Structural Aircraft Plate
5.570" overall length anodize surface treated
01-361-7300
Structural Aircraft Plate
6.820" overall length anodize surface treated
01-361-7301
Structural Aircraft Plate
6.820" overall length anodize surface treated
01-361-7302
Structural Aircraft Plate
6.820" overall length anodize surface treated
01-361-7303
Structural Aircraft Plate
6.820" overall length anodize surface treated
01-361-7304
Structural Aircraft Plate
7.050" overall length 2.500" overall width 0.050" material thickness heat treated to 2024-T62
01-361-7305
Structural Aircraft Plate
7.050" overall length 2.500" overall width 0.050" material thickness heat treated to 2024-T62
01-361-7306
Structural Aircraft Plate
4.750" overall length 2.500" overall width 0.050" material thickness heat treated to 2024-T62
01-361-7307
Structural Aircraft Plate
4.750" overall length 2.500" overall width 0.050" material thickness heat treated to 2024-T62
01-361-7308
Structural Aircraft Plate
Used on helicopter observation (ahip),oh-58d. 8.580" overall length
01-361-7309
Stiffener Aircraft Rib
16.420" overall length 8.480" overall width 4.000" material thickness nha 68A111239
01-361-7310
Stiffener Aircraft Rib
16.420" overall length 8.480" overall width 4.000" material thickness nha 68A111239
01-361-7311
Stiffener Aircraft Rib
16.420" overall length 8.480" overall width 4.000" material thickness nha 68A111239