Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-076-9044
Aircraft Pylon
01-077-1224
Structural Component Air Bracket
01-077-1297
Structural Aircraft Plate
4.000" overall length 2.000" overall width 0.016" material thickness 17-7 ph; u-shape, used in centerbody spike assembly
01-077-1308
Structural Component Air Fitting
01-077-1314
Aircraft Rudder
01-077-2133
Aircraft Stiffener
30.300" overall length 2.400" overall width 0.025" material thickness finish f-8.05
01-077-2186
Structural Component Air Fitting
U/a: fitting, wing splice; matl: form forging 160D611606f; finished wt not to exceed 11.2 pounds; anodize sulphuric acid corr preventive coat per: mil-a-8625, type ii, CL1; penetrant inspect mil-t-6866; alum ht:mil-h-6088
01-077-2198
Aircraft Fairing
17.100" overall length 4.500" overall width 0.071" material thickness le flap lwr seal 5323
01-077-2200
Aircraft Fairing
Used on F-16. 28.000" overall length 5.000" overall width 0.071" material thickness
01-077-2209
Aircraft Skin
Used on acft c135. structure installation, 39.000 in lg, 33.000 in w, 0.060 in th. plastic glass fabric laminated per bac 5449 style 181 fabric 6 plys. finish f-6.10 inside surface only
01-077-2693
Access Aircraft Cover
01-077-3367
Trim Aircraft Tab
Nuclear hardness critical item
01-077-3368
Trim Aircraft Tab
01-077-3375
Aircraft Fairing
27.000" overall length 5.000" overall width 0.025" material thickness
01-077-4198
Structural Aircraft Plate
Used on acft model no. c-5a. aluminum 2024-T3, qq-a-250/4, 6.000 in. lg, 1.000 in. w, 0.063 in. thk
01-077-4248
Airfoil Rib
Used on a-7 airplane. 11.100" overall length 5.400" overall width 0.032" material thickness
01-077-4249
Airfoil Rib
Used on a-7 corsair airplane. 11.400" overall length 5.500" overall width 0.032" material thickness
01-077-4250
Airfoil Rib
11.800" overall length 4.800" overall width 0.032" material thickness
01-077-6052
Access Aircraft Door
Iff system access
01-077-6637
Structural Aircraft Plate
2.800" overall length 2.600" overall width 0.090" material thickness
01-077-6638
Structural Component Air Fitting
2.600" overall length 2.600" overall width 1.800 " material thickness
01-077-6639
Structural Aircraft Plate
2.400" overall length 2.400" overall width 0.090" material thickness
01-077-6640
Structural Aircraft Plate
2.700" overall length 2.400" overall width 0.090" material thickness
01-077-6713
Airfoil Rib
Used on a-7 airplane.... 7.700" overall length 5.200" overall width 0.070" material thickness matt; clad
01-077-6714
Airfoil Rib
13.200" overall length 5.800" overall width 0.025" material thickness
01-077-6902
Aircraft Leading Edge
Used on aircraft model a-7e.
01-077-6903
Aircraft Leading Edge
Used on acft model a-7e.
01-077-7325
Structural Aircraft Plate
01-077-7372
Fuel Tank Aircraft Baffle
01-077-7403
Airfoil Rib
10.100" overall length 4.700" overall width 0.032" material thickness
01-077-7404
Airfoil Rib
13.500" overall length 5.800" overall width 0.025" material thickness
01-077-7405
Airfoil Rib
Used on a-7 intruder airplane.... 12.900" overall length 5.600" overall width 0.025" material thickness
01-077-7407
Airfoil Rib
01-077-7408
Airfoil Rib
Used on aircraft,model a-7. 6.900" overall length 3.700" overall width 0.040" material thickness
01-077-7412
Airfoil Rib
Used on a-7 airplane.... 8.600" overall length 4.300" overall width 0.032" material thickness
01-077-7413
Airfoil Rib
9.600" overall length 3.900" overall width 0.050" material thickness
01-077-7414
Airfoil Rib
9.600" overall length 3.900" overall width 0.050" material thickness
01-077-7419
Aircraft Skin
Used on acft c135. lefthand forward, cowl panel. 26.000 in. lg, 9.800 in. w, 0.032 in. th. commercially pure titanium sht ams 4900, annealed. finish f-10.10
01-077-7420
Aircraft Tip
Used on acft a7. lefthand, outer panel installation
01-077-8034
Structural Aircraft Plate
3.900" overall length 2.600" overall width 0.090" material thickness
01-077-8035
Structural Component Air Fitting
01-077-8036
Structural Aircraft Plate
3.600" overall length 3.300" overall width 0.080" material thickness
01-077-8037
Structural Aircraft Plate
3.600" overall length 3.300" overall width 0.080" material thickness
01-077-8038
Structural Aircraft Plate
4.500" overall length 1.500" overall width 0.090" material thickness
01-077-8039
Structural Aircraft Plate
4.000" overall length 3.500" overall width 0.100" material thickness
01-077-8040
Structural Aircraft Plate
4.500" overall length 3.500" overall width 0.100" material thickness
01-077-8041
Structural Aircraft Plate
3.500" overall length 2.500" overall width 0.100" material thickness
01-077-8042
Structural Aircraft Plate
3.500" overall length 2.500" overall width 0.100" material thickness
01-077-8043
Aircraft Slat
01-077-8044
Aircraft Slat
Page: 536 ...