Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-375-6920
Structural Aircraft Plate
Used on uh-1n helicopter. 6.690" overall length 5.870" overall width 0.088" material thickness right hand flange-ammo chute
01-375-6921
Structural Aircraft Plate
Used on aircraft uh-1n. 8.500" overall length 8.500" overall width 0.040" material thickness aluminum surface treated
01-375-6922
Structural Component Air Bracket
Used on aircraft a-4. 10.000" overall length 2.000" overall width aluminum surface treated
01-375-7259
Structural Aircraft Panel
Used on pacer special. smoothness critical item, used aslower actr acs panel
01-375-7263
Structural Component Air Bracket
P/o 35-8275 lower inbd by-pass duct, used as a clip
01-375-7264
Structural Component Air Bracket
3.300" overall length 1.800" overall width 0.063" material thickness ht T4, temper 0, u/a an angle
01-375-7443
Access Aircraft Door
Used on b-2 pacer special. smoothness critical item; p/o: door no.3, access le support struct bond assy; c/o: bond assy, nameplate, & grommets
01-375-7444
Access Aircraft Door
Used on b-2 pacer special. smoothness critical item; manufacturer suggested name: door assy-is le support; c/o: bond assy & grommets
01-375-7445
Access Aircraft Door
Used on b-2 pacer special. c/o bond assy, 1 nameplate, 30 grommet; effectivity 0998-0998, 1003-9999; nha DAA3121B011-268; used as le supportstructure bond assembly no 3 access door
01-375-7446
Access Aircraft Door
Used on b-2 pacer special. smothness critical item; manufacturer suggested name: door assy-is le support
01-375-7463
Aircraft Former
12.000" overall length used as:upper angle seal, ht T42, temper 0, opposite -515
01-375-7465
Aircraft Fairing
Nuclear hardness critical item, u/a: air refueling receptacle fairing, c/o upper & lower scuff plates, canopyharness/light assy, backup plate assy, canopy, misc hardware
01-375-7468
Aircraft Skin
37.500" overall length 6.900" overall width skin, aircraft-FS589.000 to FS595.800, lower longeron BL15.400; part of 68A324717-1010 on nha 68A324000
01-375-7469
Structural Component Air Support
12.500" overall length 2.800" overall width 0.050" material thickness bracket, angle
01-375-8701
Structural Aircraft Panel
Critical fit, tolerance,
01-375-8702
Structural Aircraft Panel
C/o 1 seal instl, 1 insulation, 50 washer, 50 retainer, 50 sleevebolt; critical fit, tolerance
01-375-8703
Structural Aircraft Panel
C/o 1 seal instl, 1 insulation, 58 washer, 58 retainer, 58 sleevebolt; critical fit, tolerance
01-375-8704
Structural Aircraft Panel
Used on B-2. critical fit/tolerances
01-375-8705
Structural Aircraft Panel
C/o 1 insulation, 30 washer, 30 retainer, 30 sleevebolt; nha DAA3118A302; eff R0017-R0999; critical fit, tolerances
01-375-8706
Structural Aircraft Panel
Used on B-2. critical fit, tolerance,
01-375-8707
Structural Aircraft Panel
Critical fit, tolerances
01-375-8709
Aircraft Frame
01-375-9699
Aircraft Stiffener
01-375-9703
Aircraft Strut
01-375-9706
Aircraft Channel
01-375-9707
Aircraft Channel
01-375-9739
Thermal Special Purpo Insulation
01-375-9925
Aircraft Boom
Used on aircraft model uh-1n.
01-375-9926
Airfoil Rib
18.500" overall length 5.800" overall width 0.080" material thickness
01-375-9932
Aircraft Skin
01-375-9933
Structural Component Air Fitting
Used on e2 acft.
01-375-9934
Structural Component Aircraf Web
Used on hercules aircraft.
01-376-0214
Aircraft Stiffener
01-376-0215
Aircraft Stiffener
01-376-0216
Aircraft Stiffener
01-376-0217
Aircraft Stiffener
01-376-0249
Structural Component Aircraf Web
Used on hercules aircraft.
01-376-0250
Structural Component Aircraf Web
Used on hercules aircraft.
01-376-0251
Structural Component Aircraf Web
Used on hercules aircraft.
01-376-1013
Structural Aircraft Panel
C/o 1 seal instl, 1 insulation, 3 stiffener, 53 washer, 21 collar, 21 lockbolt, 53 retainer, 53 sleevebolt; nuclear hardness critical
01-376-1014
Structural Aircraft Panel
C/o 1 insulation, 46 washer, 46 retainer, 46 sleevebolt; nuclear hardness; nha DAA3118A302; eff R0017-R0999
01-376-1576
Aircraft Frame
01-376-1577
Airfoil Rib
Used on c-130 aircraft.
01-376-1578
Stiffener Aircraft Rib
Used on c-130 aircraft.
01-376-1579
Aircraft Stiffener
13.300" overall length structrual tee
01-376-1580
Structural Aircraft Plate
18.000" overall length 2.000" overall width 0.020" material thickness AISI301, mil-s-5059, opposite -1, used as a director ring seal
01-376-1581
Structural Aircraft Panel
Used on e-3 awacs airplane....
01-376-1583
Structural Component Air Support
Used on c-130 aircraft.
01-376-1584
Structural Component Air Support
Used on c-130 aircraft.
01-376-1585
Structural Component Air Fitting