Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-208-3247
Thermal Special Purpo Insulation
01-208-3248
Thermal Special Purpo Insulation
01-208-3937
Movable Canopy
01-208-4183
Structural Aircraft Plate
01-208-4184
Structural Aircraft Plate
01-208-4185
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, to; 0.040 in. matl thk by 3.000 in. w by 28.000 in. lg; l cross section; prebent; right appl; w/o rivet holes
01-208-4186
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11; 2.560 in. lg; 1.100 in. w; 1.050 in. h; w/o holes; upper right position
01-208-4187
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, to; 0.040 in. matl thk by 8.500 in. w by 34.000 in. lg; bow shape; channel cross section; w/o rivet holes; left
01-208-4188
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, to; 0.040 in. matl thk by 8.500 in. w by 34.000 in. lg; bow shape; channel cross section; right appl; w/o rivet holes
01-208-4191
Aircraft Floor
Used on 1520-00-859-2670. component qty 15, mfr parts list 205-031-332; left appl; w/o attaching rivet holes
01-208-4192
Aircraft Floor
01-208-4193
Aircraft Floor
01-208-4194
Fuselage Stringer
Used on 1520-00-859-2670. 92.500" overall length 6.500" overall width 0.032" material thickness l cross section; 15 lightening holes; w/o rivet holes; left hand design
01-208-4195
Fuselage Stringer
Used on 1520-00-859-2670. 10.000" overall length 2.600" overall width 0.040" material thickness angle cross section; w/o holes
01-208-4418
Longeron
Used on F-15.
01-208-4420
Aircraft Skin
Used on acft model b-1b. al alloy clad sheet 2024-0 per qq-a-250/5; stock size 11.000 in. lg, 10.500 in. w, 0.080 thk; nha L3226009; opposite p/n -004
01-208-4421
Aircraft Skin
Used on acft model b-1b. al alloy clad sheet 2024-0 per qq-a-250/5; stock size 11.000 in. lg, 10.500 in. w, 0.080 thk; nha L3226009; opposite p/n -003
01-208-4422
Aircraft Skin
Used on acft model b-1b. al alloy clad sheet 2024-0 per qq-a-250/5; stock size 9.500 in. lg, 2.500 in. w, 0.080 in. thk; nha L3226009
01-208-4423
Aircraft Skin
Used on acft model b-1b. corrosion resistant steel sheet comp 321, cond a; c/o 1 closeout
01-208-4424
Aircraft Skin
Used on acft model b-1b. corrosion resistant steel sheet comp 321, cond a per qq-s-766; stock size 9.000 in. lg, 3.50 in. w, 0.080 in. thk; opposite p/n -008; nha L3226900
01-208-4425
Aircraft Skin
Used on acft model b-1b. corrosion resistant steel sheet comp 321, cond a per qq-s-766; stock size 9.00 in. lg, 3.50 in. w, 0.080 in. thk; opposite p/n -007; nha L3226900
01-208-4434
Thermal Special Purpo Insulation
01-208-7811
Aircraft Pylon
01-208-8376
Air Wing Fairing Inflatable Seal
Matl: cordura fabric-nylon outer material with a thin rubber backing
01-208-8446
Structural Aircraft Plate
8.000" overall length 3.500" overall width 0.160" material thickness nuclear hardness critical item
01-208-8447
Structural Aircraft Plate
01-208-8448
Structural Aircraft Plate
01-208-8449
Structural Component Air Support
Used on acft model b-1b. consist of 1 fitting, 2 plate, 4 nut, rivet a/r; nha L3223628; opposite p/n -002
01-208-8450
Structural Component Air Support
Used on acft model b-1b. consist of 1 al alloy tee, 1 bearing; opposite p/n -002; nha L3223750
01-208-8451
Structural Component Air Support
Used on acft model b-1b. 2024-T8511 al alloy per qq-a-200/3; shape AND10136-1202 by 10.75 in. long; finish 10AB02
01-208-8452
Structural Component Air Support
Used on acft model b-1b. al alloy shape, 2024-T62 per qq-a-250/5; finish 11AB02; shape LS033-0018 by 9.500 in. lg; nha L3223771-001
01-208-8453
Structural Component Air Support
Used on acft model b-1b. al alloy 2024-T4 shape; LS043-0791 by 26.400 in. lg; finish 10AB01; opposite p/n -010; nha L3203627-101
01-208-8454
Structural Component Air Support
Used on acft model b-1b. consist of 1 fitting, 2 plate, 4 nut, rivet a/r; nha L3223628; opposite p/n -001
01-208-8455
Structural Component Air Support
Used on acft model b-1b. consist of 1 al alloy tee, 1 bearing; opposite p/n -001; nha L3223750
01-208-8456
Structural Component Air Support
01-208-8457
Structural Component Air Support
Aircraft structural support component
01-208-8458
Structural Component Air Support
Used on acft model b-1b. corrosion resistant steel bar PH13-8mo, cond a, per ST0160LB0013; c/o 2 plates; 4.120 in. lg, 1.500 in. o/a w, 0.912 in. o/a thk; opposite p/n -022; nha L3226401
01-208-8459
Structural Component Air Support
Used on acft model b-1b. corrosion resistant steel PH13-3mo, cond a, ST0160LB0013; c/o 2 plates; opposite p/n -032; nha L3226401
01-208-8460
Structural Component Air Support
Used on acft model b-1b. al alloy shape 2024-T8511; shape LS043-0968; c/o 1 tee, 1 bearing; install bearing per ST0101LA0004, class ii; finish 10ac; opposite p/n -002; nha L3223750
01-208-8461
Structural Component Air Support
Used on acft model b-1b. al alloy shape 2024-T8511; shape LS043-0968; c/o 1 tee, 1 bearing; install bearing per ST0101LA0004, class ii; finish 10ac; opposite p/n -001; nha L3223750
01-208-8462
Structural Component Air Support
Used on f-15 acft. p/o former-sidepanel; fuselage station 651.060
01-208-8463
Structural Component Air Support
Used on f-15 acft. p/o former-sidepanel; fuselage station 651.060
01-208-8464
Structural Component Air Support
Used on f-15 acft. p/o former-sidepanel; fuselage station 651.060
01-208-8465
Structural Component Air Support
Used on f-15 acft. p/o former-side panel; fuselage station 651.060
01-208-8466
Structural Component Air Support
Used on f-15 acft. p/o former-sidepanel; fuselage station 651.060
01-208-8467
Structural Component Air Support
Used on f-15 acft. p/o former side panel; fuselage station 651.060
01-208-8468
Structural Component Air Support
Used on f-15 acft. p/o outboard-forward, engine upper nozzle fairing
01-208-8475
Structural Aircraft Panel
01-208-8476
Structural Aircraft Panel
Used on acft model b-1b. glass/epoxy prepreg per ST0130LB0010; located yn 87.20 to 53.75; nha L3226009
01-208-8478
Structural Aircraft Panel
Used on acft model b-1b. consist of 2 facesheet, 1 retainer, 1 batt blanket, 1 plate; nha L3207353; located at YAN2.453
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