Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-488-7329
Structural Component Air Support
Used on f/a-22 raptor. 11.260" overall length support details-ivsc A3
01-488-7332
Structural Component Air Bracket
Used on f/a-22 raptor. 1.870" overall length 1.720" overall width
01-488-7333
Structural Component Air Support
Used on f/a-22 raptor. angle
01-488-7334
Structural Component Air Support
Used on f/a-22 raptor.
01-488-7335
Structural Component Air Bracket
Used on f-22 raptor. 3.000" overall length 3.000" overall width 0.050" material thickness bracket-amad bay, assembly of
01-488-7336
Structural Component Air Support
Used on f-22 raptor. angle - bond part opposite 5HW82332-120
01-488-7337
Aircraft Arresting Hook Arm
Used on f-22 raptor. 4.000" overall length arm dim. are stock material; AMS5629, PH13-8mo soln treated stainless steel bar
01-488-7338
Structural Component Air Support
Used on f/a-22 raptor. angle-bond part, fairing attach, wing joint
01-488-7339
Structural Component Air Support
Used on f/a-22 raptor. angle-bond part, fairing attach, wing joint
01-488-7340
Structural Component Air Support
Used on f-22 raptor. angle - bond part opposite -104
01-488-7342
Structural Component Air Support
Used on f/a-22 raptor. angle matl p
01-488-7343
Structural Component Air Support
Used on f-22 raptor. angle opposite -129; bmi composite material
01-488-7345
Structural Component Air Support
Used on f/a-22 raptor.
01-488-7346
Structural Component Air Support
Used on f-22 raptor. angle, bond part opposite 5HW82332-131
01-488-7351
Structural Component Air Bracket
Used on f/a-22 raptor.
01-488-7352
Structural Component Air Bracket
Used on f/a-22 raptor. 6.000" overall length 4.000" overall width bracket ann 6al-4v (ab-1) sheet
01-488-7409
Structural Aircraft Plate
21.000" overall length 3.000" overall width 0.180" material thickness dimensions are stocksize; manf. suggested name (strl pl-filler) ; strength T6; nha -2; eff. type a from 7 thruon
01-488-7410
Structural Aircraft Plate
22.000" overall length 4.000" overall width 0.125" material thickness strength T6; dimensions are stocksize; manf. suggested name (strl pl-rpr) ; nha -2; eff. type a from 7 thru on
01-488-7411
Structural Aircraft Plate
0.900" overall length 0.700" overall width 0.300" material thickness strength T351; dimensions are stocksize; manufactured suggested name (shim) ; nha -2
01-488-7412
Structural Aircraft Plate
21.000" overall length 5.000" overall width 0.125" material thickness strength T6; effectivity type a from 7 thru on; manf. suggested name (strl pl-rpr) ; dimensions are stocksize; nha -2
01-488-7525
Structural Component Air Support
6.700" overall length 2.070" overall width 1.120" material thickness foam block unicellular felxible foam; nha 68A321451; u/o f-15c CUM15c 151-239, 240&up, f-15d CUM26-39, 40&up, f-15e CUM1-209, 210&up, f-15i, s CUM1&up
01-488-7526
Structural Component Air Support
4.700" overall length 2.070" overall width 1.120" material thickness foam block unicellular flexible foam; nha 68A321451; u/o f-15c CUM151&up, f-15d CUM26&up, f-15e CUM1-209, 210&up, f-15i CUM1&up, f-15s CUM1-12, 13&up
01-488-7528
Structural Component Air Support
6.250" overall length 3.650" overall width 1.880" material thickness honeycomb block nha 68A321451; u/o f-15c, d, j CUM1&up
01-488-7529
Structural Component Air Support
6.250" overall length 3.650" overall width 1.880" material thickness honeycomb block next higher assy, 68A321451, u/o f-15c, d, dj, j cum 1
01-488-7530
Structural Component Air Support
3.800" overall length 3.400" overall width 2.700" material thickness next higher assembly, u/o f-15c cum 151
01-488-7532
Structural Component Air Support
6.000" overall length 2.400" overall width 0.040" material thickness next higher assy, 68A321451, u/o f-15c cum 151
01-488-7533
Structural Component Air Support
6.750" overall length 0.075" overall width 0.035" material thickness next higher assy, 68A321451, u/o f-15c cum 1-150, f-15d cum 1-25, f-15dj cum 1-4, f-15j cum 1
01-488-7534
Structural Component Air Support
6.350" overall length 1.750" overall width 0.500" material thickness honeycomb block nha 68A321451; u/o f-15c, d, j CUM1&up
01-488-7535
Structural Component Air Support
6.000" overall length 2.400" overall width 0.400" material thickness nha 68A321451; unicellular flexible foam; u/o f-15c CUM151&up, f-15d CUM26&up, f-15e CUM1-209, 210&up, f-15i, s CUM1&up
01-488-7536
Structural Component Air Support
6.700" overall length 2.070" overall width 1.120" material thickness unicellular fexible foam; nha 68A321451; u/o f-15c CUM151-239&up, f-15d CUM26-40&up, f-15e CUM1-209, 210&up, f-1i, s CUM1&up
01-488-7537
Structural Component Air Support
5.900" overall length 5.370" overall width 3.090" material thickness next higher assy, 68A321451, u/o f-15c cum 151
01-488-7538
Structural Component Air Support
5.900" overall length 5.370" overall width 3.090" material thickness next higher assy, 68A321451 u/o f-15c cum 151
01-488-7539
Exhaust Aircraft Lip
01-488-7619
Structural Component Air Support
Used on F-22.
01-488-7801
Aircraft Former
0.071 sheet thickness; material 7000075-T6 alclad
01-488-8046
Structural Component Air Bracket
Used on f-22 raptor. bracket assembly
01-488-8053
Structural Component Air Support
Used on f/a-22 raptor. bracket, support-fuel line
01-488-8095
Bleed Air Duct Assembly
Used on f/a-22 raptor. duct- bleed air conditioned
01-488-8101
Bleed Air Duct Assembly
Used on f/a-22 raptor. duct-bleed air conditioned
01-488-8104
Bleed Air Duct Assembly
Used on f/a-22 raptor. duct- bleed air conditioning assy of
01-488-8322
Aircraft Latch Assembly
Used on f/a-22 raptor. 1.575" overall length 1.100" overall width 6100 series self-adjusting spring head is plastic knob; dimensions include the under-panel/mount
01-488-8419
Aircraft Tip
Used on c130j aircraft. tip assy, vertical stabilizer
01-488-8466
Structural Aircraft Plate
Used on b1-b aircraft. 6.300" overall length 2.500" overall width panel, liner-outboard fore/aft bunk
01-488-8651
Structural Component Aircraf Web
01-488-8944
Bleed Air Duct Assembly
Used on F-22. duct bleed air-conditioning ecs bay mdl 3, assy of f-22 raptor
01-488-8965
Longeron
01-488-8984
Structural Component Air Bracket
01-488-9037
Structural Aircraft Plate
Used on f/a-22 raptor. 5.000" overall length 5.000" overall width cover plate dim. are stock material; wind swept surface critical
01-488-9155
Aircraft Door
01-488-9172
Structural Component Air Support
6.350" overall length 1.750" overall width 0.500" material thickness honeycomb block nha 68A321451; u/o f-15c, d, j CUM1&up