Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-257-6878
Thermal Special Purpo Insulation
Acft model b-1b
01-257-7109
Structural Aircraft Plate
Used on KC-135. 95.000" overall length 5.000" overall width 0.040" material thickness finish f-2.115, ht tr T4
01-257-7110
Structural Component Air Support
Used on c-5b aircraft. fitting-attachment, slat actuator door; nha 4J11203 & 4J11209
01-257-7111
Structural Component Air Fitting
Nha 4J11209
01-257-7112
Structural Component Air Support
Used on c-5b aircraft. fitting-attachment, slat actuator door; nha 4J11203 & 4J11205
01-257-7113
Structural Component Air Support
Used on c-5b aircraft. fitting-attachment, slat actuator door; nha 4J11207
01-257-7114
Structural Component Air Support
Used on t-38 aircraft. fitting, attach-main spar, wing; c/o: -101 fitting (1) , bushing (1)
01-257-7115
Structural Component Air Support
Used on t-38 aircraft. fitting, attach-main spar, wing; c/o: -201 fitting (1) , bushing (1)
01-257-7116
Structural Component Air Support
Used on acft model kc-135. make from 9-60302; finish f-2.30; opposite p/n -2; nha 5-86060; located on wing station 466.36
01-257-7117
Structural Component Air Support
Used on acft model kc-135. make from 9-60302; finish f-2.30; opposite p/n -1; nha 5-86060; located on wing station 466.36
01-257-7118
Structural Component Air Support
Used on acft model b-1b.
01-257-7120
Aircraft Floor
01-257-7121
Structural Aircraft Panel
Used on e-3 airplane....
01-257-7122
Structural Aircraft Panel
Used on acft model kc-135. finish f-2.21 plus srf-12.205 plus f-12.353; opposite p/n -3072; -43 optional for spares only
01-257-7123
Structural Aircraft Panel
Used on acft model b-1b.
01-257-7124
Wing Aircraft Spoiler
C/o 2 track, 1 spoiler, 1 cam, 2 bar, misc hardware; nha L3054450; opposite -011
01-257-7134
Aircraft Former
9.800" overall length 2.600" overall width 0.050" material thickness
01-257-7135
Aircraft Former
01-257-7138
Horizontal Stabilizer
C/o 1 stab assy, 1 removable l.e.assy, 1 lh control instl, 1 lh electrical instl; opposite -8; nha 50-8286
01-257-8555
Fuselage Aircraft Fairing
01-257-8556
Fuselage Aircraft Fairing
01-257-8572
Aircraft Window Panel
01-257-9274
Structural Aircraft Panel
Used on pacer special. smoothness critical item; c/o: bracket, door assy, shims, fitting assys, bolts, washers, nuts, & pins
01-257-9282
Access Aircraft Door
Access-relay panel anodize surface treated
01-257-9340
Structural Aircraft Panel
Smoothness critical item; c/o: door assys, shims, fitting assys, duct assy, spacer, bracket, washers, bolts, nuts, pins, & bushings
01-257-9341
Structural Aircraft Panel
Used on pacer special. smoothness critical item; c/o: door assy, fitting assys, shims, bracket, bolts, washers, nuts, pins, rivets, & bushing
01-257-9342
Structural Aircraft Panel
Smoothness critical item; c/o: fitting assys, shims, bracket, washers, bolts, pins, rivets, nuts, & bushing
01-257-9351
Structural Aircraft Plate
Used on F-15.
01-257-9352
Structural Aircraft Plate
Used on F-15.
01-257-9353
Structural Aircraft Plate
Used on F-15.
01-257-9367
Structural Aircraft Plate
Used on F-15. splice
01-257-9368
Structural Aircraft Plate
Used on F-15.
01-257-9369
Structural Aircraft Plate
Used on F-15. cond 0 alclad; web
01-257-9371
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9047e comp 6; fitting, long spar vertical forward
01-257-9373
Structural Component Air Support
01-257-9375
Structural Component Air Support
Used on acft model h-53. consist of 1 pin, 1 fitting; nha 7459400
01-257-9377
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9047e; fitting-long spar, vertical aft
01-257-9378
Structural Component Air Support
Used on f-15 acft. support-door arresting hook
01-257-9379
Structural Component Air Support
Used on f-15 acft. support-door arresting hook
01-257-9381
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9047e; fitting-long spar vertical aft
01-257-9405
Aircraft Former
Used on H-53. cond 0; p/o radar mount structure
01-257-9406
Aircraft Former
Used on H-53. p/o radar mount structure
01-257-9415
Aircraft Leading Edge
01-257-9417
Airfoil Rib
44.000" overall length 8.000" overall width 0.032" material thickness heat treat T42; finish f-19; opposite 345198l
01-257-9418
Airfoil Rib
Used on C-130. consist of 1 former, 1 stiffener; nha 342328
01-257-9419
Airfoil Rib
Used on C-130.
01-257-9420
Aircraft Skin
Used on F-15. cond 0
01-257-9421
Aircraft Skin
Used on F-15. cond 0
01-257-9730
Access Aircraft Door
01-257-9733
Fuselage Aircraft Fairing
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