Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-122-8637
Structural Component Air Support
Used on acft model f111. c/o pad p/n C31L6256-11, tube p/n C31L6256-13, pad p/n C31L6256-15, pad p/n C31L6256-17
01-122-8639
Structural Component Air Support
Used on acft model f111. c/o retainer p/n C31P6004-11, bracket p/n C31P6002-11
01-122-8640
Structural Component Air Support
Used on c-141 acft. matl al alloy, 7075-T651; matl size 1.000 by 9.000 by 11.000; 4.000 in. id; opposite to p/n 3F31427-104; used at fuselage station 1058
01-122-8651
Aircraft Skin
90.3000" overall length 42.000" overall width
01-122-8817
Access Aircraft Cover
Used on T-28.
01-122-8821
Aircraft Fairing
Used on f-5 aircraft.
01-122-8887
Structural Component Air Support
Manufacturer suggested name--support, flap hinge
01-122-9245
Structural Aircraft Plate
4.000" overall length 3.000" overall width 0.063" material thickness
01-122-9961
Aircraft Frame
01-123-0012
Aircraft Skin
01-123-0013
Aircraft Spar
76.600" overall length 5.800" overall width 0.108" material thickness
01-123-0014
Aircraft Spar
116.000" overall length 8.000" overall width 0.125" material thickness
01-123-0015
Aircraft Spar
116.000" overall length 8.000" overall width 0.125" material thickness
01-123-1038
Aircraft Fairing
59.700" overall length used on upper wing station 577.275
01-123-1039
Aircraft Fairing
58.700" overall length used on upper wing station 577.275
01-123-1040
Structural Component Air Support
Used on acft model t39.
01-123-1041
Structural Component Air Support
Used on acft model f111. c/o bracket p/n C31P6003-11, 2 ea. retainer p/n C31P6004-11
01-123-1042
Structural Component Air Support
Used on acft model f111. 4.000 in. lg, 1.000 in. w
01-123-2302
Attachment Molded Tank Flange
01-123-2303
Radome
01-123-2304
Radome
01-123-3115
Structural Component Air Support
Used on t-38a acft. matl hastelloy, 0.141, ams 5536g cres sheet; used as splice, stiffener, ejector cone
01-123-3118
Structural Component Air Support
Used on f-4 aircraft. sill assembly-hydraulic access door outboard fs 303.62-fs 332.50; matl-7178-o qq-a-250/15 cond o
01-123-3122
Aircraft Former
Radome contour; matl-A356-T61 M1l-a-21180c class 10 cond T61
01-123-3123
Aircraft Former
Radome contour; matl-A356-T61 mil-a-21180c class 10 cond T61
01-123-3662
Structural Component Air Support
Ksupport block; aluminum; 2.420 in. w, 2.500 in. h, 3.660 in. l, 1.528 in. min, 1.547 in. max dia hole lengthwise; 4 holes, 0.279 in. min, 0.291 in. max dia, one at each corner, 1 hole, 1.130 in. nom dia drilled thru center
01-123-3890
Structural Aircraft Panel
Used on F-16. c/o bracket, wire fabric, panel filler, 2 ea. washer, as required sealaant, primer, cleaner, adhesive, grommet, rivet, superseded p/n 16F195-3, i/c code ni, ecn 7B556, nha 16F0190-2
01-123-4351
Airframe Modification Kit
Used on uh-1 series helicopters.
01-123-5088
Rotary Rudder Boom
C/o:fin; boom; fin
01-123-6295
Aircraft Skin
01-123-6997
Structural Component Air Support
01-123-7170
Access Aircraft Cover
Used on c-141 aircraft.
01-123-7172
Access Aircraft Cover
01-123-7174
Access Aircraft Cover
Used on c-141 aircraft.
01-123-7175
Access Aircraft Cover
01-123-7176
Access Aircraft Cover
01-123-7177
Access Aircraft Cover
01-123-7178
Access Aircraft Cover
01-123-7276
Structural Component Air Fitting
Flaperon ctr hinge
01-123-7356
Fuselage Parts Kit
Used on c-141 acft. fs 734.716
01-123-7360
Structural Aircraft Panel
Matl:7079 bare: temper T6
01-123-7361
Structural Aircraft Panel
Matl:7079-T6 bare; temper T6
01-123-7382
Structural Aircraft Panel
Used on c-5a aircraft. 15.000" overall length 14.000" overall width material per STM28-003, type 2
01-123-7383
Structural Aircraft Panel
01-123-7384
Structural Aircraft Panel
Used on b-52 aircraft.
01-123-7385
Structural Aircraft Panel
Used on b-52g aircraft. consist of one core, p/n 361-10285-537
01-123-7386
Structural Aircraft Panel
Used on b-52g aircraft. consist of one core, p/n 361-10285-538
01-123-7387
Structural Aircraft Panel
Used on b-52g aircraft. consist of one core, p/n 361-10285-535
01-123-7388
Structural Aircraft Panel
C/o core 1 ea p/n 361-10285-536
01-123-7389
Structural Aircraft Panel
Used on F-111.
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