Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-134-4576
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-362, 2024-0 clad; part of seal assy p/n 3P61599-101; used on lh pylon on station 100.00 bulkhead as achannel
01-134-4577
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-362, 2024-0 clad; part of seal assy, left hand pylon station 100.00 bulkhead; used as angle
01-134-4578
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-362, 2024-0 clad; used as angle as part of seal assy, lh pylon station 100.00 bulkhead
01-134-4579
Structural Component Air Support
5.000" overall length 3.000" overall width 0.050" material thickness u/a:angle; temper 0
01-134-4580
Structural Component Air Support
5.000" overall length 2.000" overall width 0.040" material thickness u/a: angle; temper 0
01-134-4581
Structural Component Air Support
5.000" overall length 1.000" overall width 0.020" material thickness u/a: angle; temper o
01-134-4582
Structural Component Air Bracket
Matl: cond n normalized
01-134-4585
Exhaust Pipe
Used on f-16a falcon aircraft. duct, exhaust jet fuel starter; titanium
01-134-4600
Wing Landing Flap
Used on acft model a7. left hand inboard leading edge landing flap assembly
01-134-4601
Wing Landing Flap
Used on acft model a7. right hand inboard leading edge landing flap assembly
01-134-4602
Aircraft Former
C/o angle p/n 160D611521-25, 14 ea. p/n CCR264SS3-1, 2 ea. plate nut p/n MS21075L3, 5 ea. plate nut S987DC3-3
01-134-4603
Structural Component Air Support
Angle assembly c/o angle p/n 160D611521-26, 14 ea. p/n CCR264SS3-1, 2 ea. plate nut p/n MS21075L3, 5 ea. plate nut p/n S987DC3-3
01-134-4604
Aircraft Former
C/o angle p/n 160D611521-99, 14 ea. rivet p/n CCR264SS3-1, 2 ea. plate nut p/n MS21075L3, 5 ea. plate nut p/n S987DC3-3
01-134-4605
Aircraft Former
C/o angle p/n 160D611521-100, 14 ea. p/n CCR264SS3-1, 2 ea. plate nut p/n MS21075L3, 5 ea. plate nut p/n S987DC3-3
01-134-4606
Aircraft Former
01-134-4607
Aircraft Former
01-134-4608
Aircraft Former
01-134-4610
Aircraft Pylon
01-134-4611
Aircraft Pylon
01-134-4612
Aircraft Pylon
01-134-4614
Aircraft Skin
Used on acft model c135. al alloy sheet 2024-0 clad per qq-a-362, heat treat to condition T4; 0.040 in. thk; used on forward portion of left hand outboard main landing gear door
01-134-4615
Aircraft Skin
Used on F-111.
01-134-5449
Fluid Aircraft Manifold
01-134-6120
Structural Aircraft Panel
01-134-6347
Structural Component Air Fitting
01-134-6352
Structural Component Air Fitting
01-134-6353
Structural Component Air Bracket
01-134-6354
Structural Component Air Bracket
01-134-6355
Aircraft Stiffener
01-134-6356
Aircraft Stiffener
U/a: stiffener, panel
01-134-6369
Structural Aircraft Panel
Used on c-135 aircraft. 18.000" overall length 10.500" overall width royalite sheet; 60 serieds hardness
01-134-6370
Structural Aircraft Plate
5.180" overall length 3.690" overall width matl st, AMS6359, 4340 annealed; eighteen holes, 0.190 in. dia; 0.250 in. dia hole
01-134-6371
Structural Component Air Support
Used on acft model c135. used as rear spar flap track support
01-134-6372
Structural Component Air Support
01-134-6374
Structural Component Air Support
Used on ct/t-39 aircraft.
01-134-6378
Structural Component Air Support
Used on ct/t-39 aircraft. location-pylon, rh, fus sta 368; material-302 cres sht per mil-s-5059, anl
01-134-6379
Structural Component Air Support
Used on ct/t-39 aircraft. location-pylon, lh, fus sta 344; material-302 cres sht per mil-s-5059 anl
01-134-6406
Thermal Special Purpo Insulation
Used as engine heat sheild under left hand wing; end item identification:aircraft, model F111
01-134-7301
Structural Aircraft Plate
01-134-7302
Structural Aircraft Plate
01-134-7303
Fuselage Aircraft Fairing
01-134-7391
Bleed Air Duct Assembly
01-134-7392
Bleed Air Duct Assembly
01-134-7395
Bleed Air Duct Assembly
01-134-7512
Access Aircraft Cover
Used on ch-47 turbine engine, rotary wing aircraft.
01-134-8431
Structural Component Air Support
Used on acft model f111. used on access door, forward engine, located fuselage station 604.00
01-134-8432
Structural Component Air Support
6.000" overall length 2.000" overall width 0.032" material thickness temper T4
01-134-8433
Structural Component Air Support
Used on f-15 acft. function-6.00
01-134-8434
Structural Component Air Support
Used on f-15 acft. function-6.00
01-134-8435
Structural Component Air Support
Used on f-15 acft. function-rudder trim actuator support
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