Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-365-8246
Fuel Cell Aircraft Plate
Used on helicopter,iroquois uh-1. 0.190" material thickness chromate surface treated
01-365-8247
Fuel Cell Aircraft Plate
Used on helicopter,iroquois uh-1. 0.190" material thickness assembly c/o plate l/h p/n 4290222-1, 2 ea nut selflocking, 4 ea rivet, solid chromate surface treated
01-365-9040
Access Aircraft Cover
Used on lantirn targoting pod.
01-365-9114
Structural Aircraft Plate
1.790" overall length 0.080" material thickness
01-365-9115
Structural Aircraft Plate
Used on e-3a,awacs aircraft.
01-365-9116
Structural Aircraft Plate
Used on e-3a,awacs aircraft.
01-365-9117
Aircraft Fairing
01-365-9118
Aircraft Skin
66.000" overall length 55.000" overall width exterior engine aft inlet nacelleskin
01-365-9119
Aircraft Skin
66.000" overall length 55.000" overall width exterior engine aft inlet nacelleskin
01-365-9120
Structural Component Air Support
10.580" overall length 2.740" overall width door actuator support
01-365-9121
Structural Component Air Support
10.580" overall length 2.740" overall width door actuator support
01-365-9442
Aircraft Leading Edge
01-365-9443
Aircraft Leading Edge
01-365-9444
Aircraft Leading Edge
01-365-9445
Aircraft Leading Edge
01-365-9446
Aircraft Leading Edge
01-365-9447
Aircraft Trailing Edge
01-365-9449
Structural Component Air Support
01-365-9450
Structural Component Air Support
01-365-9598
Structural Aircraft Plate
Used on f/a 18 hsp - supported. 5.040" overall length
01-366-0513
Access Aircraft Door
Used on aircraft model ea-6b. components include latch 1, hinge assy 1, shim 1, doubler 0.050 in. thick 1, skin 0.050 in. thick 1; length 4.500 in. nom., 3.810 in. w. nom. primer epoxy-polyamide surface treated
01-366-0514
Access Aircraft Door
Used on aircraft models a-6e,ea-6b. components include latches 2, hinges 1, shim 1, doubler 0.063 in. thick 1, skin 0.063 in. thick 1 primer epoxy-polyamide surface treated
01-366-0711
Aircraft Beam
Used on b-2 bomber airplane. 27.263" overall length 2.600" overall width 2.600" material thickness heat treat per T7351; consist of 52 holes
01-366-0712
Aircraft Fairing
01-366-0713
Aircraft Fairing
01-366-0714
Aircraft Strut
Used on aircraft,stratolifter c-135.
01-366-0878
Structural Component Air Support
Used on b-2 bomber aircraft. isolator, vibration; shock mount, equipment rack
01-366-1342
Access Aircraft Cover
Used on B-1B. aft vane
01-366-1343
Access Aircraft Cover
Used on B-1B. aft vane
01-366-1344
Access Aircraft Cover
Used on B-1B. aft vane
01-366-1345
Access Aircraft Cover
Used on B-1B. aft vane
01-366-1346
Access Aircraft Cover
Used on B-1B. fwd vane
01-366-1348
Access Aircraft Door
Used on B-1B. located YF472.000 to YF492.000; production part L3010790-031; used on envir cont system ground air service door; identical to L3010790-031 except allow .250 excess matl around periphey
01-366-1390
Structural Component Air Fitting
01-366-2443
Access Aircraft Door
01-366-2896
Access Aircraft Door
Used on p-3c,orion aircraft.
01-366-2962
Aircraft Wing Assembly
Used on ea-6b acft.
01-366-2963
Aircraft Wing Assembly
Used on ea6-b acft.
01-366-2964
Aircraft Wing Assembly
Used on ea6-b acft.
01-366-2968
Structural Component Air Support
4.500" overall length 3.000" overall width frame attachment fitting
01-366-3466
Structural Component Air Bracket
01-366-3674
Access Aircraft Cover
Used on b-2 pacer special. used as a safety access door asy, c/o h/c panel asy, loop ftg, rubplate, collar & hi-lok pin, next assembly DAA3116B100
01-366-3676
Access Aircraft Cover
Used on B-1B. unique spare, used on 82-001 & subq, used as a forward vane cover
01-366-3677
Access Aircraft Cover
Used on B-1B. unique spare, used on 82-001 & subq, used as a forward vane cover
01-366-3678
Access Aircraft Cover
Used on B-1B. unique spare, used on 82-0001 & subq, used as a forward vane cover
01-366-3771
Structural Aircraft Plate
15.500" overall length 4.500" overall width 0.040" material thickness cadmium surface treated
01-366-3772
Structural Aircraft Plate
15.500" overall length 4.500" overall width 0.040" material thickness cadmium surface treated
01-366-3773
Aircraft Frame
17.000" overall length 2.000" overall width 0.063" material thickness angle; u/o 3P21677-118
01-366-3775
Aircraft Leading Edge
01-366-3776
Aircraft Leading Edge