Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-149-2669
Structural Component Air Fitting
Fitting assembly, cowl latch
01-149-2679
Structural Aircraft Plate
Used on b-52 aircraft. material-cres steel aisi 321 or 347 annealed per mil-s-6721; stock size-.032 x 1.50 x 11.2"; location-sta 270.000, tail fairing installation, right hand inboard strut
01-149-2680
Structural Aircraft Plate
Location-closure rib assembly, function-web; matl 6al-4v
01-149-2681
Structural Aircraft Plate
Location-closure rib assembly; function-bearing strip; matl 6al-4v
01-149-2682
Structural Aircraft Plate
Location-closure rib assembly, function-bearing strip; matl 6al-4v
01-149-2683
Structural Aircraft Plate
Location-closure rib assembly, function-web 16; matl 6al-4v
01-149-2684
Structural Aircraft Plate
Location-closure rib assembly, function-doubler 16; matl 6al-4v
01-149-2685
Structural Aircraft Plate
Location-closure rib assembly, function-bearing strip; matl 6al-4v
01-149-2686
Structural Aircraft Plate
40.500" overall length 2.600" overall width 0.020" material thickness location-closure rib assembly; function-angle 16
01-149-2687
Structural Aircraft Plate
25.300" overall length 13.000" overall width 0.063" material thickness location-closure rib assembly, function-web 18; matl 6al-4v
01-149-2693
Aircraft Former
Used on B-52. function-chord assembly
01-149-2694
Aircraft Former
Used on B-52. function stiffener
01-149-2695
Aircraft Former
Used on B-52. function-chord assembly
01-149-2698
Aircraft Former
13.000" overall length 0.600" overall width 0.040" material thickness
01-149-2699
Aircraft Former
16.000" overall length 2.500" overall width 0.025" material thickness
01-149-2701
Aircraft Skin
Used on b-52 bomber airplane.... material; cres sheet, aisi 302, comp 302 annealed, surf cond 2n
01-149-2746
Radome
Used on c-5a aircraft.
01-149-3140
Structural Aircraft Plate
10.500" overall length 6.100" overall width 0.063" material thickness stainless steel sheet aisi 17-7 ph per bms 7-12a; heat treat to 180, 000 to 200, 000 psi; finish f-8.05
01-149-3141
Structural Aircraft Plate
11.000" overall length 11.000" overall width 0.080" material thickness used as doubler on installation rib number 5
01-149-3143
Structural Component Air Support
Used on uh-1f helicopter. function-support tail rotor drive
01-149-3144
Structural Component Air Bracket
1.400" overall length 2.100" overall width 0.063" material thickness clip
01-149-3145
Aircraft Frame
50.000" overall length 3.000" overall width 0.050" material thickness
01-149-3146
Structural Component Air Support
1.300" overall length 3.000" overall width 0.080" material thickness
01-149-3147
Structural Component Air Support
2.400" overall length 1.500" overall width 0.063" material thickness
01-149-3148
Structural Component Air Support
01-149-3149
Structural Component Air Support
2.000" overall length 1.000" overall width 0.180" material thickness
01-149-3150
Structural Component Air Support
2.500" overall length 1.000" overall width 0.180" material thickness
01-149-3151
Structural Component Air Support
2.500" overall length 1.500" overall width 0.180" material thickness
01-149-3152
Structural Component Air Support
3.200" overall length 1.500" overall width 0.125" material thickness
01-149-3153
Structural Component Air Support
01-149-3154
Structural Component Air Support
4.000" overall length 1.000" overall width 0.130" material thickness
01-149-3156
Aircraft Former
50.000" overall length 5.000" overall width 0.063" material thickness
01-149-3157
Aircraft Former
Used on B-52. 12.000" overall length 5.000" overall width 0.080" material thickness
01-149-3158
Aircraft Former
18.000" overall length 6.000" overall width 0.063" material thickness
01-149-3918
Structural Aircraft Plate
Used as filler on firewall installation
01-149-3919
Structural Aircraft Plate
5.000" overall length 1.190" overall width 0.071" material thickness
01-149-3920
Structural Aircraft Plate
5.000" overall length 1.190" overall width 0.071" material thickness
01-149-3921
Structural Aircraft Plate
3.000" overall length 0.600" overall width 0.040" material thickness used as filler on firewall installation
01-149-3922
Structural Aircraft Plate
10.000" overall length 0.500" overall width 0.032" material thickness used as doubler on firewall installation
01-149-3923
Structural Aircraft Plate
Used as doubler on firewall installation, forward nacelle; opposite p/n 25-2308-827
01-149-3924
Structural Aircraft Plate
10.000" overall length 0.500" overall width 0.032" material thickness used as doubler on firewall installation
01-149-3925
Structural Aircraft Plate
Used as doubler on firewall installation, forward nacelle; opposite p/n 25-2308-829
01-149-3926
Structural Aircraft Plate
Used on b-52 aircraft. material-cres sheet aisi 301 per mil-s-5059, comp d 1/4 hard-surf cond 2b; stock size .025 x 5.0 x 8.2; location-sta 236.25, tail fairing installation, right hand inboard strut
01-149-3927
Structural Aircraft Plate
5.000" overall length 3.000" overall width 2.000" material thickness 10 holes along lg w/3/16 in. dia equally spaced; opposite to p/n 3F21107-103; used as fitting-tee, frame
01-149-3928
Structural Component Air Support
Used on f-4 aircraft. used on camera beam, left hand, forward station vertical or oblique still picture camera installation
01-149-3929
Structural Component Air Support
Used on f-4 aircraft. used on camera beam, right hand, forward station vertical or oblique still picture camera installation
01-149-3930
Structural Component Air Support
2.700" overall length 2.100" overall width 0.050" material thickness opposite to p/n 29-2517-2; used T0 support tube
01-149-3931
Structural Component Air Support
2.700" overall length 2.100" overall width 0.050" material thickness opposite to p/n 29-2517-1; used tosupport tube; incl. nut plate
01-149-3932
Structural Component Air Support
2.600" overall length 2.200" overall width 0.050" material thickness opposite to p/n 29-2517-4; includes nut plate, self-locking; used to support tube
01-149-3933
Structural Component Air Support
2.600" overall length 2.200" overall width 0.050" material thickness opposite to p/n 29-2517-3; includes nut plate, self-locking; used to suppoort tube
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