Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-467-4883
Aircraft Stiffener
01-467-4884
Aircraft Stiffener
01-467-4885
Aircraft Stiffener
11.002" overall length 2.350" overall width 0.045" material thickness next higher assy, 68A332001, u/o f-15a cum 6-blk 11, f-15b cum 1-blk 11, dim. stock material
01-467-4886
Aircraft Stiffener
01-467-4887
Aircraft Former
01-467-4888
Aircraft Stiffener
01-467-4889
Aircraft Stiffener
11.004" overall length 2.076" overall width 0.045" material thickness next higher assy, 68A332001, u/o f-15a cum 1-blk 11, f-15b CUM1-blk 11, dim. stock material
01-467-4890
Aircraft Stiffener
6.570" overall length 1.880" overall width 0.045" material thickness dim. stock material; next higher assy 68A332001 u/o f-15a, b CUM1-BLK11
01-467-4891
Aircraft Stiffener
01-467-4892
Aircraft Stiffener
11.620" overall length 2.004" overall width 0.045" material thickness next higher assy, 68A332001, u/o f-15a CUM1-blk 11, f-15b CUM1-blk 11, dim.stock material
01-467-4893
Stiffener Aircraft Rib
5.400" overall length 2.050" overall width 0.045" material thickness next higher assy, 68A332001, u/o f-15a cum 1-blk 6, f-15b cum 1-blk 4, dim.stock material
01-467-4894
Aircraft Stiffener
9.200" overall length 4.000" overall width 0.063" material thickness dim. stock material; next higher assy 68A331083-1017 u/o f-15a, b, c, d, e CUM1&up
01-467-4895
Structural Component Air Support
01-467-4896
Aircraft Stiffener
9.200" overall length 3.750" overall width 0.063" material thickness dim. stock material; next higher assy 68A331083-1019 u/o f-15a, b, c, d, e spares
01-467-4897
Aircraft Stiffener
01-467-4898
Aircraft Former
01-467-4899
Aircraft Stiffener
9.200" overall length 3.750" overall width 0.063" material thickness dim. stock material; next higher assy 68A331083-1020 u/o f-15a, b, c, d, e spares
01-467-4900
Aircraft Former
01-467-5192
Elevon
Nuclear hardness critical item, nuclear hardness process
01-467-5193
Elevon
Nuclear hardness critical item, nuclear hardness process
01-467-5195
Access Aircraft Cover
01-467-5196
Aircraft Former
01-467-5199
Structural Component Air Support
01-467-5200
Structural Component Air Support
5.400" overall length 1.400" overall width angle dim. stock material; next higher assy 68A332013-1001 u/o f-15a, b CUM1-BLK11
01-467-5201
Aircraft Stiffener
5.650" overall length 1.390" overall width 0.045" material thickness next higher assy, u/o f-15a cum 1-blk 11, f-15b cum 1-blk 11, dim.stock material
01-467-5280
Fuel Aircraft Tank
01-467-5288
Aircraft Bulkhead
01-467-5299
Aircraft Bulkhead
01-467-5307
Structural Component Air Support
Used on h1 helicopter. shelf instl, avionics-tailbooms, b.s. 111.9 to 177.1
01-467-5575
Structural Aircraft Panel
Used on chinook helicopter.
01-467-5577
Access Aircraft Door
Used on r.h. door, avionics bay, f-16 aircraft.
01-467-5589
Aircraft Frame
01-467-5616
Stiffener Aircraft Rib
5.500" overall length 2.600" overall width 0.036" material thickness next higher assy, 68A335007, u/o f-15a cum 2-3, 6, 9-blk 11, f-15b cum 1, 3-blk 11, dim.stock material
01-467-5618
Aircraft Former
7.500" overall length 4.700" overall width 0.050" material thickness next higher assy, 68A332201, u/o f-15a blk 12
01-467-5619
Stiffener Aircraft Rib
5.400" overall length 2.050" overall width 0.045" material thickness angle next higher assy, 68A332001, u/o f-15a cum 1, 4-5, 7-8, f-15b cum 2, dim.stock material
01-467-5620
Aircraft Former
8.250" overall length 4.700" overall width 0.050" material thickness next higher assy, 68A332201, u/o f-15a blk 12
01-467-5621
Aircraft Former
12.500" overall length 2.900" overall width 0.050" material thickness next higher assy, 68A332201, u/o f-15c cum 1
01-467-5622
Aircraft Stiffener
11.200" overall length 1.900" overall width 0.050" material thickness next higher assy, 68A332201, u/o f-15a blk 12
01-467-5623
Aircraft Former
8.250" overall length 5.300" overall width 0.050" material thickness next higher assy, 68A332201, u/o f-15a blk 12
01-467-5624
Structural Component Air Support
12.250" overall length 11.060" overall width 0.050" material thickness next higher assy, 68A332300, u/o f-15c cum 288
01-467-5625
Aircraft Former
11.000" overall length 1.330" overall width 0.050" material thickness next higher assy, 68A332300, u/o f-15e cum 147
01-467-5626
Structural Component Air Support
6.800" overall length next higher assy, 68A332300, u/o f-15c cum 288
01-467-5629
Aircraft Former
11.000" overall length 1.330" overall width 0.050" material thickness next higher assy, 68A332300, u/of-15e CUM147
01-467-5630
Aircraft Former
10.150" overall length 1.250" overall width 0.050" material thickness next higher assy, 68A332399, u/o f-15e cum 147
01-467-5631
Aircraft Former
10.000" overall length 5.650" overall width 0.050" material thickness next higher assy, 68A332300, f-15e cum 147
01-467-5632
Aircraft Former
8.700" overall length 5.680" overall width 0.050" material thickness next higher assy, 68A332300, u/o f-15e cum 147
01-467-5633
Aircraft Former
8.800" overall length 1.250" overall width 0.050" material thickness next higher assy, 68A332300, u/o f-15e cum 147
01-467-5634
Aircraft Former
8.700" overall length 5.680" overall width 0.050" material thickness next higher assy, 68A332300, u/o f-15e cum 147
01-467-5635
Aircraft Former
9.500" overall length 1.250" overall width 0.050" material thickness next higher assy, 68A332300, u/o f-15e cum 147
01-467-5636
Structural Component Air Support
6.800" overall length next higher assy, 68A332300, u/o f-15e cum 3