Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-511-6991
Aircraft Hinge
Used on fighter aircraft-first ( f 18 e/f ).
01-511-6992
Access Aircraft Door
Used on fighter aircraft-first (f18 e/f). (navy) door, access, aircr
01-511-6993
Aircraft Fairing
Used on fighter aircraft-first (f18 e/f). navy) fairing, aircraft
01-511-6995
Access Aircraft Door
Used on fighter aircraft - first ( f 18 e/f ).
01-511-7067
Aircraft Intercostal
01-511-7152
Structural Component Air Support
01-511-7339
Stiffener Aircraft Rib
01-511-7347
Stiffener Aircraft Rib
01-511-7363
Structural Aircraft Panel
Foam core foam core made of dimensionally stabile, closed cell, rigid, polyuretha foam per cm-2000
01-511-7368
Stiffener Aircraft Rib
01-511-7374
Structural Aircraft Panel
Foam core foam core made of dimensionally stabile, closed cell, rigid, polyuretha foam per cm-2000
01-511-7379
Stiffener Aircraft Rib
01-511-7381
Structural Aircraft Panel
Foam core foam core made of dimensionally stabile, closed cell, rigid, polyuretha foam per cm-2000
01-511-7397
Structural Aircraft Panel
Foam core foam core made of dimensionally stabile, closed cell, rigid, polyuretha foam per cm-2000
01-511-7405
Structural Aircraft Panel
Foam core foam core made of dimensionally stabile, closed cell, rigid, polyuretha foam per cm-2000
01-511-7579
Structural Component Air Support
Used on f-22 raptor. seal assy, lns upper left
01-511-7580
Structural Component Air Support
Used on f/a-22 raptor. seal assy, lns upper right
01-511-7581
Structural Component Air Support
Used on f-22 raptor. seal assy-nozzle, longitudinal, upper keelson
01-511-7597
Structural Aircraft Panel
Foam core foam core made of dimensionally stabile, closed cell, rigid, polyuretha foam per cm-2000
01-511-7599
Structural Aircraft Panel
Foam core foam core made of dimensionally stabile, closed cell, rigid, polyuretha foam per cm-2000
01-511-7601
Structural Aircraft Panel
Foam core foam core made of dimensionally stabile, closed cell, rigid polyuretha foam per cm-2000
01-511-7604
Structural Aircraft Panel
Foam core foam core made from dimensionally stabile, closed cell, rigid, polyuretha foam per cm-2000
01-511-7611
Structural Aircraft Panel
Foam core foam core made from dimensionally stabile, closed cell , rigid, polyuretha foam per cm-2000
01-511-8278
Structural Component Air Bracket
3.100" overall length 1.000" overall width 0.050" material thickness clip dim. are stock material; finish per srf-2.3
01-511-8284
Structural Aircraft Plate
43.000" overall length 1.500" overall width 0.050" material thickness strap dim. are stock material; finish per srf-2.3
01-511-8401
Stiffener Aircraft Rib
01-511-8653
Structural Component Air Bracket
2.500" overall length 1.550" overall width 0.050" material thickness
01-511-8752
Exhaust Heat Shield
Liner, amns
01-511-8756
Bleed Air Duct Assembly
01-511-8774
Structural Component Air Bracket
6.200" overall length 4.800" overall width 0.080" material thickness clip nha 204-18279; dims are stock material; srf 2.30
01-511-8778
Structural Component Air Bracket
01-511-8947
Stiffener Aircraft Rib
01-511-8955
Stiffener Aircraft Rib
01-511-9044
Structural Component Air Bracket
27.200" overall length 4.000" overall width 0.040" material thickness bracket-duct attach dim. are stock material; nuclear hardness critcal item-no unautherized substitution; finish per F2.44, optional brush tin plate per BAC5849
01-511-9055
Structural Component Air Bracket
27.200" overall length 4.100" overall width 0.040" material thickness bracket-duct attach dim. are stock material; nuclear hardness critical item-no unautherized substitutions; finish per F2.44, optional-brush tin plate per BAC5849
01-511-9286
Aircraft Stiffener
12.000" overall length 7.000" overall width 0.050" material thickness bulkhead stiffener inbd-outbd; u/o -2; opp -181; comp b, type i, annealed; stock
01-511-9293
Structural Aircraft Plate
01-511-9502
Structural Component Air Support
50.000" overall length support next higher assy, 68A328002 u/o f-15c, d BLK23
01-511-9503
Structural Component Air Support
50.000" overall length support next higher assy, 68A328002 u/o f-15c, d BLK23
01-511-9506
Aircraft Fairing
51.000" overall length 45.000" overall width 0.063" material thickness nha 35-29710; -5 opp -6; finish per f-2.16; dimensions listed are stock size
01-511-9681
Structural Component Air Bracket
4.000" overall length 0.900" overall width nha 8148701-100 alodize surface treated
01-511-9708
Aircraft Stiffener
8.500" overall length 6.330" overall width 0.050" material thickness spacer nha 8148699-100
01-511-9723
Aircraft Stiffener
5.750" overall length 4.200" overall width 0.050" material thickness stiffener nha 8148703-100
01-511-9738
Aircraft Stiffener
8.240" overall length 1.250" overall width 0.050" material thickness stiffener nha 8148701-100
01-511-9832
Stiffener Aircraft Rib
01-511-9852
Stiffener Aircraft Rib
01-511-9860
Stiffener Aircraft Rib
01-512-0095
Structural Aircraft Panel
Used on sh-2g seasprite helicopter. lh side panel, fixed, instl sta 114.00 to sta 133.37
01-512-0096
Structural Aircraft Panel
Used on sh-2g seasprite helicopter. rh side panel, fixed, instl sta 114.00 to sta 133.37
01-512-0099
Access Aircraft Door
Used on sh-2g seasprite helicopter. door panel stock size 0.032 x 5.75 x 8.05