Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-553-7765
Aircraft Spar
28.000" overall length 6.000" overall width 1.750" material thickness dim. are stock material
01-553-7800
Structural Component Air Support
Used on A-10. 10.000" overall length 2.000" overall width 1.500" material thickness splice angle alt for -24; dim. are stocksize matl.
01-553-7818
Stiffener Aircraft Rib
01-553-7820
Aircraft Former
Used on A-10. 10.000" overall length 4.200" overall width 0.040" material thickness former cres sh 301 annealed; dim. are stocksize
01-553-7827
Stiffener Aircraft Rib
01-553-7833
Stiffener Aircraft Rib
01-553-7992
Aircraft Former
Used on F/A18D. 40.000" overall length 32.000" overall width 2.500" material thickness former-engine air inlet, Y419.000 7075-T7351 al plate
01-553-7993
Aircraft Former
01-553-7994
Aircraft Former
01-553-7999
Structural Aircraft Panel
Used on hawker 800,kars peace pioneer,packdu/kumkang.
01-553-8030
Aircraft Window Panel
Used on f16 aircraft.
01-553-8146
Movable Canopy
Used on fighter aircraft-first(f18 e/f).
01-553-8148
Movable Canopy
Used on f18c night attack, established for fa18c.
01-553-8150
Movable Canopy
Used on f18d night attack, established for fa18d.
01-553-8151
Movable Canopy
Used on canopy, movable, aircraft; airframe; f18d night attack established for fa18d.
01-553-8244
Airframe Modification Kit
Used on arrlist code; canopy, movable. (navy) modification kit
01-553-8245
Movable Canopy
Used on canopy, movable; arr list code; f/a-18f model code in support of cep 6038; aircraft model code for f/a-18f. (navy) : canopy, movable
01-553-8352
Aircraft Former
10.400" overall length 4.200" overall width 0.040" material thickness former matl cres steel sheet mil-s-5059, 301 annealed; the - 85 replaces -57; u/o a-10a 1
01-553-8357
Aircraft Stiffener
01-553-8359
Aircraft Former
9.000" overall length 2.300" overall width 0.020" material thickness former matl cres steel sheet mil-s-5059, 301 annealed hres st ams 5542 inconel x-750; u/o a-10a 1
01-553-8363
Structural Component Aircraf Web
01-553-8366
Structural Component Air Support
01-553-8370
Structural Component Air Support
01-553-8372
Aircraft Former
10.400" overall length 4.200" overall width 0.040" material thickness former matl cress steel sheet mil-5059, 301 annealed hres st ams 5542 inconel x-750; u/o a-10a 1
01-553-8380
Aircraft Stiffener
01-553-8388
Stiffener Aircraft Rib
6.374" overall length 1.500" overall width rib alt matl -9 may be fab from 2 x 6 x 8 inch stock spec fms-3002-T851; dim are stock matl
01-553-8397
Structural Component Air Bracket
Used on A-10. 1.900" overall length angle m/f 160D415008-1, u/o -3, -4, -7, -8, -9-, 10, dim are stocksize
01-553-8404
Structural Component Air Support
01-553-8407
Structural Component Air Support
01-553-8415
Airfoil Rib
81.000" overall length 2.750" overall width rib matl spec fms 3004-T7351
01-553-8454
Aircraft Spar
Spar matl fms-3004-T7351; -14 is replacement for -10 per lockheed drwg 16W131
01-553-8474
Aircraft Spar
Spar -6 opp
01-553-8476
Airfoil Rib
Used on F-16. 7.000" overall length 5.000" overall width 2.000" material thickness rib nha 16W049; opposite -18; m/f -13; fnsh A100; alt matl -15/-16, -17/-18 may be fabricated from (s x 5 x 7 stock size) FMS3002-T851, machine as shown; dim. are stocksize
01-553-8555
Structural Component Air Support
Used on airframe structural components.
01-553-8586
Control Surface Aircra Parts Kit
Used on airframe structural components.
01-553-8647
Structural Component Air Support
Used on cobham air refueling and auxiliary mission equipment. track assembly auxiliary tank
01-553-8650
Refueling Aircraft Tank
Used on cobham air refueling and auxiliary. air refueling store assembly auxiliary tank
01-553-8651
Refueling Aircraft Tank
Used on cobham air refueling and auxiliary. air refueling store assembly auxiliary tank
01-553-8701
Aircraft Spar
Spar matl al 7075 per qq-a-367 comp 7075 temp T73 precision die forging; -11 may be used as a replacement for the -9
01-553-8702
Airfoil Rib
Used on F-16. 8.000" overall length 6.000" overall width 2.000" material thickness rib nha 16W049; m/f -8; opposite -9; precision die forging; alt matl -9/-10 maybe fabricate from 2 x 6 x 8 stock, spec fms-3002-T851
01-553-8713
Airfoil Rib
Used on F-16. 80.500" overall length 6.200" overall width 2.000" material thickness rib NHA16W041; dim are stocksize; fnsh A432
01-553-8756
Aircraft Stiffener
01-553-8759
Airfoil Rib
01-553-8760
Aircraft Spar
Spar
01-553-8765
Airfoil Rib
01-553-8767
Airfoil Rib
01-553-8779
Structural Component Air Support
01-553-8780
Airfoil Rib
Used on F-16. 80.500" overall length 6.200" overall width 2.000" material thickness rib hna 16W041; dim. are stocksize; fnsh A432
01-553-8784
Aircraft Spar
8.000" overall length spar matl al aly 7075 per qq-a-367 comp 7075 temp T73 precision die forging; -12 may be used as replacement for -10 per lockheed drwg 16W145
01-553-8785
Aircraft Stiffener