Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-069-9138
Airfoil Rib
16.900" overall length 9.000" overall width 0.050" material thickness
01-069-9140
Airfoil Rib
19.000" overall length 9.000" overall width 2.500" material thickness
01-069-9141
Airfoil Rib
19.000" overall length 9.000" overall width 2.500" material thickness
01-069-9146
Aircraft Door
Used on F-15.
01-070-0306
Structural Component Air Support
01-070-2731
Structural Aircraft Plate
01-070-2732
Structural Aircraft Plate
01-070-2733
Aircraft Fairing
01-070-2734
Aircraft Fairing
01-070-2737
Airfoil Rib
26.600" overall length 10.600" overall width 0.050" material thickness
01-070-2738
Airfoil Rib
26.600" overall length 10.600" overall width 0.050" material thickness
01-070-2739
Airfoil Rib
26.600" overall length 10.600" overall width 0.050" material thickness
01-070-2740
Airfoil Rib
26.600" overall length 10.600" overall width 0.050" material thickness
01-070-2741
Airfoil Rib
26.600" overall length 10.600" overall width 0.050" material thickness
01-070-2742
Airfoil Rib
26.600" overall length 10.600" overall width 0.050" material thickness
01-070-2743
Airfoil Rib
26.600" overall length 10.600" overall width 0.050" material thickness
01-070-2744
Airfoil Rib
01-070-2745
Airfoil Rib
01-070-2746
Airfoil Rib
14.310" overall length 7.330" overall width 0.050" material thickness
01-070-2747
Airfoil Rib
14.310" overall length 7.330" overall width 0.050" material thickness
01-070-4395
Structural Component Air Bracket
01-070-4396
Structural Component Air Bracket
01-070-4416
Structural Aircraft Plate
Used on acft model f4c. alum alloy 2024-0 per qq-a-250/4 cond 0, stock size 0.125 in.thick, 8.30 in.wide, 16.80 in.length
01-070-4417
Structural Component Air Support
Used on acft model f-16. c/o support assy 1 ea p/n 16K2326-35, support 1 ea p/n 16K0328-17, support 1 ea p/n 16K0328-18, striker 1 ea p/n 16K0329-9, nut 6 ea p/n MS21042L3, bolt 2 ea p/n NAS1581A3T7, bolt 4 ea p/n NAS6203-4
01-070-4421
Aircraft Skin
01-070-4422
Aircraft Skin
Used on acft model f4c. used on rudder
01-070-4423
Aircraft Skin
01-070-5131
Aircraft Skin
Used on acft c135. 36.000 in lg, 7.000 in w, 0.051 in th. alum alloy sht 2024-0 clad per spec qq-a-250/5 0 temper. heat treat T4, finish f-2.130
01-070-5132
Aircraft Skin
Used on C-135. 48.000" overall length 48.000" overall width finish F3.35 A2.31 b cond H24
01-070-5133
Aircraft Skin
Used on B-52. 82.000" overall length 24.000" overall width
01-070-5134
Aircraft Skin
Used on B-52. finish F2.115
01-070-5135
Aircraft Skin
Used on B-52. finish F2.115
01-070-5136
Aircraft Skin
Used on B-52. finish F2.115
01-070-5137
Aircraft Skin
Used on B-52. finish F2.115
01-070-5138
Aircraft Skin
Used on B-52. 53.000" overall length 22.000" overall width finish F2.100
01-070-5139
Aircraft Skin
Used on B-52. 53.000" overall length 22.000" overall width finish F2.100
01-070-5140
Aircraft Skin
Used on B-52. 63.000" overall length 22.000" overall width finish F2.100
01-070-5141
Aircraft Skin
Used on B-52. 63.000" overall length 22.000" overall width finish F2.100
01-070-5142
Aircraft Skin
Used on B-52. 110.700" overall length 25.000" overall width cond h
01-070-5143
Aircraft Skin
01-070-5359
Aircraft Windshield Panel
Used on oh-58c acft.
01-070-5360
Aircraft Windshield Panel
Used on oh-58c acft.
01-070-5760
Aircraft Fairing
Fairing c/o 1 nose assy, 1 center section, 1 door instl, 1 aft cowl assy, 2 door, 1 hyd lines instl, 1 prop lines instl, 4 rivets, 2 latch instl
01-070-5786
Airfoil Rib
Used on ah-1 acft.
01-070-6236
Access Aircraft Door
01-070-7744
Structural Component Air Bracket
4.800" overall length 1.800" overall width 0.040" material thickness T3 temper; finish f-2.115
01-070-7754
Aircraft Fairing
Finish f-2.115; heat treat T6
01-070-7881
Structural Component Air Support
Used on acft model f-16. c/o support 1 ea p/n 16D1700-7, nut 5 ea p/n C646-10r
01-070-7883
Structural Component Air Support
Used on acft model f-16. c/o support 1 ea p/n 16D1700-11, nut 5 ea p/n C646-10r
01-070-9291
Access Aircraft Cover
Used on f-16a/b usaf aircraft. alum alloy per qq-a-250/4-T62; 0.100 in thk, 11.00 in wd, 25.00 in lg, eff on 0004 on; nha 16B6526-1
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