Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-075-6045
Elevator Rib
01-075-6217
Access Aircraft Door
Anodize surface treated
01-075-6654
Structural Component Air Fitting
01-075-6968
Radome
Used on F-4.
01-075-7527
Structural Component Air Support
Used on acft model f-4g. used on 600 gal.cl fuel tank
01-075-7538
Airfoil Rib
Used on C-141.
01-075-9672
Aircraft Engine Build- Parts Kit
F-5e acft
01-075-9758
Aircraft Skin
Used on F-16.
01-076-0559
Aircraft Tip
Used on T-38. c/o name plat pn ms 27253F1, equip instl pn 2-60021-505, wing tip panel pn 3-21200-504
01-076-0561
Aircraft Door
Used on T-38. improved door assy for mlg strut, rh
01-076-1538
Aircraft Wing Assembly
Used on ah-1 helicopter.
01-076-1539
Aircraft Wing Assembly
Used on AH-1T.
01-076-1542
Structural Aircraft Panel
Used on ah-1 series helicopter.
01-076-1583
Structural Component Air Support
01-076-1585
Structural Aircraft Plate
U/a:plate, spoiler, center console cover
01-076-1586
Structural Aircraft Panel
U/a:panel assy, hydralic selector valves
01-076-1589
Access Aircraft Cover
Used on acft c-141. lwr fwd fuselge
01-076-1593
Aircraft Stiffener
01-076-1647
Aircraft Skin
Used on C-141.
01-076-2518
Aircraft Strut
01-076-2519
Aircraft Strut
01-076-2520
Aircraft Scoop
01-076-3778
Aircraft Stiffener
75.000" overall length
01-076-3779
Structural Aircraft Plate
Eff 0025-on; nha 16B6521-53; superseded p/n 16B6521-11 ow per ECN54390
01-076-3780
Structural Aircraft Plate
Eff 0025-on; nha 16B6521-53; superseded p/n 16B6521-13 ow per ECN54390
01-076-3781
Structural Aircraft Plate
Eff 0025 on; nha 16B6521-53; superseded p/n 16B6521-15 ow per ECN54390
01-076-3804
Structural Aircraft Plate
Used on f-16 tomcat airplane.... c/o tape graphite as required 16T7450-7, surface ply as required 16T7450-17, bond ply as required 16T7450-19
01-076-3805
Structural Aircraft Plate
Used on acft model f-16. c/o tape, graphite as required p/n 16T7450-9, surface ply as required p/n 16T7450-17, bond ply as required p/n 16T7450-19
01-076-3806
Structural Aircraft Plate
C/o tape graphite as required p/n 16T7450-11, surface ply as required p/n 16T7450-17, bond ply as required p/n 16T7450-19
01-076-3807
Structural Aircraft Plate
01-076-3808
Structural Aircraft Plate
Used on acft model f-16. c/o tape graphite as required p/n 16T7450-15, surface ply as required p/n 16T7450-17, bond ply as required p/n 16T7450-19
01-076-3809
Structural Component Air Support
Made from al alloy rough casting per ams 4218-T61; eff:0001-0002, 0005
01-076-3810
Structural Component Air Support
01-076-3834
Aircraft Skin
Used on F-4.
01-076-5316
Structural Component Air Fitting
5.000" overall length 3.000" overall width 2.500 " material thickness matl:alum per fms 3002-T851; nha: 16B541-1; eff: 0020 & on
01-076-5317
Structural Component Air Fitting
5.000" overall length 3.000" overall width 2.500 " material thickness supercedes p/n: 16B6865-8; matl: alum per fms-3002-T851; nha 16B6541-1; eff: 0020 & on
01-076-5327
Cowling
Used on ah-1 acft.
01-076-5328
Cowling
Used on ah-1 series acft.
01-076-5336
Aircraft Floor
Aluminum alloy, qq-a-250/12, 7075, temper T6
01-076-5893
Cowling
Used on ah-1 series acft.
01-076-7830
Vertical Stabilizer
C/o fin tip assy, panel assy
01-076-8932
Structural Aircraft Panel
31.540" overall length 12.810" overall width
01-076-8933
Structural Aircraft Panel
31.540" overall length 12.810" overall width
01-076-8950
Structural Component Air Bracket
Leading edge elect disconnect support
01-076-8955
Aircraft Wing Assembly
01-076-8964
Movable Canopy
Form, fit
01-076-8974
Structural Aircraft Panel
Used on aircraft model uh-1n.
01-076-8975
Structural Aircraft Panel
C/o cover assy 1, 20 bolt, 20 ring; nha 16B110-5; eff 0028 on; superseded p/n 16B1530-803 ow per ecn 57505
01-076-8976
Longeron
60.000" overall length 9.000" overall width 2.500" material thickness effective on 0009-on; supercedes pn 16B2101-23 ow per ecn 50893; nha 16B2933-5
01-076-8977
Longeron
60.000" overall length 9.000" overall width 2.500" material thickness effective 0009-on; supercedes pn 16B2101-25 ow per ecn 50893; nha 16B2932-5
Page: 535 ...