FSC 1560 Airframe Structural Components: 1560-01-281-8588, 1560-01-281-9248, 1560-01-281-9884
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1560-01-281-8588 1560012818588 | 5-73139-17 | Rib, Airfoil | Aircraft Mission Design Series: KC-135 Special Features: 0 temper, heat treat T4;FINISH F-2.115;OPP -18; nha 5.71741 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 1560-01-281-8589 1560012818589 | 68A112107-2035 68A112107-2033 68A112107-2039 68A112107-2075 68A112107-2041 | Spar, Aircraft | Aircraft Mission Design Series: F-15 Aircraft Location: Spar assembly, rear Side FOR Which Designed: Left side | Boeing Company, The (76301) | |
| 1560-01-281-8590 1560012818590 | 68A112107-2050 68A112107-2030 68A112107-2040 68A112107-2076 68A112107-2042 | Spar, Aircraft | Aircraft Mission Design Series: F-15 Aircraft Location: Spar assembly, rear Side FOR Which Designed: Right side | Boeing Company, The (76301) | |
| 1560-01-281-8591 1560012818591 | L5305302-032 | Window Panel, Aircraft | Aircraft Mission Design Series: B-1B Special Features: Nuclear hardness critical item; consist of 1 shield assy, 1 wire harness, 2 bracket, 2 nutplate, 2 screw, 2 clamp, 2 washer; nha L5305301 Criticality Code Justification: FEAT | Boeing Company, The (43999) | |
| 1560-01-281-8592 1560012818592 | L5305339-012 | Window Panel, Aircraft | Aircraft Mission Design Series: B-1B Special Features: Nuclear hardness critical item; consist of 1 shield, 3 seal, 4 washer, R T-knobs; nha L5305330 Criticality Code Justification: FEAT | Boeing Company, The (43999) | |
| 1560-01-281-8593 1560012818593 | L5305302-021 | Window Panel, Aircraft | Aircraft Mission Design Series: B-1B Special Features: Nuclear hardness critical item; consist of 1 retainer, 1 glove, 4 seal, 4 receptacle, 6 nut, 2 pin, 2 washer, 1 shield, 1 doubler, 2 bulb seal; nha L5305301 Criticality Code Justification: FEAT | Boeing Company, The (43999) | |
| 1560-01-281-8594 1560012818594 | L5305302-012 | Window Panel, Aircraft | Aircraft Mission Design Series: B-1B Special Features: Nuclear hardness critical item; consist of 1 retainer, 1 glove, 3 seal, 4 receptacle, 6 nut, 2 pin, 2 washer, 1 shield, 1 doubler; nha L5305301 Criticality Code Justification: FEAT | Boeing Company, The (43999) | |
| 1560-01-281-8595 1560012818595 | L5305302-022 | Window Panel, Aircraft | Aircraft Mission Design Series: B-1B Special Features: Nuclear hardness critical item; consist of 1 retainer, 1 glove, 4 seal, 4 receptacle, 6 nut, 2 pin, 2 washer, 2 bulb seal, 1 shield, 1 doubler; nha L5305301 Criticality Code Justification: FEAT | Boeing Company, The (43999) | |
| 1560-01-281-8873 1560012818873 | 55-71 | Cover, Special | Goodrich Corporation (97153) | ||
| 1560-01-281-9178 1560012819178 | 99352-1-89 99352-1 | Conduit Assembly | III End Item Identification: F-9 aircraft | Datex-Ohmeda Inc. (44503) Northrop Grumman Systems Corporation (15280) Products Support Inc. (53247) | |
| 1560-01-281-9179 1560012819179 | 65219-09048-041 | Support, Structural Component, Air | Aero Components Inc. (59213) Essner Manufacturing L.P. (2B834) Rotair Industries Inc. (54878) | ||
| 1560-01-281-9180 1560012819180 | 65219-09048-043 | Support, Structural Component, Air | Rotair Industries Inc. (54878) W and G Machine Company Incorporated (33682) Sikorsky Aircraft Corporation (78286) | ||
| 1560-01-281-9247 1560012819247 | 145G0290-1 | Plate, Turning, Assembly | General Characteristics Item Description: Consists of one id plate; 4 screws; 2 oval sleeves; 1 cable; 4 clamp stud; 8 hex nuts; 4 support blocks; 4 wing nuts; 4 plugs; 1 base plate; 24.000 in. lg; 20.000 in. W | The Boeing Company (77272) | |
| 1560-01-281-9248 1560012819248 | 70213-01004-105 | Retainer, Window | FLO Tech Inc. (23231) Sikorsky Aircraft Corporation (78286) | ||
| 1560-01-281-9249 1560012819249 | 4F59243-101A | Support, Structural Component, Air | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-200/11 fed spec single material response Overall Width: 3.550 inches nominal | Lockheed Martin Corporation (98897) CPI Aerostructures Inc. (9U679) MRA Systems Inc. (1B6R3) | |
| 1560-01-281-9453 1560012819453 | 68A112194-2009 | Plate, Structural, Aircraft | III End Item Identification: F-15 Special Features: T81 Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 1560-01-281-9783 1560012819783 | 16B6530-849 | Cover, Access | Lockheed Martin Corporation (81755) | ||
| 1560-01-281-9882 1560012819882 | 204-70099-79 | Plate, Structural, Aircraft | Aircraft Mission Design Series: E-3A Special Features: Make from BAC1512-3404 by 1.9 in;heat treat T42; finish SRF2.30 Aircraft Location: Engine nacelle nose cowl assy | The Boeing Company (81205) | |
| 1560-01-281-9883 1560012819883 | 90-3909-6 | Support, Structural Component, Air | III End Item Identification: Acft model B-52 III Supplementary Features: Functional description:used on outboard wing trailing edge assemblies | The Boeing Company (81205) Beta Engineering Inc. (33436) | |
| 1560-01-281-9884 1560012819884 | 90-5044-1 | Balance Weight, Aileron | Special Features: Architectural bronze, revere 283 or equiv; chemical; CU56.5 ZN4.25 lead 2.25; finish F-4.30; 22.00 in lg, 2.35 in wd, 0.11 in thk; nha 3-96128; used on outboard aileron balance panel, balance weight End Item Identification: Acft model KC-135 | The Boeing Company (81205) |