Airframe Structural Components: 68A113141-2003, 68A113141-2004, 68A113146-2006
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 68A113141-2003 68A1131412003 | 1560-01-252-4051 | Support, Structural Component, Air | III End Item Identification: Acft model F-15 Special Features: 7075-0 per QQ-A-250/12 cond 0; 18.60 in. lg, 4.70 in. wd, 0.063 in. thk; opposite P/N -2004 III Supplementary Features: Functional description:used on wing inner T.E. stiffener panel support | Boeing Company, The (76301) | |
| 68A113141-2004 68A1131412004 | 1560-01-252-4052 | Support, Structural Component, Air | III End Item Identification: Acft model F-15 Special Features: 7075-0 per QQ-A-250/12 cond 0; 18.60 in. lg, 4.70 in. wd, 0.063 in. thk; opposite P/N -2003 III Supplementary Features: Functional description:used on wing inner T.E. stiffener panel support | Boeing Company, The (76301) | |
| 68A113142-2001 68A1131422001 | 1560-01-253-1222 | Support, Structural Component, Air | III End Item Identification: F-15 acft | Boeing Company, The (76301) | |
| 68A113142-2002 68A1131422002 | 1560-01-253-7765 | Support, Structural Component, Air | III End Item Identification: F-15 acft Special Features: Aluminum alloy 7075-0; support-panel, wing inner trailing edge stiffener | Boeing Company, The (76301) | |
| 68A113142-2003 68A1131422003 | 1560-01-294-6232 | Support, Structural Component, Air | III End Item Identification: F-15 acft | Boeing Company, The (76301) | |
| 68A113142-2004 68A1131422004 | 1560-01-294-7849 | Panel, Structural, Aircraft | Aircraft Mission Design Series: F-15 Special Features: Support, panel-wing inner trailing edge stiffener | Boeing Company, The (76301) | |
| 68A113142-2007 68A1131422007 | 1560-01-294-6232 | Support, Structural Component, Air | III End Item Identification: F-15 acft | Boeing Company, The (76301) | |
| 68A113142-2008 68A1131422008 | 1560-01-294-7849 | Panel, Structural, Aircraft | Aircraft Mission Design Series: F-15 Special Features: Support, panel-wing inner trailing edge stiffener | Boeing Company, The (76301) | |
| 68A113143-2003 68A1131432003 | 1560-01-253-7767 | Support, Structural Component, Air | III End Item Identification: F-15 acft Special Features: Aluminum alloy 7075-0; support-panel, wing inner trailing edge stiffener | Boeing Company, The (76301) | |
| 68A113143-2004 68A1131432004 | 1560-01-253-1218 | Support, Structural Component, Air | III End Item Identification: Acft model F-15 Special Features: 7075-0 per QQ-A-250/12 cond 0; 20.35 in. lg, 4.35 in. wd, 0.063 in. thk; used on -1002 III Supplementary Features: Functional description:used on inner T.E. stiffener wing panel support | Boeing Company, The (76301) | |
| 68A113143-2005 68A1131432005 | 1560-01-253-7767 | Support, Structural Component, Air | III End Item Identification: F-15 acft Special Features: Aluminum alloy 7075-0; support-panel, wing inner trailing edge stiffener | Boeing Company, The (76301) | |
| 68A113143-2006 68A1131432006 | 1560-01-253-1218 | Support, Structural Component, Air | III End Item Identification: Acft model F-15 Special Features: 7075-0 per QQ-A-250/12 cond 0; 20.35 in. lg, 4.35 in. wd, 0.063 in. thk; used on -1002 III Supplementary Features: Functional description:used on inner T.E. stiffener wing panel support | Boeing Company, The (76301) | |
| 68A113144-2001 68A1131442001 | 1560-01-337-8044 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15 Material: Aluminum alloy 7075 Aircraft Location: Splice;upper-hinge beamm to closure rib | Boeing Company, The (76301) | |
| 68A113144-2002 68A1131442002 | 1560-01-337-8045 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15 Material: Aluminum alloy 7075 Aircraft Location: Splice;upper hinge beam to closure rib | Boeing Company, The (76301) | |
| 68A113144-2003 68A1131442003 | 1560-01-337-8046 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15 Material: Aluminum alloy 7075 Aircraft Location: Angle;upper-hinge beam to closure rib | Boeing Company, The (76301) | |
| 68A113144-2004 68A1131442004 | 1560-01-337-8047 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15 Material: Aluminum alloy 7075 Aircraft Location: Angle;upper-hinge beam to closure rib | Boeing Company, The (76301) | |
| 68A113145-2003 68A1131452003 | 1560-01-338-3620 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15 Material: Aluminum alloy 7075 Aircraft Location: Angle, splice;lower hinge beam, trailing edge closure rib | Boeing Company, The (76301) | |
| 68A113145-2004 68A1131452004 | 1560-01-337-3453 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15 Material: Aluminum alloy 7075 Aircraft Location: Angle, splice;lower hinge beam, trailing edge closure rib | Boeing Company, The (76301) | |
| 68A113146-2005 68A1131462005 | 1560-01-064-7875 | Cover, Access | Material: Aluminum alloy Securing Device Type: Threaded fastener | Boeing Company, The (76301) | |
| 68A113146-2006 68A1131462006 | 1560-01-064-7876 | Cover, Access | Material: Aluminum alloy Securing Device Type: Threaded fastener | Boeing Company, The (76301) |