Airframe Structural Components: 68A230023-2003, 68A230027-2007, 68A230029-2003
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 68A230023-2003 68A2300232003 | 1560-01-239-9039 | Support, Structural Component, Air | III End Item Identification: F-15 aircraft Special Features: Used to prevent collapse of upper 8 in of fwd vertical stab when fasteners are installed; stock size 1.00 thk, 0.82 wide, 1.87 lg with two 0.2495 fastening holes III Supplementary Features: Functional description:block | Airborne Technologies Inc. (58730) Boeing Company, The (76301) Omega Tool Co. (5F247) | |
| 68A230023-2005 68A2300232005 | 1560-01-239-9040 | Support, Structural Component, Air | III End Item Identification: F-15 aircraft Special Features: To prevent collapse of upper 8 in of fwd box on vert stab when fasteners are installed; stock size 1.25 thk, 0.82 wide, 2.79 lg with 3 0.2495 fastening holes III Supplementary Features: Functional description:block | Boeing Company, The (76301) Omega Tool Co. (5F247) | |
| 68A230023-2007 68A2300232007 | 1560-01-239-9041 | Support, Structural Component, Air | III End Item Identification: F-15 aircraft Special Features: Used to prevent collapsing of the upper box of the vertical stabilizer when fasteners are installed; stock size 1.00 thk, 1.25 wide, 7.83 lg with 7 fastening holes 0.1895 dia III Supplementary Features: Functional description:closure block | Boeing Company, The (76301) Jakic Industries Inc. (9M348) Omega Tool Co. (5F247) | |
| 68A230023-2009 68A2300232009 | 1560-01-432-7283 | Support, Structural Component, Air | Aircraft Mission Design Series: F-15 Special Features: Requested name-block uhf; next higher assy 68A230620; U/O FMF-15C 10 and up, FMF-15D 7 and up Material: Aluminum alloy 2124 | Boeing Company, The (76301) | |
| 68A230023-2013 68A2300232013 | 1560-01-478-5916 | Support, Structural Component, Air | Aircraft Mission Design Series: F-15E Special Features: U/O F-15E CUM201&UP Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A230023-2015 68A2300232015 | 1560-01-478-4770 | Support, Structural Component, Air | Aircraft Mission Design Series: F-15E Special Features: Dim. are stock material; U/O F-15E CUM201&UP Material: Aluminum alloy 2124 | Boeing Company, The (76301) | |
| 68A230024-2003 68A2300242003 | 1560-01-246-5610 | Skin, Aircraft | III End Item Identification: F-15 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5-0 fed spec single material response | Boeing Company, The (76301) | |
| 68A230024-2009 68A2300242009 | 1560-01-246-5610 | Skin, Aircraft | III End Item Identification: F-15 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5-0 fed spec single material response | Boeing Company, The (76301) | |
| 68A230025-2001 68A2300252001 | 1560-01-253-7744 | Plate, Structural, Aircraft | III End Item Identification: F-15 Special Features: Cond 0, alclad Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A230025-2003 68A2300252003 | 1560-01-478-4771 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15E, I, s Special Features: Dim. are stock material; U/O F-15E 30&, F-15I CUM1&UP, F-15S CUM1&UP Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A230027-1003 68A2300271003 | 1560-01-467-5639 | Skin, Aircraft | Aircraft Mission Design Series: F-15E Special Features: Next higher assy, 68A230024, U/O F-15E cum 20 and up Material: Titanium alloy and aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A230027-2001 68A2300272001 | 1560-01-240-3577 | Skin, Aircraft | III End Item Identification: F-15 Aircraft Location: Vertical stabilizer, forward box upper | Boeing Company, The (76301) | |
| 68A230027-2003 68A2300272003 | 1560-01-241-8010 | Support, Structural Component, Air | Aircraft Mission Design Series: F-15 Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A230027-2007 68A2300272007 | 1560-01-240-3482 | Plate, Structural, Aircraft | III End Item Identification: F-15 Special Features: Filler Material: Titanium | Boeing Company, The (76301) | |
| 68A230027-2015 68A2300272015 | 1560-01-478-5101 | Channel, Aircraft | Aircraft Mission Design Series: F-15E Special Features: Dim. are stock material; U/O F-15E CUM201 and up Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A230027-2017 68A2300272017 | 1560-01-478-4430 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15E Special Features: Dim. are stock material; U/O F-15E CUM201 and up Material: Titanium alloy | Boeing Company, The (76301) | |
| 68A230027-2019 68A2300272019 | 1560-01-478-2556 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15 Material: Titanium alloy Aircraft Location: Forward box upper vertical stabilizer | Boeing Company, The (76301) | |
| 68A230028-2001 68A2300282001 | 1560-01-204-7526 | Support, Structural Component, Air | III End Item Identification: F-15 acft Special Features: Closure, upper-lower forward box, vertical stabilizer | Boeing Company, The (76301) | |
| 68A230029-2001 68A2300292001 | 1560-01-204-9654 | Support, Structural Component, Air | III End Item Identification: F-15 acft Special Features: Closure, lower-forward box, vertical stabilizer | Boeing Company, The (76301) | |
| 68A230029-2003 68A2300292003 | 1560-01-204-9655 | Support, Structural Component, Air | III End Item Identification: F-15 acft Special Features: Closure, lower-forward box, vertical stabilizer | Boeing Company, The (76301) |