Airframe Structural Components: 68A230082-2003, 68A230098-2031, 68A230152-2005
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 68A230082-2003 68A2300822003 | 1560-01-204-7515 | Support, Structural Component, Air | III End Item Identification: F-15 acft Special Features: Closure, vertical stabilizer-rear spar | Boeing Company, The (76301) | |
| 68A230088-2001 68A2300882001 | 1560-01-482-8588 | Rib, Airfoil | Aircraft Mission Design Series: F-15A, b, C, D, dj, J Special Features: Next higher assembly 68A230091, U/O F-15A blk 1 abd UP;F-15B cum 1 and UP;F-15C cum 1 and UP;F-15D cum 1 and UP;F-15DJ cum 1 and UP;F-15J cum 1 and up Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A230091-1015 68A2300911015 | 1560-01-161-5638 | Box Assembly | III End Item Identification: F-15 aircraft General Characteristics Item Description: Upper, aft box, vertical stabilizer;c/O skin 2, filler, block, rib, mounting 2, block 2, conduit, hardware | Boeing Company, The (76301) | |
| 68A230091-1017 68A2300911017 | 1560-01-161-5638 | Box Assembly | III End Item Identification: F-15 aircraft General Characteristics Item Description: Upper, aft box, vertical stabilizer;c/O skin 2, filler, block, rib, mounting 2, block 2, conduit, hardware | Boeing Company, The (76301) | |
| 68A230091-1019 68A2300911019 | 1560-01-161-5638 | Box Assembly | III End Item Identification: F-15 aircraft General Characteristics Item Description: Upper, aft box, vertical stabilizer;c/O skin 2, filler, block, rib, mounting 2, block 2, conduit, hardware | Boeing Company, The (76301) | |
| 68A230091-2007 68A2300912007 | 1560-01-481-9280 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-15 Special Features: Dim. are stock material; U/O F-15A CUM223&UP, F-15B CUM36&UP, F-15C CUM1&UP, F-15D CUM1&UP, F-15E CUM1-67 Material: Aluminum alloy 5052 | Boeing Company, The (76301) | |
| 68A230091-2027 68A2300912027 | 1560-01-423-4299 | Skin, Aircraft | Aircraft Mission Design Series: F-15E Material: Aluminum alloy 2024 Aircraft Location: Skin-upper aft box-vertical stabilizer | Boeing Company, The (76301) | |
| 68A230091-2028 68A2300912028 | 1560-01-423-4300 | Skin, Aircraft | Aircraft Mission Design Series: F-15E Material: Aluminum alloy 2024 Aircraft Location: Skin-upper aft box-vertical stabilizer | Boeing Company, The (76301) | |
| 68A230094-2005 68A2300942005 | 1560-01-235-9350 | Rib, Airfoil | Aircraft Mission Design Series: F-15 Special Features: 6AL-4V; nha 68A230000 Material: Titanium alloy | Boeing Company, The (76301) | |
| 68A230097-2003 68A2300972003 | 1560-01-235-9333 | Plate, Structural, Aircraft | III End Item Identification: F-15 Material: Titanium alloy Aircraft Location: Vertical stabilizer | Boeing Company, The (76301) | |
| 68A230098-2031 68A2300982031 | 1560-01-238-6511 | Rib, Airfoil | Aircraft Mission Design Series: F-15 Special Features: Cond 0 alclad Material: Aluminum alloy 2024 | Airborne Technologies Inc. (58730) Boeing Company, The (76301) Kent Associates Inc. (8R034) Triumph Fabrications-Hot Springs (3H339) | |
| 68A230100-2001 68A2301002001 | 1560-01-235-9336 | Plate, Structural, Aircraft | III End Item Identification: F-15 Special Features: Splice angle | Boeing Company, The (76301) | |
| 68A230100-2002 68A2301002002 | 1560-01-235-9335 | Plate, Structural, Aircraft | III End Item Identification: F-15 Special Features: Splice angle | Boeing Company, The (76301) | |
| 68A230108-2003 68A2301082003 | 1560-01-482-0002 | Support, Structural Component, Air | Aircraft Mission Design Series: F-15A, b, C, D Special Features: Next higher assembly 68A230091 U/O F-15A cum 223 and UP;F-15B cum 36 and UP;F-15C cum 1 and UP;F-15D cum 1 and up Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A230113-2005 68A2301132005 | 1560-01-204-7516 | Support, Structural Component, Air | III End Item Identification: F-15 acft Special Features: Closure, vertical stabilizer-leading edge and front spar, lower forward box | Boeing Company, The (76301) | |
| 68A230124-1005 68A2301241005 | 1560-01-007-7188 | Shell Subassembly, Vertical Stabi | III End Item Identification: Aircraft, model F&15 | Boeing Company, The (76301) | |
| 68A230124-2007 68A2301242007 | 1560-00-335-6757 | Shell Subassembly, Vertical Stabi | III End Item Identification: Aircraft, model F15 General Characteristics Item Description: Steel, MIL-S-6721, composition ti, condition tn, annealed | Boeing Company, The (76301) | |
| 68A230151-2019 68A2301512019 | 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) | |
| 68A230151-2025 68A2301512025 | 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) | |
| 68A230152-2005 68A2301522005 | 1560-01-204-6304 | Plate, Structural, Aircraft | III End Item Identification: F-15 acft Special Features: Closure: vertical stabilizer-leading edge and front spar, forward box | Boeing Company, The (76301) |