Airframe Structural Components: 68A311909-2009, 68A311952-2077, 68A311956-1015
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 68A311909-2009 68A3119092009 | 1560-01-583-4871 | Door, Access, Aircraft | Special Features: SHEET-T81 alclad Material: Aluminum alloy 2024 End Item Identification: F-15 acft | Boeing Company, The (76301) | |
| 68A311915-2001 68A3119152001 | 1560-01-036-2933 | Plate, Doorlatch Pin | III End Item Identification: F-15 acft General Characteristics Item Description: One surface serrated, 0.257 in. dia hole | Boeing Company, The (76301) | |
| 68A311951-1007 68A3119511007 | 1560-01-249-6072 | Door, Access, Aircraft | Special Features: Access to aft avionics l.H. End Item Identification: F-15 acft | Boeing Company, The (76301) | |
| 68A311951-1009 68A3119511009 | 1560-01-249-6072 | Door, Access, Aircraft | Special Features: Access to aft avionics l.H. End Item Identification: F-15 acft | Boeing Company, The (76301) | |
| 68A311951-2071 68A3119512071 | 1560-00-282-1076 | 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) | |
| 68A311951-2073 68A3119512073 | 1560-00-282-1076 | 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) | |
| 68A311951-2085 68A3119512085 | 1560-00-282-1076 | 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) | |
| 68A311951-2091 68A3119512091 | 1560-00-282-1076 | 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) | |
| 68A311951-2131 68A3119512131 | 1560-01-249-1769 | Skin, Aircraft | III End Item Identification: F-15 Aircraft Mission Design Series: F-15 Special Features: P/O door, access, aircraft, aft avionics; cond 0 | Boeing Company, The (76301) | |
| 68A311951-2137 68A3119512137 | 1560-01-249-1769 | Skin, Aircraft | III End Item Identification: F-15 Aircraft Mission Design Series: F-15 Special Features: P/O door, access, aircraft, aft avionics; cond 0 | Boeing Company, The (76301) | |
| 68A311952-1005 68A3119521005 | 1560-01-007-7118 | Door, Access, Aircraft | Securing Device Type: Threaded fastener | Boeing Company, The (76301) | |
| 68A311952-1007 68A3119521007 | 1560-01-007-7118 | Door, Access, Aircraft | Securing Device Type: Threaded fastener | Boeing Company, The (76301) | |
| 68A311952-2069 68A3119522069 | 1560-00-282-1080 | Skin, Aircraft | III End Item Identification: F-15 | Boeing Company, The (76301) | |
| 68A311952-2077 68A3119522077 | 1560-00-282-1080 | Skin, Aircraft | III End Item Identification: F-15 | Boeing Company, The (76301) | |
| 68A311952-2099 68A3119522099 | 1560-00-282-1080 | Skin, Aircraft | III End Item Identification: F-15 | Boeing Company, The (76301) | |
| 68A311952-2129 68A3119522129 | 1560-01-531-0606 | Skin, Aircraft | III End Item Identification: Door, access, aircraft-aft avionics, rh Aircraft Mission Design Series: F-15 acft Special Features: Heat treat T0; per E/O -2133 skin same as (and replacing) -2129 except for enlarging (2) .22 dia drain holes to .25 dia and adding rivet pattern mating with added covers as shown | Boeing Company, The (76301) | |
| 68A311952-2133 68A3119522133 | 1560-00-282-1080 | Skin, Aircraft | III End Item Identification: F-15 | Boeing Company, The (76301) | |
| 68A311952-2135 68A3119522135 | 1560-00-282-1080 | Skin, Aircraft | III End Item Identification: F-15 | Boeing Company, The (76301) | |
| 68A311956-1013 68A3119561013 | 1560-01-435-8555 | Rod Assembly, Cover, Aircraft | Aircraft Mission Design Series: F-15I Special Features: Requestedname:brace, acft ground s;dimension from centerline of clevis P/N 68A311963-2003 to that of pin assembly P/N ST9M553-1A is 15.63 inches; length of tube P/N 68A311956-2001 is 12.63 inches Material: Aluminum alloy 2024 | Boeing Company, The (76301) | |
| 68A311956-1015 68A3119561015 | 1560-01-435-8567 | Rod Assembly, Cover, Aircraft | Aircraft Mission Design Series: F-15I Special Features: Requestedname:brace, acft ground s;dimension from centerline of clevis P/N 68A311963-2003 to that of pin assembly P/N ST9M553-1A is 15.77 inches; length of tube P/N 68A311956-2005 is 12.77 inches Material: Aluminum alloy 2024 | Boeing Company, The (76301) |