Airframe Structural Components: 16W176-30, 16W184-807, 16W184-809
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16W176-30 16W17630 | 1560-01-376-2085 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-16C Special Features: Upper wing skin cover plate Material: Aluminum alloy 2024 | Lockheed Martin Corporation (81755) | |
| 16W176-4 16W1764 | 1560-01-333-7223 | Cover, Access, Aircraft | Special Features: Access-wing box upper, R-H Material: Aluminum alloy 2024 End Item Identification: F-16 acft | Lockheed Martin Corporation (81755) | |
| 16W176-803 16W176803 | 1560-01-335-8087 | Cover, Access, Aircraft | Special Features: Access-wing box upper, l-H Material: Aluminum alloy 2024 End Item Identification: F-16 acft | Lockheed Martin Corporation (81755) | |
| 16W176-804 16W176804 | 1560-01-333-7222 | Cover, Access, Aircraft | Special Features: Access-wing box upper, R-H Material: Aluminum alloy 2024 End Item Identification: F-16 acft | Lockheed Martin Corporation (81755) | |
| 16W177-13 16W17713 | 1560-01-421-6894 | Cover, Access, Aircraft | Special Features: Wing upper access hole plug Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4-T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-15 16W17715 | 1560-01-333-7312 | Cover, Access, Aircraft | Special Features: Wing upper access hole plug Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4-T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-19 16W17719 | 1560-01-421-6892 | Cover, Access, Aircraft | Special Features: Wing upper access hole plug Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4-T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-23 16W17723 | 1560-01-341-7219 | Cover, Access, Aircraft | Special Features: Access-wing, upper surface Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4, T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-29 16W17729 | 1560-01-339-2132 | Cover, Access, Aircraft | Special Features: Access-wing, upper surface Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4, T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-5 16W1775 | 1560-01-315-1303 | Cover, Access, Aircraft | Special Features: Plug, access hole, wing upper surface Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4-T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-803 16W177803 | 1560-01-333-8981 | Cover, Access, Aircraft | Special Features: Wing upper access hole plug Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4-T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-805 16W177805 | 1560-01-339-2130 | Cover, Access, Aircraft | Special Features: Access-wing upper surface; included additional 3.000 in. dia bolt hole circle W/ 6 holes Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4, T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-807 16W177807 | 1560-01-339-2134 | Cover, Access, Aircraft | Special Features: Access-wing, upper surface Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4, T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-809 16W177809 | 1560-01-339-2133 | Cover, Access, Aircraft | Special Features: Access-wing, upper surface; includes additional 3.000 in. dia bolt hole circle W/ 6 holes Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4, T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W177-811 16W177811 | 1560-01-339-2131 | Cover, Access, Aircraft | Special Features: Access-wing, upper surface Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4, T851 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16W184-801 16W184801 | 1560-01-040-9662 | Fairing, Aircraft | III End Item Identification: F-16 | Lockheed Martin Corporation (81755) S.A.B.C.A. SA (B1252) | |
| 16W184-802 16W184802 | 1560-01-042-2106 | Fairing, Aircraft | III End Item Identification: F-16 | Lockheed Martin Corporation (81755) S.A.B.C.A. SA (B1252) | |
| 16W184-807 16W184807 | 1560-01-310-2030 | Fairing, Aircraft | Material Thickness: 0.160 inches nominal Criticality Code Justification: FEAT Aircraft Location: Upper wing root | Aerospace & Commerical Technologies (1XKR3) Cyclone Aviation Products LTD (S5503) Lockheed Martin Corporation (81755) S.A.B.C.A. SA (B1252) | |
| 16W184-808 16W184808 | 1560-01-310-2031 | Fairing, Aircraft | Material Thickness: 0.160 inches nominal Aircraft Location: Upper wing root Aircraft Mission Design Series: F-16C and F-16D | Aerospace & Commerical Technologies (1XKR3) Cyclone Aviation Products LTD (S5503) Korean Air Aerospace (0SEP6) Lockheed Martin Corporation (81755) S.A.B.C.A. SA (B1252) | |
| 16W184-809 16W184809 | 1560-01-356-0748 | Fairing, Aircraft | Aircraft Mission Design Series: F-16C/D Material: Aluminum alloy 2024 Aircraft Location: Upper wing root | Lockheed Martin Corporation (81755) |