Airframe Structural Components: 16T7463-807, 16T7471-9, 16T7482
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16T7463-807 16T7463807 | 1560-01-397-6738 | Fairing, Aircraft | Aircraft Mission Design Series: F-16 Special Features: Horiz stabilizer leading edge | Lockheed Martin Corporation (81755) | |
| 16T7463-9 16T74639 | 1560-01-278-2970 | Support, Structural Component, Air | Aircraft Mission Design Series: F-16A/C | Lockheed Martin Corporation (81755) | |
| 16T7465-10 16T746510 | 1560-01-165-0197 | Skin, Aircraft | Aircraft Mission Design Series: F-16 | Lockheed Martin Corporation (81755) | |
| 16T7465-3 16T74653 | 1560-01-256-2446 | Skin, Aircraft | III End Item Identification: F-16 | Aerospace & Commerical Technologies (1XKR3) CPI Aerostructures Inc. (9U679) Cyclone Aviation Products LTD (S5503) EDO Corp. (32500) Fokker Aircraft B.V. (H0643) Lockheed Martin Corporation (81755) Nordam Group Inc., The (29957) | |
| 16T7465-4 16T74654 | 1560-01-253-5258 | Skin, Aircraft | III End Item Identification: F-16 Aircraft Location: Horizontal stabilizer, nsn 1560011411064WF | Aerospace & Commerical Technologies (1XKR3) CPI Aerostructures Inc. (9U679) Cyclone Aviation Products LTD (S5503) EDO Corp. (32500) Fokker Aircraft B.V. (H0643) Lockheed Martin Corporation (81755) Nordam Group Inc., The (29957) | |
| 16T7466-9 16T74669 | 1560-01-548-9151 | Spar, Aircraft | ACE Clearwater Enterprises Inc. (7N843) Lockheed Martin Corporation (81755) | ||
| 16T7467-803 16T7467803 | 1560-01-265-8451 | Support, Structural Component, Air | III End Item Identification: F-16 aircraft III Supplementary Features: Functional description:shaft, pivot, horizontal stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7469-9 16T74699 | 1560-01-355-5954 | Spar, Aircraft | Aircraft Mission Design Series: F-16A/B/C/D Material: Aluminum alloy 2124 Aircraft Location: Horizontal stabilizer | Aerospace & Commerical Technologies (1XKR3) Arinc Engineering Services LLC (0PN76) Cyclone Aviation Products LTD (S5503) Fokker Aircraft B.V. (H0643) Fokker Services B.V. (H0W98) Lockheed Martin Corporation (81755) Progressive Incorporated (64900) | |
| 16T7470-7 16T74707 | 1560-01-253-7824 | Rib, Airfoil | Aircraft Mission Design Series: F-16 Aircraft Location: Rib, forward foot, horizontal stabilizer | Aerospace Engineering & Support Inc. (1DA92) Craft Manufacturing and Tooling Inc. (0CMM5) Lockheed Martin Corporation (81755) | |
| 16T7471 | 1560-01-500-7910 | Rib, Airfoil | Lockheed Martin Corporation (81755) | ||
| 16T7471-7 16T74717 | 1560-01-500-7910 | Rib, Airfoil | Lockheed Martin Corporation (81755) | ||
| 16T7471-9 16T74719 | 1560-01-434-0352 | Rib, Airfoil | Aircraft Mission Design Series: F-16 Special Features: Metal removal per FPA-3017;FORM part per FPS03018;CONTOUR at horiz. stab. sta. 1.585 ref;models a, b, C, D Material: Aluminum alloy | Lockheed Martin Corporation (81755) | |
| 16T7477-1 16T74771 | 1560-01-457-7779 | Skin, Aircraft | Aircraft Mission Design Series: F-16C/D Special Features: Lefthand Material: Aluminum alloy 2024 | Lockheed Martin Corporation (81755) | |
| 16T7477-10 16T747710 | 1560-01-163-6746 | Skin, Aircraft | III End Item Identification: F-16 Special Features: Kit for all dash numbers this drawing, all layers | Lockheed Martin Corporation (81755) | |
| 16T7477-2 16T74772 | 1560-01-457-7780 | Skin, Aircraft | Aircraft Mission Design Series: F-16C/D Special Features: Righthand Material: Aluminum alloy 2024 | Cyclone Aviation Products LTD (S5503) Lockheed Martin Corporation (81755) | |
| 16T7479 | 1560-01-500-7947 | Rib, Airfoil | Lockheed Martin Corporation (81755) | ||
| 16T7479 | 1560-01-500-7949 | Rib, Airfoil | Lockheed Martin Corporation (81755) | ||
| 16T7479-7 16T74797 | 1560-01-500-7947 | Rib, Airfoil | Lockheed Martin Corporation (81755) | ||
| 16T7479-9 16T74799 | 1560-01-500-7949 | Rib, Airfoil | Lockheed Martin Corporation (81755) | ||
| 16T7480-7 16T74807 | 1560-01-114-0396 | Support, Structural Component, Air | Overall Length: 11.000 inches nominal Overall Width: 7.000 inches nominal Material Thickness: 4.000 inches nominal | Aerospace & Commerical Technologies (1XKR3) Lockheed Martin Corporation (81755) Triumph Structures-LOS Angeles Inc. (6D161) | |
| 16T7482 | 1560-01-488-4094 | Rib, Airfoil | Aircraft Mission Design Series: F-16 Aircraft Location: Rib, tip-horizontal stablizer | Lockheed Martin Corporation (81755) |