Airframe Structural Components: 16T7244-25, 16T7251-76, 16T7252-802
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16T7244-25 16T724425 | 1560-01-043-0875 | Fairing, Aircraft | Aircraft Mission Design Series: F-16A & b Aircraft Station Number: FS368.1 to FS408.78 | Lockheed Martin Corporation (81755) | |
| 16T7244-5 16T72445 | 1560-01-077-8113 | Cover, Access | Material: Glass fiber END Item Identification: Acft model F-16A&B FSC Application Data: Used on antenna-dorsal, superseded P/N 16T7244-5, I/C code ow, effectivity 0028-ON, ecn 52898, nha 16T7240-5 | Lockheed Martin Corporation (81755) | |
| 16T7244-7 16T72447 | 1560-01-043-0875 | Fairing, Aircraft | Aircraft Mission Design Series: F-16A & b Aircraft Station Number: FS368.1 to FS408.78 | Aerospace & Commerical Technologies (1XKR3) Lockheed Martin Corporation (81755) | |
| 16T7244-801 16T7244801 | 1560-01-077-8113 | Cover, Access | Material: Glass fiber END Item Identification: Acft model F-16A&B FSC Application Data: Used on antenna-dorsal, superseded P/N 16T7244-5, I/C code ow, effectivity 0028-ON, ecn 52898, nha 16T7240-5 | Camnetics Manufacturing Corporation (0P657) Lockheed Martin Corporation (81755) | |
| 16T7244-803 16T7244803 | 1560-01-160-5430 | Fairing Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: Part of-access cover, antenna, DORSAL;C/O-CORE-2(MATL-PO21-1B, E103 finish), adhesive, BUILDUP-2, SKIN-2, fairing | Lockheed Martin Corporation (81755) | |
| 16T7245-1 16T72451 | 1560-01-043-0876 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: C/O frame material per FMS-1023 cl I P/N 16T7245-9, plug P/N 16T7245-21, as required adhesive, effectivity 0001-ON, nha 16T7240-3 | Lockheed Martin Corporation (81755) | |
| 16T7245-3 16T72453 | 1560-01-043-0877 | Frame Assembly | III End Item Identification: Acft model F-16A&B General Characteristics Item Description: C/O web material fms 1023 cl I P/N 16T7245-11, flange P/N 16T7245-13, angle P/N 16T7245-27, as required compound, rivet, adhesive, effectivity 0003-0003 0005-ON, nha 16T7240-3 | Lockheed Martin Corporation (81755) | |
| 16T7245-5 16T72455 | 1560-01-043-0877 | Frame Assembly | III End Item Identification: Acft model F-16A&B General Characteristics Item Description: C/O web material fms 1023 cl I P/N 16T7245-11, flange P/N 16T7245-13, angle P/N 16T7245-27, as required compound, rivet, adhesive, effectivity 0003-0003 0005-ON, nha 16T7240-3 | Lockheed Martin Corporation (81755) | |
| 16T7246-17 16T724617 | 1560-01-046-4187 | Rib, Airfoil | III End Item Identification: F-16 | Lockheed Martin Corporation (81755) | |
| 16T7246-19 16T724619 | 1560-01-046-9885 | Closure, Rib Assembly | III End Item Identification: Acft model F-16 | Lockheed Martin Corporation (81755) | |
| 16T7246-5 16T72465 | 1560-01-045-4622 | Rib, Airfoil | III End Item Identification: F-16 | Lockheed Martin Corporation (81755) | |
| 16T7246-7 16T72467 | 1560-01-046-9885 | Closure, Rib Assembly | III End Item Identification: Acft model F-16 | Lockheed Martin Corporation (81755) | |
| 16T7251-59 16T725159 | 1560-01-527-5018 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-16 Material: Aluminum alloy 2024 Aircraft Location: Support-dorsal fairing-vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7251-60 16T725160 | 1560-01-527-5015 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-16 Material: Aluminum alloy 2024 Aircraft Location: Support-dorsal fairing-vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7251-75 16T725175 | 1560-01-527-5028 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-16 Material: Aluminum alloy 2024 Aircraft Location: Support-dorsal fairing-vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7251-76 16T725176 | 1560-01-527-5026 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-16 Material: Aluminum alloy 2024 Aircraft Location: Support-dorsal fairing-vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7252-4 16T72524 | 1560-01-050-9340 | Fairing, Stabilizer, Aircraft | III End Item Identification: Acft model F-16A&B Special Features: 1 outer skin 16T7252-8; 1 inner skin 16T7252-10; 3 core; 1 buildup 16T7252-20; 1 buildup 16T7252-24; 46 bushing C9521-10-120; adhesive as required; superseding | Lockheed Martin Corporation (81755) | |
| 16T7252-6 16T72526 | 1560-01-050-9340 | Fairing, Stabilizer, Aircraft | III End Item Identification: Acft model F-16A&B Special Features: 1 outer skin 16T7252-8; 1 inner skin 16T7252-10; 3 core; 1 buildup 16T7252-20; 1 buildup 16T7252-24; 46 bushing C9521-10-120; adhesive as required; superseding | Lockheed Martin Corporation (81755) | |
| 16T7252-801 16T7252801 | 1560-01-078-8197 | Cover, Access, Aircraft | Special Features: Vertical stabilizer root fitting access Material: Glass fiber and aluminum alloy Material Document and Classification: FMS1023 mfr ref 1ST material response and P190-1B mfr ref 2ND material response | Lockheed Martin Corporation (81755) | |
| 16T7252-802 16T7252802 | 1560-01-158-5864 | Cover, Access, Aircraft | Special Features: Vertical stabilizer root fitting access Material: Glass fiber and aluminum alloy Material Document and Classification: FMS1023 mfr ref 1ST material response and P190-1B mfr ref 2ND material response | Lockheed Martin Corporation (81755) |