Airframe Structural Components: 16T7232-11, 16T7241-23, 16T7241-43
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16T7232-11 16T723211 | 1560-01-079-7677 | Support, Structural Component, Air | III End Item Identification: Acft model F-16 Special Features: Alum alloy 7075-T73 per QQ-A-367 comp 7075, temper T73, verify heat treat per NDTS1500 | Lockheed Martin Corporation (81755) | |
| 16T7232-15 16T723215 | 1560-01-079-7677 | Support, Structural Component, Air | III End Item Identification: Acft model F-16 Special Features: Alum alloy 7075-T73 per QQ-A-367 comp 7075, temper T73, verify heat treat per NDTS1500 | Lockheed Martin Corporation (81755) | |
| 16T7232-17 16T723217 | 1560-01-079-7677 | Support, Structural Component, Air | III End Item Identification: Acft model F-16 Special Features: Alum alloy 7075-T73 per QQ-A-367 comp 7075, temper T73, verify heat treat per NDTS1500 | Lockheed Martin Corporation (81755) | |
| 16T7232-19 16T723219 | 1560-01-436-4517 | Fitting, Structural Component, Air | III End Item Identification: F-16 falcon aircraft Aircraft Mission Design Series: F-16 Special Features: Hinge support, rudder-rib NO.4 vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7233-11 16T723311 | 1560-01-050-9315 | Hinge Support | III End Item Identification: Acft model F-16 General Characteristics Item Description: C/O forging P/N 16T7233-7, material 7075-T73 al per QQ-A-367 comp 7075 temper T73, verify heat treat per NDTS1500 | Lockheed Martin Corporation (81755) | |
| 16T7234-11 16T723411 | 1560-01-050-9316 | Hinge Support | III End Item Identification: Acft model F-16 General Characteristics Item Description: C/O forging P/N 16T7234-7, material 7075-T73 al per QQ-A-367 comp 7075 temper T73, verify heat treat per NDTS1500 | Lockheed Martin Corporation (81755) | |
| 16T7235 | 1560-01-476-2825 | Support, Structural Component, Air | Lockheed Martin Corporation (81755) | ||
| 16T7235-11 16T723511 | 1560-01-050-9317 | Hinge Support | III End Item Identification: Acft model F-16 General Characteristics Item Description: C/O forging P/N 16T7235-7, material 7075-T73 al per QQ-A-367 comp 7075 temper T73, verify heat treat per PDTS1500 | Lockheed Martin Corporation (81755) | |
| 16T7235-13 16T723513 | 1560-01-476-2825 | Support, Structural Component, Air | Dunn H M Company L.P (64666) Lockheed Martin Corporation (81755) | ||
| 16T7240-17 16T724017 | 1560-01-043-0868 | Frame Assembly, Dorsal | III End Item Identification: Acft model F-16A&B General Characteristics Item Description: Consists of frame P/N 16T7241-25, and attaching hardware, effectivity 0004-ON, nha 16T7240 III Functional Description: Located station 368.10 to 444.40 | Lockheed Martin Corporation (81755) | |
| 16T7240-19 16T724019 | 1560-01-043-0869 | Frame Assembly, Dorsal | III End Item Identification: Acft model F-16A&B General Characteristics Item Description: Consists of frame P/N 16T7241-29 and attaching hardware, effectivity 0004-ON, nha 16T7240-3 III Functional Description: Located station 368.10 to 444.40 | Lockheed Martin Corporation (81755) | |
| 16T7240-49 16T724049 | 1560-01-164-5973 | Plate, Structural, Aircraft | III End Item Identification: F-16 aircraft Special Features: C/O-frame assy, cover, rubber sheet, support, sealant, adhesive;replaces -19;LOCATION-FROM fs 427.00 to fs 436.50;PART of-dorsal insl-fs 368.10 to 444.40 (Non-Core Data) Supplementary Features: Frame assy | Lockheed Martin Corporation (81755) | |
| 16T7240-51 16T724051 | 1560-01-164-5974 | Plate, Structural, Aircraft | III End Item Identification: F-16 aircraft Special Features: C/O-frame, rubber sheet, hardware;replaces -17;LOCATION-FS 417.40 to fs 427.00;PART of dorsal installation, fs 368.10 to 444.40 (Non-Core Data) Supplementary Features: Frame assy | Lockheed Martin Corporation (81755) | |
| 16T7240-7 16T72407 | 1560-01-043-0868 | Frame Assembly, Dorsal | III End Item Identification: Acft model F-16A&B General Characteristics Item Description: Consists of frame P/N 16T7241-25, and attaching hardware, effectivity 0004-ON, nha 16T7240 III Functional Description: Located station 368.10 to 444.40 | Lockheed Martin Corporation (81755) | |
| 16T7240-9 16T72409 | 1560-01-043-0869 | Frame Assembly, Dorsal | III End Item Identification: Acft model F-16A&B General Characteristics Item Description: Consists of frame P/N 16T7241-29 and attaching hardware, effectivity 0004-ON, nha 16T7240-3 III Functional Description: Located station 368.10 to 444.40 | Lockheed Martin Corporation (81755) | |
| 16T7241-23 16T724123 | 1560-01-043-0870 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Effectivity 0001 on, nha 16T7240-3 Material: Aluminum alloy | Lockheed Martin Corporation (81755) | |
| 16T7241-27 16T724127 | 1560-01-043-0871 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Nha 16T7240-3;EFF -0001 on Material: Aluminum alloy | Master Lubricants Co. Inc. (76227) | |
| 16T7241-27S 16T724127S | 1560-01-043-0871 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Nha 16T7240-3;EFF -0001 on Material: Aluminum alloy | Master Lubricants Co. Inc. (76227) | |
| 16T7241-31 16T724131 | 1560-01-044-9347 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Frame;stock SIZE-.063 X 12 X 20 in;finish A403; nha 16T7241-5;EFF 0002 on Material: Aluminum alloy | Lockheed Martin Corporation (81755) | |
| 16T7241-43 16T724143 | 1560-01-044-9348 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Superseding P/N 16T7241-47, I/C code ni, ecn 33179, nha P/N 16T7241-803, finish A403 Material: Aluminum alloy | Lockheed Martin Corporation (81755) |