Airframe Structural Components: 16T7241-47, 16T7242-804, 16T7243-803
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16T7241-47 16T724147 | 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) | |
| 16T7241-49 16T724149 | 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) | |
| 16T7241-5 16T72415 | 1560-01-043-0872 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: C/O -31, -33, -35, -45 clips, rivet, -31 frame; frame matl al alloy per QQ-A-250/4-T62, finish A403; frame stock size - 0.063 X 12 X 20 in; nha P/N 16T7240-3, eff 0001 on Aircraft Location: Frame assembly, fairing-forward dorsal | Lockheed Martin Corporation (81755) | |
| 16T7241-803 16T7241803 | 1560-01-043-0873 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: C/O -39 clip, -49 frame, rivet; frame stock size 0.063 X 12 X 20; matl of frame - aluminum alloy per QQ-A-250/4-T62, finish A403; nha P/N 16T7240-3; eff -0007 on Aircraft Location: Frame assembly, fairing-forward dorsal | Lockheed Martin Corporation (81755) | |
| 16T7241-805 16T7241805 | 1560-01-043-0873 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: C/O -39 clip, -49 frame, rivet; frame stock size 0.063 X 12 X 20; matl of frame - aluminum alloy per QQ-A-250/4-T62, finish A403; nha P/N 16T7240-3; eff -0007 on Aircraft Location: Frame assembly, fairing-forward dorsal | Lockheed Martin Corporation (81755) | |
| 16T7241-807 16T7241807 | 1560-01-043-0873 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: C/O -39 clip, -49 frame, rivet; frame stock size 0.063 X 12 X 20; matl of frame - aluminum alloy per QQ-A-250/4-T62, finish A403; nha P/N 16T7240-3; eff -0007 on Aircraft Location: Frame assembly, fairing-forward dorsal | Lockheed Martin Corporation (81755) | |
| 16T7242-5 16T72425 | 1560-01-051-0447 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: C/O skin P/N 16T7242-7, skin P/N 16T7242-9, buildup P/N 16T7242-1, core P/N 16T7242-13, core P/N 16T7242-15, core P/N 16T7242-19, as required adhesive, superseding P/N 16T7242-803, I/C code ow, ecn 40352, nha 16B7240-3 | Lockheed Martin Corporation (81755) | |
| 16T7242-6 16T72426 | 1560-01-051-0448 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: C/O skin P/N 16T7242-7, skin P/N 16T7242-9, buildup P/N 16T7242-1, core P/N 16T7242-14, core P/N 16T7242-16, core P/N 16T242-18, core P/N 16T7242-20, as required adhesive, superseding P/N 16T7242-804, I/C code ow, ecn 40352, nha 16T7240-3 | Lockheed Martin Corporation (81755) | |
| 16T7242-802 16T7242802 | 1560-01-051-0448 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: C/O skin P/N 16T7242-7, skin P/N 16T7242-9, buildup P/N 16T7242-1, core P/N 16T7242-14, core P/N 16T7242-16, core P/N 16T242-18, core P/N 16T7242-20, as required adhesive, superseding P/N 16T7242-804, I/C code ow, ecn 40352, nha 16T7240-3 | Lockheed Martin Corporation (81755) | |
| 16T7242-803 16T7242803 | 1560-01-051-0447 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: C/O skin P/N 16T7242-7, skin P/N 16T7242-9, buildup P/N 16T7242-1, core P/N 16T7242-13, core P/N 16T7242-15, core P/N 16T7242-19, as required adhesive, superseding P/N 16T7242-803, I/C code ow, ecn 40352, nha 16B7240-3 | Lockheed Martin Corporation (81755) | |
| 16T7242-804 16T7242804 | 1560-01-051-0448 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: C/O skin P/N 16T7242-7, skin P/N 16T7242-9, buildup P/N 16T7242-1, core P/N 16T7242-14, core P/N 16T7242-16, core P/N 16T242-18, core P/N 16T7242-20, as required adhesive, superseding P/N 16T7242-804, I/C code ow, ecn 40352, nha 16T7240-3 | Lockheed Martin Corporation (81755) | |
| 16T7242-805 16T7242805 | 1560-01-071-8342 | Panel, Structural, Aircraft | Special Features: C/O 2 ea skin, buildup, as required adhesive and sealer, superseded P/N 16T7242-803, effectivity 0028-ON, ecn 52898, nha 16T7240-5 | Lockheed Martin Corporation (81755) | |
| 16T7242-806 16T7242806 | 1560-01-080-3083 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: P/N 16T7240 Aircraft Location: Dorsal installation | Lockheed Martin Corporation (81755) | |
| 16T7242-807 16T7242807 | 1560-01-160-5484 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: Replaces -805 Aircraft Location: Access cover, hydraulic accumulator, dorsal | Aerospace & Commerical Technologies (1XKR3) Hellenic Aerospace Industry LTD. (G0808) Hellenic Aerospace Industry SA EAV (5U422) Lockheed Martin Corporation (81755) Sonaca SA (B0128) Tusas Havacilik VE Uzay SAN.A.S. (T0544) | |
| 16T7242-808 16T7242808 | 1560-01-160-5485 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: Replaces -806 Aircraft Location: Access cover, hydraulic accumulator dorsal | Hellenic Aerospace Industry LTD. (G0808) Hellenic Aerospace Industry SA EAV (5U422) Lockheed Martin Corporation (81755) Sonaca SA (B0128) Tusas Havacilik VE Uzay SAN.A.S. (T0544) | |
| 16T7243-1 16T72431 | 1560-01-071-8382 | Leading Edge, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: 16T7243-803 supercedes -801 TWO-WAY;NHA-16T7240-805;EFF ON-61 0028 0568, 61 0570 0577, 61 0579 0656, 61 0657 9999, 61 0007 0568, 61 0570 0577, 61 0579 9999 | Lockheed Martin Corporation (81755) | |
| 16T7243-3 16T72433 | 1560-01-071-8382 | Leading Edge, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: 16T7243-803 supercedes -801 TWO-WAY;NHA-16T7240-805;EFF ON-61 0028 0568, 61 0570 0577, 61 0579 0656, 61 0657 9999, 61 0007 0568, 61 0570 0577, 61 0579 9999 | Lockheed Martin Corporation (81755) | |
| 16T7243-5 16T72435 | 1560-01-071-8382 | Leading Edge, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: 16T7243-803 supercedes -801 TWO-WAY;NHA-16T7240-805;EFF ON-61 0028 0568, 61 0570 0577, 61 0579 0656, 61 0657 9999, 61 0007 0568, 61 0570 0577, 61 0579 9999 | Lockheed Martin Corporation (81755) | |
| 16T7243-5 16T72435 | 1560-01-073-7528 | Leading Edge, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: C/o: edge 1 ea P/N 16T7243-7, web 1 ea P/N 16T7243-15, adhesive ar, red P/N 16T7243-9, eff 0018-0027, nha 16T7240-5 | Lockheed Martin Corporation (81755) | |
| 16T7243-801 16T7243801 | 1560-01-071-8382 | Leading Edge, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: 16T7243-803 supercedes -801 TWO-WAY;NHA-16T7240-805;EFF ON-61 0028 0568, 61 0570 0577, 61 0579 0656, 61 0657 9999, 61 0007 0568, 61 0570 0577, 61 0579 9999 | Lockheed Martin Corporation (81755) | |
| 16T7243-803 16T7243803 | 1560-01-071-8382 | Leading Edge, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: 16T7243-803 supercedes -801 TWO-WAY;NHA-16T7240-805;EFF ON-61 0028 0568, 61 0570 0577, 61 0579 0656, 61 0657 9999, 61 0007 0568, 61 0570 0577, 61 0579 9999 | Lockheed Martin Corporation (81755) |