# N759FX: 2023 Textron 408 - Status: Valid registration - Airframe: [Textron 408](https://openairdocs.org/model/textron-408) (registry code 2076527, 2 seats) - Engine: [P&Wc PT6A-65SC](https://openairdocs.org/engine/p-wc-pt6a-65sc) (registry code 51759) - Data sheets: [TCDS A00016WI](https://openairdocs.org/tcds/A00016WI) (Textron Aviation Inc.), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 408-0015 - Year built: 2023 - Type: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: May 31, 2023 - Certificate issued: July 13, 2023 - Expires: July 31, 2030 - Mode S code: AA3C0B - Registered owner: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0254° N, 89.7893° W: Placed by OpenAirDocs at the center of ZIP code 38125, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=759FX - Page: https://openairdocs.org/aircraft/N759FX From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 2 in force ### Matched by airframe (Textron 408) - [AD 2026-14-10](https://openairdocs.org/ad/2026-14-10): Vertical Stabilizer Structure, Horizontal Stabilizer Structure · Textron 408. Effective Aug 18, 2026 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 ### Matched by engine (P&Wc PT6A-65SC) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N759FX. ## FAA accident and incident reports None matched to N759FX. ## Service difficulty reports (12) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COEA2026100810759](https://openairdocs.org/sdr/COEA2026100810759), Aug 5, 2026: STRINGER. DAMAGED. ON SKIN REMOVAL, FOUND OVERSIZED HOLE IN FRAME 3, ON STRINGER 13L. FREEZE BUSHING REPAIR TO OVERSIZED HOLE, FRAME 3, ON STRINGER 13L IAW FR-408-00-15-54161. - [SDR COEA2026101314759](https://openairdocs.org/sdr/COEA2026101314759), Jun 19, 2026: SKIN. DAMAGED. PERMANENT REPAIR OF L/H NOSE SKIN AND L/H DOOR DRIP CAP DAMAGE. PERMANENT REPAIR COMPLETED IAW DQ51100M2. - [SDR COEA2026010601759](https://openairdocs.org/sdr/COEA2026010601759), Jan 5, 2026: LEAD. FAULTED. FLIGHT 8658, ENROUTE: SMF - CEC AIR TURNBACK, RECURRING AMBER PROP HEAT L CAS MESSAGE MIDWAY TO CEC DURING ICING CONDITIONS. AIRCRAFT RETURNED TO SMF. NO EMERGE - [SDR COEA2025110616759](https://openairdocs.org/sdr/COEA2025110616759), Oct 30, 2025: LINK. CORRODED. WO 271980 NR 5 MINOR REPAIR/DISCREPANCY: RT ENGINE AFT DOOR LINK ASSY FRETTED AROUND CHAMBERED AREA. REPLACED RT AFT INERTIAL SEPERATOR DOOR LINK ASSY REF IPC 3 - [SDR COEA2025110615759](https://openairdocs.org/sdr/COEA2025110615759), Oct 30, 2025: LINK. CORRODED. WO 271980 NR 3 MINOR REPAIR/DISCREPANCY: LT ENGINE AFT DOOR LINK ASSY FRETTED AROUND CHAMBERED AREA. CORRECTIVE ACTION: REPLACED L/H AFT INERTIAL SEPERATOR DOOR - [SDR COEA2025110614759](https://openairdocs.org/sdr/COEA2025110614759), Oct 30, 2025: LINK. CRACKED. WO 271980 NR 2 MINOR REPAIR/DISCREPANCY: R/H ENGINE FWD DOOR LINK ASSY IS CRACKED. REPLACED FWD INERTIAL SEPERATOR DOOR LINK ASSY REF C408 IPC 30-20-05 FIG 1-5. - [SDR COEA2025082106759](https://openairdocs.org/sdr/COEA2025082106759), Aug 20, 2025: SEAT. CRACKED. CAPTAIN SEAT BROKEN, FOAM UNDER CUSHION CRACKED. REPLACED WITH NEW CREW SEAT REF. MM 25-71-05. - [SDR COEA2024110633759](https://openairdocs.org/sdr/COEA2024110633759), Nov 1, 2024: SKIN. CRACKED. DURING A DETAILED VISUAL INSPECTION OF THE UPPER VERTICAL STABILIZER FAIRING R/H SIDE CRACK. REPLACED WITH NEW PER SRM 51-40-05 REV. 4. - [SDR COEA2024110632759](https://openairdocs.org/sdr/COEA2024110632759), Nov 1, 2024: SKIN. DAMAGED. WO 262496 NR 1 DISCREPANCY: DURING A DETAILED VISUAL INSPECTION OF THE UPPER VERTICAL STABILIZER INNER AND EXTERIOR STRUCTURE PULLED THROUGH HARDWARE ON FORWARD - [SDR COEA2024110631759](https://openairdocs.org/sdr/COEA2024110631759), Nov 1, 2024: CLOSEOUT PANEL. CRACKED. DURING A DETAILED VISUAL INSPECTION OF THE UPPER VERTICAL STABILIZER INNER AND EXTERIOR STRUCTURE A CRACK WAS FOUND ON THE VERTICAL STABILIZER CLOSEOUT PANEL LH - [SDR COEA2024051415759](https://openairdocs.org/sdr/COEA2024051415759), May 10, 2024: ACCESS PANEL. CRACKED. DURING A SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE DISCOVERED ON THE L/H ENGINE AFT INBOARD ACCESSORY PANEL 421CR. A TEMPORARY REPAIR WAS PERFORMED ON THE L - [SDR COEA2024041213759](https://openairdocs.org/sdr/COEA2024041213759), Apr 11, 2024: PANEL. CRACKED. DURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS FOUND ON THE R/H ENGINE AFT OUTBOARD ACCESSORY PANEL. A TEMPORARY REPAIR WAS PERFORMED ON THE R/H ENGINE ## STCs that may be installed (OpenAirDocs) (2) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Textron 408) - [STC SA02825LA](https://openairdocs.org/stc/SA02825LA): Installation of a Unit Load Device (ULD), including pallet, net, and container. Satco Inc - [STC SA04553AT](https://openairdocs.org/stc/SA04553AT): Installation of a Bulk Load Cargo Handling System, P/N 73604-101,. Telair US, LLC ## Earlier aircraft with N759FX The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N759FX before. - [Cancelled 2001-05-08](https://openairdocs.org/deregistered/N759FX-2001-05-08): Cessna 208B, S/N 208B0542. Exported to Canada. Owner: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) ## Related - Other Textron 408 aircraft: https://openairdocs.org/model/textron-408/aircraft.md - The P&Wc PT6A-65SC engine: https://openairdocs.org/engine/p-wc-pt6a-65sc.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.