- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 408-0015
- Year built
- 2023
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- May 31, 2023
- Certificate issued
- July 13, 2023
- Expires
- July 31, 2030
- Mode S code
- AA3C0B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 2
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2023 | 1 |
|---|---|
| 2026 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N759FXMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Textron 408 aircraft
FAA incident reports
No FAA accident or incident reports matched to N759FXMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Textron 408 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR COEA2026100810759Stringer · damagedON 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 COEA2026101314759Skin · damagedPERMANENT REPAIR OF L/H NOSE SKIN AND L/H DOOR DRIP CAP DAMAGE. PERMANENT REPAIR COMPLETED IAW DQ51100M2.SDR COEA2026010601759Lead · faultedFLIGHT 8658, ENROUTE: SMF - CEC AIR TURNBACK, RECURRING AMBER PROP HEAT L CAS MESSAGE MIDWAY TO CEC DURING ICING CONDITIONS. AIRCRAFT RETURNED TO SMF. NO EMERGENCY WAS DECLARED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT NR 3 PROP LEAD. SDR COEA2025110616759Link · corrodedWO 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 30-20-05 FIG 1-5.SDR COEA2025110615759Link · corrodedWO 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 LINK ASSY. REF IPC 30-20-05 FIG 1-5.SDR COEA2025110614759Link · crackedWO 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 COEA2025082106759Seat · crackedCAPTAIN SEAT BROKEN, FOAM UNDER CUSHION CRACKED. REPLACED WITH NEW CREW SEAT REF. MM 25-71-05.SDR COEA2024110633759Skin · crackedDURING 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 COEA2024110632759Skin · damagedWO 262496 NR 1 DISCREPANCY: DURING A DETAILED VISUAL INSPECTION OF THE UPPER VERTICAL STABILIZER INNER AND EXTERIOR STRUCTURE PULLED THROUGH HARDWARE ON FORWARD ATTACHMENT POINTS. REPLACED WITH NEW PER TEXTRON AVIATION 408 SRM 51-40-05 REV. 4.SDR COEA2024110631759Closeout Panel · crackedDURING A DETAILED VISUAL INSPECTION OF THE UPPER VERTICAL STABILIZER INNER AND EXTERIOR STRUCTURE A CRACK WAS FOUND ON THE VERTICAL STABILIZER CLOSEOUT PANEL LH FASTENER HOLE JUST AFT OF FWD ATTACHMENT POINTS. CRACK ON THE VERTICAL STABILIZER CLOSEOUT PANEL LHSDR COEA2024051415759Access Panel · crackedDURING 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/H ENGINE AFT INBOARD ACCESSORY PANEL PER TEXTRON REF: DQ44226M1. REPLACED THE L/H ENGINE AFT INBOASDR COEA2024041213759Panel · crackedDURING 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 AFT OUTBOARD ACCESSORY PANEL PER TEXTRON DOCUMENT REF: DQ428170M2. REPLACED THE R/H ENGINE AFT OUTB
STCs that may be installed · 2
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Earlier aircraft with this N-number · 1
This aircraft carried N759FX before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.