- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 408-0004
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 29, 2022
- Certificate issued
- January 11, 2023
- Expires
- January 31, 2030
- Mode S code
- A972D9
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 N708FXMatched 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 N708FXMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR COEA2026100109708Skin · crackedEVIDENCE OF A CRACK ON THE R/H WING AFT SIDE TOWARDS THE OUTBOARD PORTION OF THE FLAP. OPENSDR COEA2026100108708Panel · dentedDENT UNDER LT SPONSON PANEL. OPENSDR COEA2026010702708Pressure Switch · faultedFLIGHT 8737, ENROUTE GEG - YKM AIR TURNBACK, DURING CRUISE, THE STAB DE-ICE FAIL ILLUMINATED. DUE TO ICING CONDITIONS, THE PILOT DECLARED AN EMERGENCY AND RETURNED TO GEG WITHOUT INCIDENT. MAINTENANCE REMOVED THE EMPENNAGE PRESSURE SWITCH SV001 AND FOUND RSDR COEA2025081903708Pan · crackedCAPTAIN SEAT SUPPORT PAN CRACKED. MAINTENANCE REPLACED THE CREW SEAT IAW 408 MM 25-10-05.SDR COEA2025080702708Fuel Filter · faultedFLT 8737 GEG-YKM AIR TURNBACK NO EMERGENCY DECLARED. FUEL BYPASS LIGHT TURNED ON DURING CLIMB. MAINTENANCE REPLACED BOTH FUEL HEATER FILTERS. LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR COEA2024071222708Bulkhead · crackedWO 259393 NR 3 DISCREPANCY: R/H ENGINE ACCESSORY PANEL BULKHEAD CRACKED. REPLACED THE BULKHEAD IAW CESSNA 408 SMR SMP.SDR COEA2024061219708Torque Tube · wornWO 258062 NR 3 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION OF THE R/H LOWER COWL INERTIAL SEPERATOR TORQUE TUBE ASSYS, PLAY AND WEAR WAS DISCOVERED ON THE FWD TORQUE TUBE TO OUTBOARD SHAFT FITTING, THE AFT TORQUE TUBE TO R/H ARM ASSY AND THE FWD TORSDR COEA2024061218708Torque Tube · wornDURING A SCHEDULED MAINTENANCE INSPECTION OF THE L/H LOWER COWL INERTIAL SEPERATOR TORQUE TUBE ASSY'S, PLAY AND WEAR WAS DISCOVERED ON THE FWD TORQUE TUBE TO INBOARD SHAFT FITTING, THE FWD TORQUE TUBE TO R/H ARM ASSY AND THE FWD TORQUE TUBE TARGET ARM. REPLASDR COEA2024052917708Longeron · crackedWO 257747 NR 6 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, THE L/H NACELLE INBOARD SIDE LONGERON UNDER THE ICE VANE ATTACH POINT SHOWS SIGNS OF CRACKED STARTING. REPLACED THE L/H LOWER AFT COWLING AND FORWARD INTAKE COWLING REF. MM 71-10-05 AND SDR COEA2024052916708Longeron · crackedWO 257747 NR 5 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, THE R/H NACELLE OUTBOARD SIDE LONGERON IS CRACKED IN BEND RADIUS UNDER THE ICE VANE ACTUATOR ATTACH POINTS. REPLACED THE R/H LOWER AFT COWLING AND FORWARD INTAKE COWLING REF. C408 MM 71-1SDR COEA2024032612708Skin · chafedL/H FLAP LE CHAFING FROM INBOARD FLAP ACTUATOR ACCESS PANEL. L/H PANEL FIT INSTALLED PER C408 SRM 51-00-00 AND C408 IPC 57-20-25. L/H FLAP ACTUATOR PANELS MODIFIED AND INSTALLED IAW SR-408-ATA57-43632 REV A PARA 4.3.3 AND 4.4. OPS CHECK GOOD. NO CONTACT WITH SDR COEA2024032611708Access Panel · chafedR/H FLAP LE CHAFING FROM INBOARD FLAP ACTUATOR ACCESS PANEL. R/H PANEL FIT INSTALLED PER C408 SRM 51-00-00 AND C408 IPC 57-20-25. R/H FLAP ACTUATOR PANELS MODIFIED AND INSTALLED IAW SR-408-ATA57-43632 REV A PARA. 4.3.3 AND 4.4. OPS CHECK GOOD. NO CONTACT WITHSDR COEA2023112902708Unknown · unknownWO 252637/NR 6 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE R/H INTAKE INTERIOR LOWER SURFACE PANEL IS CRACKED. REPLACED THE R/H ENGINE LOWER COWL SKIN IAW 408 SRM CH 51-00-00 AND IPC 71-10-10.SDR COEA2023112901708Exhaust Stack · crackedW/O 252637/NR 8 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE R/H EXHAUST STACK ASSEMBLY BLEED PORT-TO-INLET ANTI-ICE HOSE WELD IS CRACKED. CORRECTIVE ACTION: MAINTENANCE REPLACED THE EXHAUST STACK ASSEMBLY WITH NEW PER C
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 N708FX before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.