- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 408-0026
- Year built
- 2023
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- December 14, 2023
- Certificate issued
- January 26, 2024
- Expires
- January 31, 2031
- Mode S code
- AA5C1C
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 N767FXMatched 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 N767FXMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR COEA2026101212767Skin · crackedDURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK ON THE RT UPPER WING SKIN BETWEEN WS 224.32 AND WS 241.68. OPENSDR COEA2026101211767Skin · crackedDURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK IN THE LT UPPER WING SKIN BETWEEN WS 157.95 AND WS 142.30. OPENSDR COEA2024032610767Skin · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS DISCOVERED IN THE #2 ENGINE R/H OUTBOARD ACCESSORY PANEL SKIN AROUND 1/4 TURN FASTENER. #2 R/H OUTBOARD ACCESSORY PANEL SKIN REPAIRED VIA REPLACEMENT AS NEEDED IAW C408 SPM 20-50-00 AND C408 IPC 54-10-00 SDR COEA2024013005767Longeron · crackedWO 254814 NR 6 DISCREPANCY: DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED ON THE L/H NACELLE UNDER THE INERTIAL SEPERATOR MOUNTING POINT, INBOARD SIDE. (LONGERON). REPAIRED COWLING WAS REINSTALLED IAW C408 MM 71-10-15.SDR COEA2024013004767Support Bracket · crackedWO 254814 NR 6 DISCREPANCY: DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED ON THE L/H NACELLE UNDER THE INERTIAL SEPERATOR MOUNTING POINT, INBOARD SIDE. LONGERON SUPPORT BRACKET. REPAIRED COWLING REINSTALLED IAW C408 MM 71-10-15.
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.