N747FX

CESSNA 208B · 1996 · Fixed-wing single-engine · 1 engine · 12 seats · Valid Registration

Registered owner: FEDERAL EXPRESS CORPORATION, TN (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
CSA Air, Inc. (SBAA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

3 reports on file, 2013-02-25 – 2013-04-23.

OTHER · 2013-04-23 Matched by certificate designator
ATA 3010

Part: VALVE — FAULTY (ZONE 600) · airframe 7,549 hrs · 7,605 cycles

FOUND PROPORTIONING VALVE MALFUNCTIONING. INTERNAL CHECK VALVE INOP, LETTING FLUID IN LINES TO PANELS BLEED BACK INTO TANK. IAW OPS CHECK, THE CHECK CAN BE DONE 3 TIMES. THE VALVE FAILED EACH TIME. REPLACED VALVE WITH ANOTHER NEW VALVE WHICH THEN PASSED THE FLOW CHECK. THIS IS THE PROPORTIONING VALVE IN THE AFT FUSELAGE THAT FEEDS THE RIGHT WING AND STRUT PANELS.

Source: SDR YN8R201304230003
NO TEST · 2013-04-23 Matched by certificate designator
ATA 3010

Part: VALVE — FAULTY (ZONE 600) · airframe 7,549 hrs · 7,605 cycles

DURING FLOW CHECK, FOUND PROPORTIONING VALVE MALFUNCTIONING. INTERNAL CHECK VALVE INOP, LETTING FLUID IN LINES TO PANELS BLEED BACK INTO TANK. IAW OPS CHECK, THE CHECK CAN BE DONE 3 TIMES. THE VALLVE FAILED EACH TIME. REPLACED VALVE WITH ANOTHER NEW VALVE WHICH THEN PASSED THE FLOW CHECK. THIS IS THE PROPORTIONING VALVE IN THE AFT FUSELAGE THAT FEEDS THE STABILIZER PANELS.

Source: SDR YN8R201304230004
OTHER · 2013-02-25 Matched by certificate designator
ATA 5730

Part: PANEL — DEFORMED (LT WING) · airframe 7,544 hrs · 7,604 cycles

DURING VISUAL INSPECTION NOTICED THAT LEFT WING INBOARD AND RIGHT WING INBOARD TKS PANELS WERE SLIGHTLY DEFORMED ALONG LEADING EDGE FROM WS 37.00 TO WS 47.00. TKS PANELS DID NOT APPEAR LOOSE AND SEEMED TO OPERATE NORMALLY.

Source: SDR SBAA2013022700003