N54TJ

CIRRUS DESIGN CORP SF50 · Fixed-wing single-engine · 1 engine · 7 seats · M

Registered owner: CIRRUS DESIGN CORP, MN (owner ≠ operator)

Operators of this aircraft

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

No operator established for this aircraft.

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.

4 reports on file, 2018-11-13 – 2019-01-18.

WARNING INDICATION · 2019-01-18 Matched by certificate designator
ATA 3010

Part: BLEED VALVE — DEFECTIVE · airframe 2,407 hrs · 1,367 cycles

SEVERAL PILOT REPORTS OF THE RH WING ANTI-ICE SYSTEM SLOW TO WORK. THE CURRENT ATTEMPT TO CLEAR THIS FAULT WAS TO SWAP THE LH AND RH BI-LEVEL VALVES FOR TROUBLESHOOTING. OPS AND LEAK CHECKS GOOD NO FURTHER ACTION REQUIRED

Source: SDR 9JLA2019021210734
FALSE WARNING · 2019-01-05 Matched by certificate designator
ATA 7830

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER) · airframe 2,399 hrs · 1,362 cycles

THE FLIGHT CREW REPORTED THAT THE RH THRUST REVERSER UNLOCK LIGHT CONTINUOUSLY FLICKERED IN FLIGHT. TROUBLESHOT AND CHECKED OPERATION OF THE TR STOW SWITCHES FOUND NO DEFECTS, COULD NOT DUPLICATE.

Source: SDR 9JLA2019021210731
OTHER · 2018-11-24 Matched by certificate designator
ATA 2310

Part: ANTENNA — BROKEN (HF COMMS) · airframe 2,360 hrs · 1,344 cycles

DURING THE FLIGHT CREW POST FLIGHT AIRCRAFT CHECKS. IT WAS DISCOVERED THAT THE HF ANTENNA WIRE WAS BROKEN FROM MOUNT AND CAUSED DAMAGED TO THE LH ELEVATOR TRIM TAB

Source: SDR 9JLA2019021221728
WARNING INDICATION · 2018-11-13 Matched by certificate designator
ATA 7510

Part: SENSOR — FAILED (LT ENG ANTI-ICE) · airframe 2,350 hrs · 1,329 cycles

FLIGHT CREW REPORTED THAT THE LH ENGINE ANTI-ICE ANNUNCIATOR WAS SLOW TO EXTINGUISH AFTER SYSTEM WAS ACTIVATED.TROUBLESHOOTING DETERMINED THAT THE LH ENGINE INLET ANTI-ICE TEMP SENSOR WAS DEFECTIVE. THE SWITCH AS REPLACED

Source: SDR 9JLA2019021210727