N712TA

CIRRUS DESIGN CORP SR20 · 2021 · Fixed-wing single-engine · 1 engine · 4 seats · Valid Registration

Registered owner: RMAG LLC, TX (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.

5 reports on file, 2001-11-12 – 2008-01-21.

ENGINE FLAMEOUT; WARNING INDICATION · 2008-01-21 Matched by certificate designator
ATA 7321

Part: HMU — OUT OF ADJUST (ENGINE) · airframe 7,863 hrs · 6,520 cycles

DURING TAXI, PRIOR TO FLIGHT, WHILE PERFORMING THE EFC AUTHORITY CHECK THE NR1 ENGINE SHUTDOWN. MAINT FOUND THE NR1 HMU OUT OF ADJUSTMENT. THE HMU WAS ADJUSTED IAW THE MM AND THE ENGINE OPERATIONAL CHECK WAS SUCCESSFUL.

Source: SDR DJFA2008006
OTHER · 2007-04-30 Matched by certificate designator
ATA 5310

Part: SUPPORT BEAM — CRACKED (BS 190) · airframe 7,313 hrs · 6,024 cycles

DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A CRACK ON THE SUPPORT BEAM BETWEEN FS 190.35 AND FS 196.46 ON THE RT SIDE. THE CRACK WAS .172 INCHES LONG AND EXTENDED FROM THE CENTER OF THE RADIUS CUT OUT ON THE IB SIDE. MAINTENANCE REPAIRED THE CRACKED STIFFNER.

Source: SDR DJFA2007053
OTHER · 2007-04-26 Matched by certificate designator
ATA 5511

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 7,313 hrs · 6,024 cycles

DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZONTAL STABILIZER, THE LT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NR 70. [SUP 05-21-07] MAINTENANCE REPLACED THE RIB.

Source: SDR DJFA2007051
OTHER · 2004-12-17 Unresolved
ATA 3230

Part: CONNECTOR — LOOSE (MLG)

INVESTIGATED LANDING GEAR RETRACT SYSTEM FAULT (LANDING GEAR WOULD NOT RETRACT WHEN GEAR HANDLE SELECTED (UP) AFTER TAKEOFF) FOUND P162 CONNECTOR LOOSE, NOT FULLY SEATED ON A162 PC BOARD ASSY. J1 CONNECTOR, RESEATED P162 CONNECTOR TO A162J1 CONNECTOR, LANDING GEAR RETRACT/EXTENSION SYSTEM OPERATIONS NORMAL DURING 10 RETRACT/EXTENSION CYCLES. (K)

Source: SDR 2005FA0000703
OTHER · 2001-11-12 Unresolved
ATA 7120

Part: MOUNT — CRACKED (ENGINE)

WHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT TO BE CRACKED.

Source: SDR 2002FA0000013