Safety record in brief:1 NTSB accident (substantial damage, Apr 2013)4 ADs may apply3 service difficulty reports
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Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The loss of engine power due to fuel starvation for reasons that could not be determined because a postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN13LA245)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-05-16 | Reciprocating Engine Power Section | Mar 15, 2023 | Engine (IO-550-B) |
| 2022-04-04 | Reciprocating Engine Oil System | Mar 29, 2022 | Engine (IO-550-B)Only with: F&M Enterprises, Inc. or Stratus Tool Technologies, LLC oil filter adapter installed per STC SE8409SW, SE09356SC, or SE10348SC. |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO-550-B)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 2009-15-01 | Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft… | Jul 27, 2009 | Airframe (G36)Certain serial numbers: G36 E-3630; G36 E-3636–E-3817; G36 E-3819–E-3834; G36 E-3836–E-3887; G36 E-3889–E-3896; G36 E-3898; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
NR 1 CYLINDER HEAD CRACKED FROM THE SPARK PLUG HOLE TO THE INTAKE VALVE SEAT AND LEAKING EXHAUST EXTERNALLY.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE PILOT REPORTED A "POP" AS HE WAS GROUND HANDLING THE AIRCRAFT ON THE RAMP (IN A STRAIGHT DIRECTION USING AN AIRTUG). FURTHER INVESTIGATION REVEALED 1 NUT/BOLT COMBINATION HAD SHEARED ON THE INBOARD WHEEL HALF OF THE RIGHT HAND MAIN LANDING GEAR ASSEMBLY. THE BOLT HAD SUBSEQUENTLY BACK OUT…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE PILOT REPORTED A "POP" AS HE WAS GROUND HANDLING THE AIRCRAFT ON THE RAMP (IN A STRAIGHT DIRECTION USING AN AIRTUG). FURTHER INVESTIGATION REVEALED 1 NUT/BOLT COMBINATION HAD SHEARED ON THE INBOARD WHEEL HALF OF THE RIGHT MAIN LANDING GEAR ASSEMBLY. THE BOLT HAD SUBSEQUENTLY BACK OUT…
From FAA Service Difficulty Reports; matched by N-number and serial number.