Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Sep 2010)1 AD may apply2 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
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 pilot’s inadequate compensation for the wind and failure to maintain directional control during the takeoff roll.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR10CA444)
A cracked cylinder head which resulted in a loss of engine power while maneuvering. High vegetation was a factor.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA04LA125)
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 |
|---|---|---|---|
| 99-11-02 | Pratt & Whitney R-1340 Series Reciprocating Engines | Jul 19, 1999 | Engine (R1340 SERIES) |
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.
CYLINDER SEPARATED BETWEEN 2ND AND 3RD HORIZONTAL FINS THROUGH THE SPARK PLUG BOSS. ENGINE LOST POWER AND THE AIRCRAFT NOSED OVER ON EMERGENCY LANDING CAUSING SUBSTANTIAL DAMAGE. THIS CYLINDER HAD BEE OVERHAULED THREE PREVIOUS TIMES.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE NUMBER SEVEN CYLINDER HEAD IS CRACKED STARTING AT THE FORWARD SPARK PLUG BOSS RADIATING UP OVER THE TOP OF THE HEAD AND STOPS AT THE AFT SPARK PLUG BOSS. THE CRACK IS OPEN TO AS MUCH AS .0625 INCH, AND EXHAUST GAS RESIDUE IS PRESENT. TOTAL TIME OF CYLINDER IS UNKNOWN. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.