This N-number isn't registered right now. Below is its last known registration, canceled Apr 30, 2015.
Safety record in brief:1 NTSB accident (substantial damage, Oct 2006)1 AD may apply1 service difficulty report
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 pre-flight planning which resulted in fuel starvation and the subsequent the loss of engine power. A contributing factor was the lack of suitable terrain for the forced landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DFW07LA009)
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 |
|---|---|---|---|
| 98-03-16 | The New Piper Aircraft Corporation Model PA-38-112 Airplanes | Mar 16, 1998 | Airframe (PA-38-112)Certain serial numbers: PA-38-112 38-80A0166–38-82A0122 |
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.
OIL LEAK AT NR 1 CYLINDER APPEARED TO BE COMING FROM PUSHROD TUBE SEALS. FURTHER INVESTIGATION AND PRESSURE CHECK DISCLOSED LEAK UNDER INTAKE PUSHROD AT HEAD/BARREL JOINT. A 2 INCH CRACK, 1.50 INCHES DOWN FROM TOP OF CYLINDER WALL WAS VISIBLE INSIDE THE CYLINDER. CYLINDER HAD BEEN CHROMED.…
From FAA Service Difficulty Reports; matched by N-number and serial number.