Accident · destroyed
Aug 28, 2003 · Vigo Park, TXThe loss of propeller pitch control for undetermined reasons.
- Damage
- Destroyed
- Injuries
- None
- Report
- FTW03LA209
From NTSB records; matched by N-number.Read NTSB report (search CAROL for FTW03LA209)
This N-number isn't registered right now. Below is its last known registration, canceled May 19, 2005.
Safety record in brief:1 NTSB accident (destroyed damage, Aug 2003)No ADs since 1998 matched1 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 loss of propeller pitch control for undetermined reasons.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for FTW03LA209)
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.
No ADs published since 1998 matched this airframe or engine model.
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.
HOT TURBINE EXHAUST IS DIRECTED ON TO LANDING GEAR V-STRUT (LEFT SIDE), CAUSING CORROSION INSIDE STEEL V-STRUT AT ABOUT MID-POINT OF STRUT. THIS UNIT HAD ABOUT 18 INCHES OF CORROSION.
From FAA Service Difficulty Reports; matched by N-number and serial number.