20021113032929A

Accident · Destroyed

FAA accident report · Beech A36TC · San Andreas, CA · November 13, 2002

Date
November 13, 2002 · 13:05 local
Place
San Andreas, CA
Airport
Calaveras Co-Maury Airport
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N32FW
NTSB investigation
NTSBSEA03FA008
Reported as
Beech A36TC
People aboard
2
Fatal injuries
2

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) On 11-13-2002 ratheon A36TC departed northbound from San Andreas, CA airport (0O3) and had a total loss of engine power at about 200 feet above ground level. The aircraft glided to a point 1/2 mile from the end of the runway and impacted in a level attitude with a cluster of rocks. The pilot and front seat passenger were fatally injured. The rear-seat passenger was seriously injured. Fuel tanks were full and fuel was found in the supply hose to the fuel injector manifold as well as the fuel selector. No mechanical irregularities were noted during the on scene investigation. All witnesses interviewed stated they heard a loud bang or pop followed by silence. The aircraft was destroyed. No fire followed the impact. Weather was not an issue. Due to the damage of the engine due to impact, it was sent to Continental engines in mobile, Alabama for analysis. This report will be amended as results are made available.

As the FAA filed it

(-23) ON 11-13-2002 RATHEON A36TC DEPARTED NORTHBOUND FROM SAN ANDREAS, CA AIRPORT (0O3) AND HAD A TOTAL LOSS OF ENGINE POWER AT ABOUT 200 FEET ABOVE GROUND LEVEL. THE AIRCRAFT GLIDED TO A POINT 1/2 MILE FROM THE END OF THE RUNWAY AND IMPACTED IN A LEVEL ATTITUDE WITH A CLUSTER OF ROCKS. THE PILOT AND FRONT SEAT PASSENGER WERE FATALLY INJURED. THE REAR-SEAT PASSENGER WAS SERIOUSLY INJURED. FUEL TANKS WERE FULL AND FUEL WAS FOUND IN THE SUPPLY HOSE TO THE FUEL INJECTOR MANIFOLD AS WELL AS THE FUEL SELECTOR. NO MECHANICAL IRREGULARITIES WERE NOTED DURING THE ON SCENE INVESTIGATION. ALL WITNESSES INTERVIEWED STATED THEY HEARD A LOUD BANG OR POP FOLLOWED BY SILENCE. THE AIRCRAFT WAS DESTROYED. NO FIRE FOLLOWED THE IMPACT. WEATHER WAS NOT AN ISSUE. DUE TO THE DAMAGE OF THE ENGINE DUE TO IMPACT, IT WAS SENT TO CONTINENTAL ENGINES IN MOBILE, ALABAMA FOR ANALYSIS. THIS REPORT WILL BE AMENDED AS RESULTS ARE MADE AVAILABLE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.