20080530834429A

Accident · Destroyed

FAA accident report · Amtr Lancair · Murrieta/Temec, CA · May 30, 2008

Date
May 30, 2008 · 11:50 local
Place
Murrieta/Temec, CA
Airport
French Valley
Phase of flight
Final Approach
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N109DC
NTSB investigation
NTSBSEA08LA145
Reported as
Amtr Lancair
Reported engine
Continental IO550N
People aboard
2
Fatal injuries
2
Pilot’s flight hours
600 total0 in this make and model0 in the last 90 days

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 approach to landing, at an estimated distance of one and a quarter miles. From the end of the runway aircraft crashed into a field north of runway 18. The eye witness accounts said the engine made a loud noise and then the aircraft rolled over on the left wing, inverted rolled 180 degrees and went vertically into the ground. The crash site and wreckage indicated the aircraft was near vertical on impact. The wreckage was confined to approximately 100 square meters. Fuselage disintergrated on impact, wings except spar disintegrated, tail section aft of cockpit area was intact. Propeller was not under power when the aircraft hit the ground. There was no sign of fuel in the wings or in the engne. There was no sign offuel on the ground or on the surrounding plants, or ground, no fuel odor was present at the crash site.

As the FAA filed it

(-23) ON APPROACH TO LANDING, AT AN ESTIMATED DISTANCE OF ONE AND A QUARTER MILES. FROM THE END OF THE RUNWAY AIRCRAFT CRASHED INTO A FIELD NORTH OF RUNWAY 18. THE EYE WITNESS ACCOUNTS SAID THE ENGINE MADE A LOUD NOISE AND THEN THE AIRCRAFT ROLLED OVER ON THE LEFT WING, INVERTED ROLLED 180 DEGREES AND WENT VERTICALLY INTO THE GROUND. THE CRASH SITE AND WRECKAGE INDICATED THE AIRCRAFT WAS NEAR VERTICAL ON IMPACT. THE WRECKAGE WAS CONFINED TO APPROXIMATELY 100 SQUARE METERS. FUSELAGE DISINTERGRATED ON IMPACT, WINGS EXCEPT SPAR DISINTEGRATED, TAIL SECTION AFT OF COCKPIT AREA WAS INTACT. PROPELLER WAS NOT UNDER POWER WHEN THE AIRCRAFT HIT THE GROUND. THERE WAS NO SIGN OF FUEL IN THE WINGS OR IN THE ENGNE. THERE WAS NO SIGN OFFUEL ON THE GROUND OR ON THE SURROUNDING PLANTS, OR GROUND, NO FUEL ODOR WAS PRESENT AT THE CRASH SITE.

NTSB investigation

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