20000811040879A

Accident · Destroyed

FAA accident report · Amtr SR2500 · Bakersfield, CA · August 11, 2000

Date
August 11, 2000 · 19:00 local
Place
Bakersfield, CA
Airport
Private
Phase of flight
Forced Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N24VW
NTSB investigation
NTSBLAX00LA293
Reported as
Amtr SR2500
Reported engine
Continental IO470D
People aboard
3
Fatal injuries
2
Pilot’s flight hours
900 total48 in this make and model10 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) The pilot was circling to land a Private air strip at approximately 150 feet AGL when the engine lost power. Due to the aircraft altitude of 150 feet AGL. The pilot was unable to land at the Private airstrip and attempted to make an emergency landing on a dirt road adjacent to a corn field. As the aircraft was about to touch down on the dirt road, the left wing struck a metal pole causing the aircraft to divert and crash into the corn field. (.4) during an emergency landing the left wing of the airplane struck an irrigation standpipe, and the airplane was destroyed in a post impact fire. The pilot reduced the power to descend and circle to land at a dirt airstrip. When he advanced the throttle to arrest the airplane's descent there was no corresponding power increase. He conducted the emergency procedures, but was unable to restart the engine. He overflew the airstrip and attempted an emergency landing in a cornfield. Review of the airplane's power plant logbook revealed that an overhauled engine had been installed on the experimental airplane in March 1999. The last entry was December 8, 1999, when the engine was test ran, and the fuel injection system was adjusted according to manufacturer's specifications. No further entries were found in the airframe or power plant logbooks. During the engine examination the throttle valve was found jammed in the closed position. Investigators also found the idle speed stop screw backed off from the throttle shaft arm about 1/8 inch. No further mechanical anomalies were noted.

As the FAA filed it

(-23) THE PILOT WAS CIRCLING TO LAND A PRIVATE AIR STRIP AT APPROXIMATELY 150 FEET AGL WHEN THE ENGINE LOST POWER. DUE TO THE AIRCRAFT ALTITUDE OF 150 FEET AGL. THE PILOT WAS UNABLE TO LAND AT THE PRIVATE AIRSTRIP AND ATTEMPTED TO MAKE AN EMERGENCY LANDING ON A DIRT ROAD ADJACENT TO A CORN FIELD. AS THE AIRCRAFT WAS ABOUT TO TOUCH DOWN ON THE DIRT ROAD, THE LEFT WING STRUCK A METAL POLE CAUSING THE AIRCRAFT TO DIVERT AND CRASH INTO THE CORN FIELD. (.4) DURING AN EMERGENCY LANDING THE LEFT WING OF THE AIRPLANE STRUCK AN IRRIGATION STANDPIPE, AND THE AIRPLANE WAS DESTROYED IN A POST IMPACT FIRE. THE PILOT REDUCED THE POWER TO DESCEND AND CIRCLE TO LAND AT A DIRT AIRSTRIP. WHEN HE ADVANCED THE THROTTLE TO ARREST THE AIRPLANE'S DESCENT THERE WAS NO CORRESPONDING POWER INCREASE. HE CONDUCTED THE EMERGENCY PROCEDURES, BUT WAS UNABLE TO RESTART THE ENGINE. HE OVERFLEW THE AIRSTRIP AND ATTEMPTED AN EMERGENCY LANDING IN A CORNFIELD. REVIEW OF THE AIRPLANE'S POWER PLANT LOGBOOK REVEALED THAT AN OVERHAULED ENGINE HAD BEEN INSTALLED ON THE EXPERIMENTAL AIRPLANE IN MARCH 1999. THE LAST ENTRY WAS DECEMBER 8, 1999, WHEN THE ENGINE WAS TEST RAN, AND THE FUEL INJECTION SYSTEM WAS ADJUSTED ACCORDING TO MANUFACTURER'S SPECIFICATIONS. NO FURTHER ENTRIES WERE FOUND IN THE AIRFRAME OR POWER PLANT LOGBOOKS. DURING THE ENGINE EXAMINATION THE THROTTLE VALVE WAS FOUND JAMMED IN THE CLOSED POSITION. INVESTIGATORS ALSO FOUND THE IDLE SPEED STOP SCREW BACKED OFF FROM THE THROTTLE SHAFT ARM ABOUT 1/8 INCH. NO FURTHER MECHANICAL ANOMALIES WERE NOTED.

NTSB investigation

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