20100307030139A

Accident · Substantial damage

FAA accident report · Sutton Jame Avid Hauler · Rigby, ID · March 7, 2010

Date
March 7, 2010 · 13:00 local
Place
Rigby, ID
Airport
Rigby-Jefferson
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N22EJ
NTSB investigation
NTSBWPR10LA154
Reported as
Sutton Jame Avid Hauler
Reported engine
Bombardier ROTAX (ALL)
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
424 total9 in this make and model9 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.

Pilot performed normal preflight and run-up. Did not notice any irregularities. Shortly after take off at about 300 feet AGL the engine lost power. The engine would idle but there was no power to sustain flight. Pilot immediately executed a turn back to the airport. When it was apparent he would not make it he landed in a field. The touch down was normal but as the aircraft lost ground speed the landing gear sank into the soft field and the aircraft flipped onto it's back. A post accident inspection by two FSDO airworthiness inspectors failed to determine any mechanical defect. An engine tear-down was not performed due to the nature of the Rotax engine and the asi's unfamiliarity with that engine. A Rotax representative was invited to attend but they were unable. The pilot had recently installed an after market mixture leaning device and it is suspected that this device contributed to the power loss.

As the FAA filed it

PILOT PERFORMED NORMAL PREFLIGHT AND RUN-UP. DID NOT NOTICE ANY IRREGULARITIES. SHORTLY AFTER TAKE OFF AT ABOUT 300 FEET AGL THE ENGINE LOST POWER. THE ENGINE WOULD IDLE BUT THERE WAS NO POWER TO SUSTAIN FLIGHT. PILOT IMMEDIATELY EXECUTED A TURN BACK TO THE AIRPORT. WHEN IT WAS APPARENT HE WOULD NOT MAKE IT HE LANDED IN A FIELD. THE TOUCH DOWN WAS NORMAL BUT AS THE AIRCRAFT LOST GROUND SPEED THE LANDING GEAR SANK INTO THE SOFT FIELD AND THE AIRCRAFT FLIPPED ONTO IT'S BACK. A POST ACCIDENT INSPECTION BY TWO FSDO AIRWORTHINESS INSPECTORS FAILED TO DETERMINE ANY MECHANICAL DEFECT. AN ENGINE TEAR-DOWN WAS NOT PERFORMED DUE TO THE NATURE OF THE ROTAX ENGINE AND THE ASI'S UNFAMILIARITY WITH THAT ENGINE. A ROTAX REPRESENTATIVE WAS INVITED TO ATTEND BUT THEY WERE UNABLE. THE PILOT HAD RECENTLY INSTALLED AN AFTER MARKET MIXTURE LEANING DEVICE AND IT IS SUSPECTED THAT THIS DEVICE CONTRIBUTED TO THE POWER LOSS.

NTSB investigation

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