20080907845079A

Accident · Substantial damage

FAA accident report · Amtr MINIMAX1500R · Tiverton, RI · September 7, 2008

Date
September 7, 2008 · 16:50 local
Place
Tiverton, RI
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N43436
NTSB investigation
NTSBMIA08LA186
Reported as
Amtr MINIMAX1500R
Reported engine
ROTAX ROTAX447
Fatal injuries
0
Pilot’s flight hours
3,000 total600 in this make and model20 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) Aircraft lost power at approximately 1000 ft MSL. Pilot made an emergency landing onto a closed bridge. The aircraft landed on the bridge then bounced making contact with a retaining wall which flipped the aircraft over tearing off the landing gear. The aircraft landed on the beach destroying the right wing and damaging the left wing. The pilot sustained bumps and bruises and refused medical attention. No passengers on board. Engine tear down indicated that rear cylinder walls were scored and rings were extremely tight. Cylinder had approx. 200+ hours.

As the FAA filed it

(-23) AIRCRAFT LOST POWER AT APPROXIMATELY 1000 FT MSL. PILOT MADE AN EMERGENCY LANDING ONTO A CLOSED BRIDGE. THE AIRCRAFT LANDED ON THE BRIDGE THEN BOUNCED MAKING CONTACT WITH A RETAINING WALL WHICH FLIPPED THE AIRCRAFT OVER TEARING OFF THE LANDING GEAR. THE AIRCRAFT LANDED ON THE BEACH DESTROYING THE RIGHT WING AND DAMAGING THE LEFT WING. THE PILOT SUSTAINED BUMPS AND BRUISES AND REFUSED MEDICAL ATTENTION. NO PASSENGERS ON BOARD. ENGINE TEAR DOWN INDICATED THAT REAR CYLINDER WALLS WERE SCORED AND RINGS WERE EXTREMELY TIGHT. CYLINDER HAD APPROX. 200+ HOURS.

NTSB investigation

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