20110822018889A

Accident · Substantial damage

FAA accident report · Piper PA-18-150 · Emmett, ID · August 22, 2011

Date
August 22, 2011 · 11:00 local
Place
Emmett, ID
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4376Z
NTSB investigation
NTSBWPR11CA402
Reported as
Piper PA-18-150
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
1,000 total500 in this make and model15 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.

The aircraft had left mead, WA the morning of 08-22-2011 enroute to new Mexico. The pilot had stopped in lewiston, ID for fuel and continued the flight. The pilot was landing runway 28 in Emmett, ID (S78). Upon touch down the aircraft bounced slightly, the pilot lost control and the aircraft groundlooped to the right striking the left wing on the ground, bending the rear spar at the lift strut attach point, causing a bend in the aileron and damaging the fiberglass wingtip. The pilot reported calm winds and no mechanical irregularities with the aircraft.

As the FAA filed it

THE AIRCRAFT HAD LEFT MEAD, WA THE MORNING OF 08-22-2011 ENROUTE TO NEW MEXICO. THE PILOT HAD STOPPED IN LEWISTON, ID FOR FUEL AND CONTINUED THE FLIGHT. THE PILOT WAS LANDING RUNWAY 28 IN EMMETT, ID (S78). UPON TOUCH DOWN THE AIRCRAFT BOUNCED SLIGHTLY, THE PILOT LOST CONTROL AND THE AIRCRAFT GROUNDLOOPED TO THE RIGHT STRIKING THE LEFT WING ON THE GROUND, BENDING THE REAR SPAR AT THE LIFT STRUT ATTACH POINT, CAUSING A BEND IN THE AILERON AND DAMAGING THE FIBERGLASS WINGTIP. THE PILOT REPORTED CALM WINDS AND NO MECHANICAL IRREGULARITIES WITH THE AIRCRAFT.

NTSB investigation

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