20150819018649I

Incident · Minor damage

FAA incident report · Piper PA-25-235 · Warren, VT · August 19, 2015

Date
August 19, 2015 · 15:30 local
Place
Warren, VT
Phase of flight
Takeoff: Departure Roll
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N9584P
Reported as
Piper PA-25-235
Reported engine
Lycoming 0-540 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
2,430 total1,400 in this make and model53 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.

On takeoff at around 40 mph while towing a glider, the pilot suddenly realized the aircraft was settling, grass was being thrown into the air, and he could hear the prop hitting the sod runway. He immediately pulled the power back to idle and shut the engine down with the mixture control, and the aircraft settled farther and groundlooped to the right. On exiting the aircraft, the pilot noted the bolt that connected the inner attachment point of the right main gear to the bungee shock system had broken and half of the bolt was hanging from the safety cable. The glider was able to stop with no problems. There were no injuries and minor damage to the aircraft.

As the FAA filed it

ON TAKEOFF AT AROUND 40 MPH WHILE TOWING A GLIDER, THE PILOT SUDDENLY REALIZED THE AIRCRAFT WAS SETTLING, GRASS WAS BEING THROWN INTO THE AIR, AND HE COULD HEAR THE PROP HITTING THE SOD RUNWAY. HE IMMEDIATELY PULLED THE POWER BACK TO IDLE AND SHUT THE ENGINE DOWN WITH THE MIXTURE CONTROL, AND THE AIRCRAFT SETTLED FARTHER AND GROUNDLOOPED TO THE RIGHT. ON EXITING THE AIRCRAFT, THE PILOT NOTED THE BOLT THAT CONNECTED THE INNER ATTACHMENT POINT OF THE RIGHT MAIN GEAR TO THE BUNGEE SHOCK SYSTEM HAD BROKEN AND HALF OF THE BOLT WAS HANGING FROM THE SAFETY CABLE. THE GLIDER WAS ABLE TO STOP WITH NO PROBLEMS. THERE WERE NO INJURIES AND MINOR DAMAGE TO THE AIRCRAFT.