20240708008169A

Accident · Substantial damage

FAA accident report · Piper PA-18-150 · AK · July 8, 2024

Date
July 8, 2024 · 20:05 local
Place
AK
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N243AK
NTSB investigation
NTSBANC24LA061
Reported as
Piper PA-18-150
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot
Pilot’s flight hours
5,500 total300 in this make and model25 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.

After several successful landings of this type and an aborted one before this incident, the pilot and friend were searching for wildlife and observing the terrain when they decided to land on a particular ridge-top covered with tundra. The weather was high overcast, clouds at 5000 feet and VFR. The pilot had never been there before, but decided that due to favorable initial observations by performing several flyovers and a roll-on, that it was suitable for a full stop, ridge-top landing. During the second roll-on attempt, with the aircraft carrying speed, the aircraft hit a rough patch and bounced in the air at which time power was added in an attempted abort the landing and go-around but due to the lack of enough airspeed, failed to keep the aircraft aloft. The aircraft hit the ground causing the left gear to collapse, allowing the left wing to contact the ground and the plane “cartwheeled” over on its back coming to rest. None of the occupants were injured in the crash, and both evacuated successfully.

The pilot determined that contributing factors included that he was carrying too much speed which caused him to run out of ridge-top space, yet when his left gear collapsed while performing the roll-on, he lost so much speed that he could no longer control the aircraft for a go-around and prevent the wing from contacting the ground.

As the FAA filed it

AFTER SEVERAL SUCCESSFUL LANDINGS OF THIS TYPE AND AN ABORTED ONE BEFORE THIS INCIDENT, THE PILOT AND FRIEND WERE SEARCHING FOR WILDLIFE AND OBSERVING THE TERRAIN WHEN THEY DECIDED TO LAND ON A PARTICULAR RIDGE-TOP COVERED WITH TUNDRA. THE WEATHER WAS HIGH OVERCAST, CLOUDS AT 5000 FEET AND VFR. THE PILOT HAD NEVER BEEN THERE BEFORE, BUT DECIDED THAT DUE TO FAVORABLE INITIAL OBSERVATIONS BY PERFORMING SEVERAL FLYOVERS AND A ROLL-ON, THAT IT WAS SUITABLE FOR A FULL STOP, RIDGE-TOP LANDING. DURING THE SECOND ROLL-ON ATTEMPT, WITH THE AIRCRAFT CARRYING SPEED, THE AIRCRAFT HIT A ROUGH PATCH AND BOUNCED IN THE AIR AT WHICH TIME POWER WAS ADDED IN AN ATTEMPTED ABORT THE LANDING AND GO-AROUND BUT DUE TO THE LACK OF ENOUGH AIRSPEED, FAILED TO KEEP THE AIRCRAFT ALOFT. THE AIRCRAFT HIT THE GROUND CAUSING THE LEFT GEAR TO COLLAPSE, ALLOWING THE LEFT WING TO CONTACT THE GROUND AND THE PLANE “CARTWHEELED” OVER ON ITS BACK COMING TO REST. NONE OF THE OCCUPANTS WERE INJURED IN THE CRASH, AND BOTH EVACUATED SUCCESSFULLY.

THE PILOT DETERMINED THAT CONTRIBUTING FACTORS INCLUDED THAT HE WAS CARRYING TOO MUCH SPEED WHICH CAUSED HIM TO RUN OUT OF RIDGE-TOP SPACE, YET WHEN HIS LEFT GEAR COLLAPSED WHILE PERFORMING THE ROLL-ON, HE LOST SO MUCH SPEED THAT HE COULD NO LONGER CONTROL THE AIRCRAFT FOR A GO-AROUND AND PREVENT THE WING FROM CONTACTING THE GROUND.

NTSB investigation

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