20110130000729A

Accident · Substantial damage

FAA accident report · Cessna 172P · South Point, OH · January 30, 2011

Date
January 30, 2011 · 13:35 local
Place
South Point, OH
Airport
Lawrence County Airpark
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N55212
NTSB investigation
NTSBCEN11LA169
Reported as
Cessna 172P
Reported engine
Lycoming 0-320-D2J
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Private pilot
Pilot’s flight hours
220 total60 in this make and model8 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 stated, after departure from runway 8, the aircraft engine suddenly began to run rough during the climb. Pilot stated he executed a steep left turn with intention to land on runway 26. During approach pilot stated he was too high and subsequently overshot runway 26. Pilot stated he applied full power, retracted flaps, and increased pitch to avoid hitting trees west of runway. Pilot stated the stall warning sounded as the aircraft rotated left, descended rapidly, striking trees before impacting ground, and coming to rest in an upright position. Ground scarring indicated a low velocity, high angle impact while the aircraft was rotating to the left. The first impact scar (and matching paint chips) indicated that the left wingtip made first contact with the ground. Propeller damage was consistent with impact while the engine was operating under full power. Engine continuity field test was performed and found no mechanical malfunctions.

As the FAA filed it

PILOT STATED, AFTER DEPARTURE FROM RUNWAY 8, THE AIRCRAFT ENGINE SUDDENLY BEGAN TO RUN ROUGH DURING THE CLIMB. PILOT STATED HE EXECUTED A STEEP LEFT TURN WITH INTENTION TO LAND ON RUNWAY 26. DURING APPROACH PILOT STATED HE WAS TOO HIGH AND SUBSEQUENTLY OVERSHOT RUNWAY 26. PILOT STATED HE APPLIED FULL POWER, RETRACTED FLAPS, AND INCREASED PITCH TO AVOID HITTING TREES WEST OF RUNWAY. PILOT STATED THE STALL WARNING SOUNDED AS THE AIRCRAFT ROTATED LEFT, DESCENDED RAPIDLY, STRIKING TREES BEFORE IMPACTING GROUND, AND COMING TO REST IN AN UPRIGHT POSITION. GROUND SCARRING INDICATED A LOW VELOCITY, HIGH ANGLE IMPACT WHILE THE AIRCRAFT WAS ROTATING TO THE LEFT. THE FIRST IMPACT SCAR (AND MATCHING PAINT CHIPS) INDICATED THAT THE LEFT WINGTIP MADE FIRST CONTACT WITH THE GROUND. PROPELLER DAMAGE WAS CONSISTENT WITH IMPACT WHILE THE ENGINE WAS OPERATING UNDER FULL POWER. ENGINE CONTINUITY FIELD TEST WAS PERFORMED AND FOUND NO MECHANICAL MALFUNCTIONS.

NTSB investigation

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

Other reports on N55212 · 3

Matched to the same aircraft by N-number and date.