19980209008059A

Accident · Substantial damage

FAA accident report · Piper PA-22-160 · Point Lookout, MO · February 9, 1998

Date
February 9, 1998 · 11:30 local
Place
Point Lookout, MO
Airport
M Graham Clark Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1958P
NTSB investigation
NTSBCHI98LA093
Reported as
Piper PA22160
Reported engine
Lycoming O320B2B
People aboard
4
Fatal injuries
0
Pilot’s flight hours
22,651 total55 in this make and model73 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.

Lost directional control landing. Ground looped. Tail wheel type landing gear. (.4)the pilot landed the airplane on runway 11. Directional control was lost and the airplane ground looped. The pilot stated that he had experienced a tendency for the airplane to track to the left on rollout in the past and had mentioned to a mechanic. The wind recorded at the airport 10 minutes after the accident were 120 degrees at 9 knots. An examination of the airplane after the accident failed to reveal any mechanical anomalies which might have contributed to a left turning tendency. (-23)on February 9, 1998, privacy data omitted operated Piper 22/20-160, N1958P, as pilot in command ona flight from jacksonville, Texas, to m. Graham Clark airport, Point Lookout, Missouri. At approximately 1130 CST, while landing on runway 11, privacy data omitted said the aircraft began to turn left. He then applied rudder and aileron to the right, resulting a ground loop to the right. Although aircraft maintenance records indicated some recent problems with a tail wheel shimmy, the pilot in command should have been able to perform a landing on the main wheels.

As the FAA filed it

LOST DIRECTIONAL CONTROL LANDING. GROUND LOOPED. TAIL WHEEL TYPE LANDING GEAR. (.4)THE PILOT LANDED THE AIRPLANE ON RUNWAY 11. DIRECTIONAL CONTROL WAS LOST AND THE AIRPLANE GROUND LOOPED. THE PILOT STATED THAT HE HAD EXPERIENCED A TENDENCY FOR THE AIRPLANE TO TRACK TO THE LEFT ON ROLLOUT IN THE PAST AND HAD MENTIONED TO A MECHANIC. THE WIND RECORDED AT THE AIRPORT 10 MINUTES AFTER THE ACCIDENT WERE 120 DEGREES AT 9 KNOTS. AN EXAMINATION OF THE AIRPLANE AFTER THE ACCIDENT FAILED TO REVEAL ANY MECHANICAL ANOMALIES WHICH MIGHT HAVE CONTRIBUTED TO A LEFT TURNING TENDENCY. (-23)ON FEBRUARY 9, 1998, ^PRIVACY DATA OMITTED^ OPERATED PIPER 22/20-160, N1958P, AS PILOT IN COMMAND ONA FLIGHT FROM JACKSONVILLE, TEXAS, TO M. GRAHAM CLARK AIRPORT, POINT LOOKOUT, MISSOURI. AT APPROXIMATELY 1130 CST, WHILE LANDING ON RUNWAY 11, ^PRIVACY DATA^ SAID THE AIRCRAFT BEGAN TO TURN LEFT. HE THEN APPLIED RUDDER AND AILERON TO THE RIGHT, RESULTING A GROUND LOOP TO THE RIGHT. ALTHOUGH AIRCRAFT MAINTENANCE RECORDS INDICATED SOME RECENT PROBLEMS WITH A TAIL WHEEL SHIMMY, THE PILOT IN COMMAND SHOULD HAVE BEEN ABLE TO PERFORM A LANDING ON THE MAIN WHEELS.

NTSB investigation

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