20190323001849A

Accident · Substantial damage

FAA accident report · Piper PA-12 · Mecosta, MI · March 23, 2019

Date
March 23, 2019 · 10:30 local
Place
Mecosta, MI
Airport
Canadian Lakes
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2733M
NTSB investigation
NTSBGAA19CA178
Reported as
Piper PA-12
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
450 total70 in this make and model3 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 March 23, 2019 at 1030 eastern, a Piper PA-12 aircraft, N2733M, registered to and operated by a private pilot, received substantial damage when it impacted a runway marker cone and a flag pole during landing at Canadian Lakes Airport (0C5), Mecosta county, Michigan. Both the pilot and single passenger were uninjured. Visual meteorological conditions and very light winds prevailed at the time of the accident. The personal flight was being conducted under the provisions of title 14 code of federal regulations (CFR) part 91 without a flight plan. The local flight originated from the paul c. miller airport (8D4), sparta, Michigan at approximately 0900L.

According to the pilot, he was landing to the north on the 3,800 foot grass runway, when the aircraft started to drift to the right. Before the pilot could react, the tundra tire equipped right main landing gear struck a runway marker cone mid-field. Following the impact the aircraft continued to drift to the right until the right wing made contact with a steel flag pole approximately 300 feet from the initial impact point. The aircraft then spun 180 degrees and came to rest approximately 50 feet from the broken flag pole. Both the pilot and passenger were able to egress from the wreckage without injury. Upon investigation the aircraft was found with major damage to the right wing with aft impact damage mid length twisting the wingtip 90 degrees up. The right fuel tank had been breached and a strong odor of avgas could be detected. The local fire department had responded and sprayed the wreckage with afff. The right main landing gear was buckled and folded outward. The left wing struts were also buckled with the wingtip also showing signs of impact damage. The main fuselage remained intact as well as the vertical and horizontal stabilizers. The propeller tips showed signs of impact scratching with aft bending. There was no post-crash fire. The pilot also stated there were no mechanical issues with the aircraft prior to the accident.

Weather report at krqb airport at 1455 UTC was: wind 250 degrees at 4 knots, visibility 10 statute miles, clear, temp 0 dew point 7 and altimeter 3029.

As the FAA filed it

ON MARCH 23, 2019 AT 1030 EASTERN, A PIPER PA-12 AIRCRAFT, N2733M, REGISTERED TO AND OPERATED BY A PRIVATE PILOT, RECEIVED SUBSTANTIAL DAMAGE WHEN IT IMPACTED A RUNWAY MARKER CONE AND A FLAG POLE DURING LANDING AT CANADIAN LAKES AIRPORT (0C5), MECOSTA COUNTY, MICHIGAN. BOTH THE PILOT AND SINGLE PASSENGER WERE UNINJURED. VISUAL METEOROLOGICAL CONDITIONS AND VERY LIGHT WINDS PREVAILED AT THE TIME OF THE ACCIDENT. THE PERSONAL FLIGHT WAS BEING CONDUCTED UNDER THE PROVISIONS OF TITLE 14 CODE OF FEDERAL REGULATIONS (CFR) PART 91 WITHOUT A FLIGHT PLAN. THE LOCAL FLIGHT ORIGINATED FROM THE PAUL C. MILLER AIRPORT (8D4), SPARTA, MICHIGAN AT APPROXIMATELY 0900L.

ACCORDING TO THE PILOT, HE WAS LANDING TO THE NORTH ON THE 3,800 FOOT GRASS RUNWAY, WHEN THE AIRCRAFT STARTED TO DRIFT TO THE RIGHT. BEFORE THE PILOT COULD REACT, THE TUNDRA TIRE EQUIPPED RIGHT MAIN LANDING GEAR STRUCK A RUNWAY MARKER CONE MID-FIELD. FOLLOWING THE IMPACT THE AIRCRAFT CONTINUED TO DRIFT TO THE RIGHT UNTIL THE RIGHT WING MADE CONTACT WITH A STEEL FLAG POLE APPROXIMATELY 300 FEET FROM THE INITIAL IMPACT POINT. THE AIRCRAFT THEN SPUN 180 DEGREES AND CAME TO REST APPROXIMATELY 50 FEET FROM THE BROKEN FLAG POLE. BOTH THE PILOT AND PASSENGER WERE ABLE TO EGRESS FROM THE WRECKAGE WITHOUT INJURY. UPON INVESTIGATION THE AIRCRAFT WAS FOUND WITH MAJOR DAMAGE TO THE RIGHT WING WITH AFT IMPACT DAMAGE MID LENGTH TWISTING THE WINGTIP 90 DEGREES UP. THE RIGHT FUEL TANK HAD BEEN BREACHED AND A STRONG ODOR OF AVGAS COULD BE DETECTED. THE LOCAL FIRE DEPARTMENT HAD RESPONDED AND SPRAYED THE WRECKAGE WITH AFFF. THE RIGHT MAIN LANDING GEAR WAS BUCKLED AND FOLDED OUTWARD. THE LEFT WING STRUTS WERE ALSO BUCKLED WITH THE WINGTIP ALSO SHOWING SIGNS OF IMPACT DAMAGE. THE MAIN FUSELAGE REMAINED INTACT AS WELL AS THE VERTICAL AND HORIZONTAL STABILIZERS. THE PROPELLER TIPS SHOWED SIGNS OF IMPACT SCRATCHING WITH AFT BENDING. THERE WAS NO POST-CRASH FIRE. THE PILOT ALSO STATED THERE WERE NO MECHANICAL ISSUES WITH THE AIRCRAFT PRIOR TO THE ACCIDENT.

WEATHER REPORT AT KRQB AIRPORT AT 1455 UTC WAS: WIND 250 DEGREES AT 4 KNOTS, VISIBILITY 10 STATUTE MILES, CLEAR, TEMP 0 DEW POINT 7 AND ALTIMETER 3029.

NTSB investigation

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