PIPER PA-28R-201

Grand Forks, ND — May 14, 2011

Event Information

DateMay 14, 2011
Event TypeACC
NTSB NumberCEN11LA390
Event ID20110614X10547
LocationGrand Forks, ND
CountryUSA
Coordinates47.94722, -97.17389
AirportGrand Forks International
Highest InjuryNONE

Aircraft

MakePIPER
ModelPA-28R-201
CategoryAIR
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor0
None2
Total Injured0

Event Location

Probable Cause

The flight instructor’s inadequate supervision of the landing, which resulted in an inadequate flare and subsequent hard landing.

Full Narrative

On May 14, 2011, at 1430 central daylight time, a Piper model PA-28R-201 airplane, N204ND, was substantially damaged during a hard landing at Grand Forks International Airport (KGFK), Grand Forks, North Dakota. The flight instructor and student were not injured. The airplane was registered to and operated by the University of North Dakota, under the provisions of 14 Code of Federal Regulations Part 91. Day visual meteorological conditions prevailed for the flight, which was operated without a flight plan. The local instructional flight originated from KGFK at 1300.

The flight instructor reported that his student was practicing a simulated forced landing to runway 35L when the accident occurred. The student, who was obtaining instruction toward a flight instructor certificate, was flying from the right seat. The flight instructor stated that after a "firm" touchdown the airplane began to veer to the right. He noted that the right wing was lower than the left wing and his initial thought was that the right tire was flat. After coming to a stop, the airplane would not move forward without an excessive application of engine power. The engine was shut down and the flight crew notified the control tower that they required a tow to the ramp. After exiting the airplane the flight instructor noticed that the right main landing gear had collapsed rearward during the landing.

A postaccident inspection of the airplane revealed substantial damage to both wings and the fuselage. The right main landing gear strut assembly was observed to be fully extended at the accident site; however, when examined by the operator the strut assembly did not exhibit any material failure, corrosion, or binding. Interviews of recent flight crews did not reveal any hard landings that could have damaged the right main landing gear before the accident flight.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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