What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On June 29, 2004, about 1530 Alaska daylight time, a PA-22-160 airplane, N9038D, modified with conventional landing gear, and equipped with tundra tires, sustained substantial damage when its left main landing gear collided with rocks during the landing roll on an unimproved landing strip, 30 miles northwest of Tyonek, Alaska. The airplane was being operated by the pilot as a visual flight rule (VFR) personal cross-country flight under title 14 CFR part 91 when the accident occurred. The airline transport pilot, the sole occupant, was not injured. The pilot stated that during the landing roll the airplane had slowed to about 25 knots, when the left main wheel collided with large rocks that were lining the left side of the landing strip. The left main landing gear collapsed, and the left wing and propeller struck the ground. The pilot also stated that the left wing strut, left wing, propeller, and fuselage were damaged in the accident. He noted no mechanical anomalies with the airplane prior to the accident.
As the FAA filed it
(-23) ON JUNE 29, 2004, ABOUT 1530 ALASKA DAYLIGHT TIME, A PA-22-160 AIRPLANE, N9038D, MODIFIED WITH CONVENTIONAL LANDING GEAR, AND EQUIPPED WITH TUNDRA TIRES, SUSTAINED SUBSTANTIAL DAMAGE WHEN ITS LEFT MAIN LANDING GEAR COLLIDED WITH ROCKS DURING THE LANDING ROLL ON AN UNIMPROVED LANDING STRIP, 30 MILES NORTHWEST OF TYONEK, ALASKA. THE AIRPLANE WAS BEING OPERATED BY THE PILOT AS A VISUAL FLIGHT RULE (VFR) PERSONAL CROSS-COUNTRY FLIGHT UNDER TITLE 14 CFR PART 91 WHEN THE ACCIDENT OCCURRED. THE AIRLINE TRANSPORT PILOT, THE SOLE OCCUPANT, WAS NOT INJURED. THE PILOT STATED THAT DURING THE LANDING ROLL THE AIRPLANE HAD SLOWED TO ABOUT 25 KNOTS, WHEN THE LEFT MAIN WHEEL COLLIDED WITH LARGE ROCKS THAT WERE LINING THE LEFT SIDE OF THE LANDING STRIP. THE LEFT MAIN LANDING GEAR COLLAPSED, AND THE LEFT WING AND PROPELLER STRUCK THE GROUND. THE PILOT ALSO STATED THAT THE LEFT WING STRUT, LEFT WING, PROPELLER, AND FUSELAGE WERE DAMAGED IN THE ACCIDENT. HE NOTED NO MECHANICAL ANOMALIES WITH THE AIRPLANE PRIOR TO THE ACCIDENT.
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 N9038D · 2
Matched to the same aircraft by N-number and date.