N6038D is a 1956 Piper PA-22-150. It is a fixed-wing single-engine aircraft with 4 seats, powered by a Lycoming 0-320 series rated at 180 horsepower. The registration is active, with the registrant based in Port Townsend, WA. Its standard airworthiness certificate was issued in Dec 1956. It has been registered to its current owner since Jan 2010. This page also carries 1 NTSB event.
- 70 years old
- 1 of 1,239 Piper PA-22-150
2010
1956
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N6038D's record changes.
On August 20, 2009, about 2020 Pacific daylight time, a tailwheel equipped Piper PA-22-150, N6038D, sustained substantial damage subsequent to a main landing gear collapse during landing at Tacoma-Narrows Airport, Tacoma, Washington. The student pilot, the sole occupant of the airplane, was not injured. The airplane was registered to the pilot and operated as a personal flight under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The flight departed Paine Field, Everett, Washington, about 1915 with a planned destination of Tacoma. Visual meteorological conditions prevailed, and no flight plan had been filed.
In a written report submitted to the National Transportation Safety Board, the pilot reported that during a crosswind landing the right main landing gear strut collapsed. He added that shortly after the "right wing low" wheel landing, he heard the right "gear leg pop." The pilot stated that the winds were from 210 degrees at 8-12 knots and he was landing on runway 17.
The airplane sustained substantial damage to the gear support structure and associated gearbox.
The forward right landing gear strut attachment fitting was removed from the gear assembly and forwarded to the NTSB Materials Laboratory in Washington, DC, for examination. A Safety Board Senior Metallurgist examined the fitting and reported that the fracture faces displayed features and deformations consistent with overstress separations. The metallurgist reported that no indications of preexisting cracking or corrosion were detected.
The Materials Laboratory Factual Report is included in the public docket for this accident.
The pilot reported no mechanical anomalies with the airplanes flight control systems prior to the accident.
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