Summary
On January 17, 2003, a Classic Fighter Industries ME-262 Reproduction (N262AZ) was involved in an incident near Everett, WA. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: Failure of the left main gear hydraulic actuator locking slide during landing. Factors include an embankment adjacent to the landing runway.
On January 17, 2003, at 1430 Pacific standard time, an experimental ME 262 reproduction, N262AZ, sustained substantial damage following a gear collapse during the landing rollout at Snohomish County Airport (Paine Field), Everett, Washington. The airline transport pilot-in-command was not injured. The airplane is owned by a private party and was being operated as a visual flight rules (VFR) post production test flight under Title 14, CFR Part 91, when the accident occurred.
This incident is documented in NTSB report SEA03LA027. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N262AZ.
Accident Details
Probable Cause and Findings
Failure of the left main gear hydraulic actuator locking slide during landing. Factors include an embankment adjacent to the landing runway.
Aircraft Information
Registered Owner (Current)
Analysis
On January 17, 2003, at 1430 Pacific standard time, an experimental ME 262 reproduction, N262AZ, sustained substantial damage following a gear collapse during the landing rollout at Snohomish County Airport (Paine Field), Everett, Washington. The airline transport pilot-in-command was not injured. The airplane is owned by a private party and was being operated as a visual flight rules (VFR) post production test flight under Title 14, CFR Part 91, when the accident occurred. Visual meteorological conditions prevailed, and a flight plan had been filed for the local test flight that originated from Paine Field approximately 30 minutes prior to the accident.
During a telephone conversation with the Investigator-In-Charge (IIC), the pilot reported that he experienced a problem with the airplane's landing gear and utilized the emergency gear extension system (nitrogen blow-down) to lower the gear. The pilot stated that after activating the system, the landing gear extended and the green gear down indicator lights illuminated.
After successfully lowering the gear, the pilot initiated a landing at the departure airport. He reported that shortly after touchdown, the left main landing gear collapsed and the aircraft veered to the left, eventually exiting the runway edge and traveling down an embankment that's adjacent to the runway.
Post accident inspection of the aircraft's left main gear hydraulic system revealed that the hydraulic actuator locking slide was undersized which allowed the gear to collapse (unlock) when placed under a load. See attached report for additional information.
During the accident sequence, the airplane sustained substantial damage to the fuselage.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA03LA027