LAX00LA131
2000-03-19 · SCOTTSDALE, Arizona, United States · None · 1 aircraft · Status: Completed
Airport SDL
N5WC has since been reassigned. It is now registered to a different aircraft (CESSNA 560, built 1997), which was not involved in this event.
Aircraft involved
Probable cause & findings
The pilot's failure to ensure that the landing gear was lowered before touchdown.
Factual narrative
On March 19, 2000, at 1945 hours mountain standard time, a Piper PA-31-T1, N5WC, landed gear up at the Scottsdale, Arizona, airport. The airplane, operated by Gunslinger Investment Corporation, Telluride, Colorado, sustained substantial damage. The airline transport pilot and passenger were not injured. The personal cross-country flight had originated in Telluride, Colorado, at 1815, and was terminating at the time of the accident. Visual meteorological conditions prevailed and an instrument flight rules (IFR) flight plan was filed. The pilot reported that while landing on runway 21, he felt the rudder pedals vibrating. The airplane settled and he heard the propellers striking the runway. The airplane veered to the right off the runway centerline and struck a runway light. The pressure bulkhead was punctured and there was damage to the right engine air scoop cowling, the right wing leading edge, the flaps, gear doors, bottom antennas, pitot tube, and right spinner. A Federal Aviation Administration inspector from the Scottsdale Flight Standards District Office responded to the site. He reported that on March 23, 2000, he witnessed the landing gear being swung at the Scottsdale airport. He stated that no discrepancies were noted during the test. The landing gear light and horn systems functioned normally. The pilot reported that while landing, he felt the rudder pedals vibrating. The airplane settled and he heard the propellers striking the runway. The airplane veered to the right off the runway centerline and struck a runway light. The pressure bulkhead was punctured and there was damage to the right engine air scoop cowling, the right wing leading edge, the flaps, gear doors, bottom antennas, pitot tube, and right spinner. An FAA inspector witnessed the landing gear being swung and stated that no discrepancies were noted during the test. The landing gear light and horn systems functioned normally. No preexisting anomalies were found. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_LAX00LA131.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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