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ANC99LA062

1999-05-15 · DILLINGHAM, Alaska, United States · None · 1 aircraft · Status: Completed

Airport DLG

Current FAA registration · N8883C

Make / Model
PIPER PA-22
Year of manufacture
1953 · 46 years old at event
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19560614
ADS-B equipped
Yes — Mode-S AC3E51

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The inadequate preflight by the pilot, who left the rudder gust lock installed, making directional control not possible.

Factual narrative

On May 15, 1999, at 1754 Alaska daylight time, a tailwheel equipped Piper PA-20 airplane, N8883C, sustained substantial damage when it departed the left edge of runway 19 at the Dillingham Airport, Dillingham, Alaska. The commercial pilot and sole passenger were not injured. The airplane was being operated under 14 CFR Part 91 as a personal flight by the pilot and his wife. The pilot originally intended to depart for the village of Ekuk, but was returning to park after taxiing for takeoff. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The pilot told the NTSB investigator-in-charge (IIC) during a telephone interview on May 18, that during taxi, the airplane did not steer correctly, but he could not determine the reason. He told the IIC that he decided to return to parking. During the return taxi on runway 19, the airplane ground looped to the left, and the pilot was unable to control the turn with rudder input or wheel brakes. The tailwheel went off the left side of the runway onto uneven ground, damaging the tailwheel support structure and center empennage. The pilot told the IIC that after the accident, he discovered the external rudder gust lock still installed. Reported winds at the time of the accident were 210 degrees at 7 knots. Runway 19 measures 6,404 feet long by 150 feet wide. The pilot stated that during taxi for takeoff the tailwheel equipped airplane did not steer correctly. He said that he decided to return to parking. While returning to park, the airplane turned to the left 270 degrees, substantially damaging the empennage. Postaccident inspection revealed the rudder gust lock was still installed on the tail. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1999_ANC99LA062.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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