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ANC07CA030

2007-04-24 · Soldotna, Alaska, United States · None · 1 aircraft · Status: Completed

Airport SXQ

Current FAA registration · N3579A

Make / Model
PIPER PA-22-135
Year of manufacture
1953 · 54 years old at event
Engine
LYCOMING IO-320 SERIES (150 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19560101
ADS-B equipped
Yes — Mode-S A40262

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to compensate for a crosswind during the landing roll, which resulted in a loss of control, an encounter with a muddy berm, and a nose over. A factor in the accident was a crosswind.

Factual narrative

The private certificated pilot was landing a tailwheel-equipped airplane while practicing touch-and-go landings, which required a correction for a left crosswind, during a Title 14, CFR Part 91 personal flight. During touchdown, the pilot inadvertently allowed the airplane to veer to the right, and he applied takeoff power in an attempt to abort the landing. The pilot said that after he applied takeoff power, the veer worsened, and he reduced power in an attempt to stop the airplane. The airplane subsequently went off the right side of the runway, encountered a muddy berm, and nosed over. The airplane sustained structural damage to the wing lift struts and empennage. The pilot noted that there were no preaccident mechanical anomalies with the airplane. The private certificated pilot was landing a tailwheel-equipped airplane while practicing touch-and-go landings, which required a correction for a left crosswind, during a Title 14, CFR Part 91 personal flight. During touchdown, the pilot inadvertently allowed the airplane to veer to the right, and he applied takeoff power in an attempt to abort the landing. The pilot said that after he applied takeoff power, the veer worsened, and he reduced power in an attempt to stop the airplane. The airplane subsequently went off the right side of the runway, encountered a muddy berm, and nosed over. The airplane sustained structural damage to the wing lift struts and empennage. The pilot noted that there were no preaccident mechanical anomalies with the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2007_ANC07CA030.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (icing, loss of control). All research papers