WPR13CA258
2013-04-18 · Corvallis, Oregon, United States · None · 1 aircraft · Status: Completed
Airport CVO
Current FAA registration · N711BG
- Make / Model
- CESSNA P210N
- Year of manufacture
- 1982 · 31 years old at event
- Engine
- CONT MOTOR TSIO-520 SER (300 hp)
- Seats / Engines
- 6 seats · 1 engine
- Last airworthiness date
- 19970711
- ADS-B equipped
- Yes — Mode-S A97FE4
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadvertent selection and activation of the landing gear handle rather than the flap handle during the landing roll. Contributing to the accident was the pilot's decision to alter the configuration of the airplane before exiting the runway.
Factual narrative
At the conclusion of a cross-country flight, the pilot announced his position as he was approaching the non-towered airport with the intention to conduct a straight in approach to runway 35. The landing was normal, and the pilot reported that there was "at least" 4,000 feet of runway remaining after touchdown. During the landing roll, when the airplane had slowed to about 50 knots, he decided to retract the flaps. However, he inadvertently grasped and raised the landing gear handle instead, and the nose gear retracted. The main gear remained extended, and the airplane came to a stop on the runway. The airplane sustained substantial damage to the nose keel structure, as well as damage to the cowl, nose gear doors, and propeller. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot further reported, “When landing, pilot should make no changes to flaps or other systems until the airplane has fully decelerated.” At the conclusion of a cross-country flight and as the airplane was approaching the non-towered airport, the pilot announced his position and his intention to conduct a straight-in approach to runway 35. The landing was normal, and during the landing roll, when the airplane had slowed to about 50 knots, the pilot decided to retract the flaps. However, he inadvertently grasped and raised the landing gear handle instead, and the nose gear retracted. The main gear remained extended, and the airplane came to a stop on the runway. The airplane sustained substantial damage to the nose keel structure, as well as damage to the cowl, nose gear doors, and propeller. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot further reported, “When landing, pilot should make no changes to flaps or other systems until the airplane has fully decelerated.” Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
- F Personnel issues-Action/decision-Action-Unneccessary action-Pilot - F
- F Personnel issues-Action/decision-Info processing/decision-(general)-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2013_WPR13CA258.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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