LAX01LA010
2000-10-12 · SAN CARLOS, California, United States · None · 1 aircraft · Status: Completed
Airport SQL
Current FAA registration · N2562D
- Make / Model
- CESSNA 170B
- Year of manufacture
- 1952 · 48 years old at event
- Engine
- CONT MOTOR IO-360-D (210 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20100329
- ADS-B equipped
- Yes — Mode-S A2706A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper and excessive application of brakes resulting from his failure to maintain directional control during landing rollout.
Factual narrative
On October 12, 2000, about 1127 hours Pacific daylight time, a Cessna 170B, N2562D, owned and operated by the pilot, nosed over during landing rollout at the San Carlos Airport, San Carlos, California. Visual meteorological conditions prevailed during the personal flight, and no flight plan was filed. The airplane was substantially damaged, and the private pilot was not injured. The flight was performed under 14 CFR Part 91, and it originated from San Carlos about 1115. The pilot reported that during the previous 90-day period he had flown his airplane for about 1.8 hours. The purpose of the accident flight was to practice landings. Upon completing one circuit around the traffic pattern, the pilot landed on runway 30, and the airplane decelerated. Upon slowing to about 15 miles per hour, the rudder lost effectiveness, and the airplane rolled toward the side of the runway. The pilot further reported that as the airplane was about to depart the runway he "stepped hard on the brakes," and the airplane nosed over. A witness reported that the midfield windsock indicated that a right quartering tail wind existed at the time of the mishap. According to San Carlos control tower personnel, at the time of the mishap the official wind was from 300 degrees at 4 knots. Upon completing one circuit around the traffic pattern, the pilot landed on runway 30. Upon slowing to about 15 miles per hour, the rudder lost effectiveness, and the airplane rolled toward the side of the runway. The pilot indicated that as his airplane was about to depart the runway he "stepped hard on the brakes," and the airplane nosed over. A witness reported that the midfield windsock indicated that a right quartering tail wind existed at the time of the mishap. According to San Carlos control tower personnel, at the time of the mishap the official wind was from 300 degrees at 4 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_LAX01LA010.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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