NTSB CAROL · Event
Event LAX04CA070
Registry · N1338B
FAA Aircraft Registry record.
Make / Model
CESSNA 206H
Year of manufacture
2011
Engine
LYCOMING IO-540-AC1A5 (300 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
20111128
ADS-B equipped
Yes — Mode-S A089C8
Registrant of record
SILVER CREEK AVIATION SERVICES
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain directional control of the airplane during the landing roll.
Factual narrative
On December 18, 2003, about 1130 Pacific standard time, a Luscombe 8E, N1338B, veered off runway 31L on the landing rollout, struck a taxiway sign, and came to rest inverted at the Reid-Hillview Airport of Santa Clara County (RHV), San Jose, California. The pilot/owner operated the airplane under the provisions of 14 CFR Part 91. The airplane sustained substantial damage. The private pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed for the local area flight, and no flight plan had been filed. The flight departed the Hollister Municipal Airport (3O7), Hollister, California, about 1045. In a written statement, the pilot reported that he made a normal, straight-in approach to the runway, where he completed a three-point landing. During the landing roll, the right main gear and wing lifted. He corrected with right aileron, and the airplane began turning to the right. He then applied left rudder; however, he had released backpressure on the stick during the right aileron correction, and the rudder application was ineffective. The airplane then traveled off of the runway, impacted a taxiway sign, and came to rest inverted. The pilot indicated that there were no mechanical problems with the airplane. The airplane veered off the runway on the landing rollout, struck a taxiway sign, and came to rest inverted. The pilot made a normal, straight-in approach to the runway, where he completed a three-point landing. During the landing roll, the right main gear and wing lifted. He corrected with right aileron, and the airplane began turning to the right. He then applied left rudder; however, he had released backpressure on the stick during the right aileron correction, and the rudder application was ineffective. The airplane then traveled off of the runway. The pilot indicated that there were no mechanical problems with the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_LAX04CA070.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2019 · Conference Paper
Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper
Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
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