DEN02LA108
2002-09-14 · Spanish Fork, Utah, United States · None · 1 aircraft · Status: Completed
Airport U77
Current FAA registration · N8369H
- Make / Model
- STINSON L-5
- Engine
- LYCOMING 0-435A/0-435C (190 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19561016
- ADS-B equipped
- Yes — Mode-S AB723F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's inadequate use of rudder and failure to maintain direcctional control following a bounced landing. A contributing factor was the pilot's improper recovery from the bounced landing.
Factual narrative
On September 14, 2002, approximately 1130 mountain daylight time, a Stinson L-5E, N8369H, was substantially damaged when it collided with terrain following a hard landing at Spanish Fork-Springville Airport, Spanish Fork, Utah. The private pilot and his passenger were not injured. Day visual meteorological conditions prevailed, and no flight plan had been filed for the personal flight being conducted under Title 14 CFR Part 91. The flight originated approximately 1040 from Nephi Municipal Airport, Nephi, Utah. According to the pilot's accident report and a previous telephone conversation, the airplane landed hard and bounced. The pilot said he added power. When the airplane touched down, "the nose had drifted to the right" and the airplane departed the runway. "I don't believe I applied sufficient rudder to offset the p-factor of the added power," the pilot wrote. The left main landing gear dropped into a hole and broke off. The airplane fell to the ground, damaging the outboard portion of the left wing spar and wing tip. The wooden prop was shattered, the firewall was wrinkled, and the carburetor and exhaust system were damaged. The airplane landed hard and bounced, and the pilot added power. When the airplane touched down again, the nose had drifted to the right and the airplane departed the runway. The pilot said, "I don't believe I applied sufficient rudder to offset the p-factor of the added power." The left main landing gear dropped into a hole and broke off. The airplane fell to the ground, damaging the outboard portion of the left wing spar and wing tip. The wooden prop was shattered, the firewall was wrinkled, and the carburetor and exhaust system were damaged. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_DEN02LA108.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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