FTW03LA074
2002-12-22 · West Helena, Arkansas, United States · None · 1 aircraft · Status: Completed
Airport HEE
Current FAA registration · N1392D
- Make / Model
- CESSNA 170A
- Engine
- CONT MOTOR C145 SERIES (145 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19570412
- ADS-B equipped
- Yes — Mode-S A09F42
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during landing. A contributing factor was the deflated tire.
Factual narrative
On December 22, 2002, at approximately 1600 central standard time, a Cessna 170A tail-wheel equipped airplane, N1392D, registered to and operated by a private individual, was substantially damaged during a loss of control while landing on Runway 17 at the West Helena Municipal Airport (HEE), near West Helena, Arkansas. The private pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the Title 14 Code of Federal Regulations Part 91 personal flight. The cross-country flight originated at 1500 from Clarksdale, Mississippi (CKM). In a telephone interview with the NTSB Investigator-In-Charge, the 850-hour pilot stated that after an uneventful flight from Clarksdale, he "landed hard" on Runway 17 at HEE and executed a go-around to set up for another approach/landing. Upon landing, the airplane ground looped and skidded off the runway to the left, in a 45-degree angle. The pilot further stated that he believed the airplane had "blown" the right tire during the first hard landing, and upon touch down after the go-around, the blown tire contributed to the groundloop. Examination of the wreckage by the FAA inspector, who responded to the accident site, noted a bent propeller blade and the landing gear had jammed, resulting in structural damage to the landing gear box. At the time of the accident, the winds at HEE were reported from 170 degrees at 5 knots, 10 statute miles visibility, clear sky, temperature at 16 degrees Celsius, dewpoint 4 degrees Celsius, and an altimeter setting of 29.91 inches Mercury. The density altitude was calculated by the Investigator-In-Charge at 428 feet. The 850-hour pilot lost of control of the tail-wheel equipped airplane while landing with a flat tire. The pilot stated that after an uneventful flight, he "landed hard" on Runway 17 and executed a go-around to set up for another approach/landing. Upon landing, the airplane ground looped and skidded off the runway to the left, in a 45 degree angle. The pilot further stated that he believed that the airplane had "blown" the right tire during the first hard landing, and upon touchdown after the go-around, the blown tire contributed to the ground loop. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_FTW03LA074.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (loss of control, go-around). All research papers
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- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
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- SKYbrary (Eurocontrol) 2024 · SKYbrary article Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
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In Urban Air Mobility (UAM), maintaining a minimum separation between aircraft is a safety requirement, which becomes challenging amidst congested air traffic and off-nominal conditions, such as Loss …
- Embry-Riddle Scholarly Commons 2023 · Conference paper Utilizing Deep Learning to Predict Unstabilized Approaches for General Aviation Aircraft
Unstabilized approaches pose a major hazard for general aviation aircraft. In the period from 2009 to 2019, 3,257 general aviation accidents occurred during the landing phase of flight in which loss o…