Casualties unknown

2024-07-07: Cessna 172P (JA4101) — Corporate body — Fukushima City Temporary Operation Site, Fukushima Prefecture, JP

Fukushima City Temporary Operation Site, Fukushima Prefecture, JP

On July 7, 2024, a Cessna 172P (registration JA4101) operated by Corporate body was involved in an aviation accident near Fukushima City Temporary Operation Site, Fukushima Prefecture, JP. Investigators recorded the probable cause as: The captain judged that the aircraft could land without difficulty with the student pilot at the controls, and the student pilot performed a normal landing procedure. This summary draws on records from the Japan Transport Safety Board (JTSB).

Sourcesthe Japan Transport Safety Board (JTSB)Primary reportUpdated 1785096185Data APIEditorial standards
Aircraft registered JA4101
Aircraft registered JA4101. Photo: Alec Wilson from Khon Kaen, Thailand / CC BY-SA 2.0, via Wikimedia Commons

On July 7, 2024, a Cessna 172P (JA4101) struck its lower aft fuselage on landing at Fukushima Sky Park. Three aboard were uninjured. The Japan Transport Safety Board investigated.

Aircraft and Personnel

The aircraft involved was a Cessna 172P, serial number 17274771, manufactured on March 11, 1981. Its airworthiness certificate was valid until May 8, 2025. The captain, aged 65, held a commercial pilot certificate and flight instructor rating, with approximately 5,713 flight hours total and about 5,200 hours on type. The student pilot, aged 56, held a student pilot certificate and had 64 flight hours, all on type. A passenger was also on board.

Incident Details

On Sunday, July 7, 2024, at approximately 10:14 Japan Standard Time, the aircraft was landing at Fukushima Sky Park (a temporary operation site for agricultural use) in Fukushima City, Fukushima Prefecture. The lower aft section of the fuselage contacted the runway during landing. No injuries occurred among the three occupants.

Meteorological Conditions

At 10:00, the meteorological observation system recorded wind from 360° at 8 knots. Earlier at 09:00, wind was from 140° at 4 knots. Windsocks visible from the runway indicated variable wind direction, frequently shifting between south and north. Fukushima Sky Park staff provided wind information to the aircraft four minutes before landing, describing the wind as unstable.

Damage

The aircraft sustained scratch marks on the lower aft fuselage and underside of the rudder, and the tie-down ring was broken at its root. The runway showed scratch marks approximately 9 cm (deepest 7 mm) and 91 cm long.

Analysis and Probable Cause

The Japan Transport Safety Board concluded that, based on surveillance camera footage, the wind over the runway changed direction frequently during the approach. The captain and student pilot, observing a north-westerly wind from the windsock, did not expect such changes in summer. The captain judged that the aircraft could land without difficulty with the student pilot at the controls, and the student pilot performed a normal landing procedure. However, as the aircraft began to flare, the wind shifted from north-west to south, blowing from the rear left, causing a loss of airspeed and leading to the lower aft fuselage contacting the runway.

Investigation report by the Japan Transport Safety Board (JTSB). Original record: https://jtsb.mlit.go.jp/eng-air_report/JA4101.pdf. This page is a structured re-presentation; facts and quotes are in the Japan Transport Safety Board (JTSB) - Ministry of Land, Infrastructure, Transport and Tourism.