Casualties unknown

2014-10-09: Aérospatiale AS332L1 (JA6741) — Shin Nihon Helicopter Co., Ltd. — In Komoro City, Nagano Prefecture, JP

In Komoro City, Nagano Prefecture, JP

On October 9, 2014, an Aérospatiale AS332L1 (registration JA6741) operated by Shin Nihon Helicopter Co., Ltd. was involved in an aviation accident near In Komoro City, Nagano Prefecture, JP. Investigators recorded the probable cause as: The effect of the airstream and air pressure induced by flying contributed to the drop of the door. This summary draws on records from the Japan Transport Safety Board (JTSB); 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe Japan Transport Safety Board (JTSB)Primary reportUpdated 1785096185Data APIEditorial standards

On October 9, 2014, an Aérospatiale AS332L1 helicopter (JA6741) operated by Shin Nihon Helicopter lost the left door of a slung toilet hut in mid-flight. No injuries or damage resulted; the door detached due to aerodynamic forces.

Incident Overview

On October 9, 2014, at 11:38 JST, an Aérospatiale AS332L1 helicopter, registered JA6741 and operated by Shin Nihon Helicopter Co., Ltd., was conducting a sling transport operation of a toilet hut from a temporary helipad in Takamine Kogen to the Mount Asama Kazankan Lodge site. During the flight, the left door of the hut's double swing doors became detached and fell to the ground.

Flight and Operational Details

The helicopter was crewed by a captain (right seat) and a mechanic (rear seat) who monitored the operation visually and via a surveillance camera mounted on the aircraft. The flight route required an initial climb to clear a mountain ridge, followed by a descent along the mountain surface and a wide circling approach around the southern ridge of Mount Kurofu. The helicopter maintained stable flight conditions at approximately 60 knots, a speed considered appropriate for stable sling transport. The load (the hut) was connected via a 16-meter sling rope attached to the helicopter, with four ropes extending from clasps on the hut's roof.

The hut, weighing approximately 1.7 tons, was equipped with four doorways: two single swing doors at the front, one single swing door at the back, and a pair of double swing doors at the side for access to the Bio-toilet apparatus. Prior to transport, company staff secured all fixtures and fittings inside the hut, locked all doors and windows, and performed double-checks due to the presence of an aperture area in the floor. No external securing ropes or protective nets were used, as the crew and ground staff judged the locking of doors and windows sufficient.

Sequence of the Door Detachment

Video footage from the surveillance camera revealed the door detachment process. While airborne, the hut was rotating counterclockwise as viewed from above. When the hut's orientation placed the door facing opposite the direction of flight, the door was forced open. It briefly closed but then, as the rotation brought the door perpendicular to the flight direction, it was forcefully reopened, struck the hut's sidewall, and broke apart, falling to the ground. The captain and mechanic were unaware of the incident until ground workers reported a missing door after the fourth unloaded operation at the site.

Damage and Location

The left-side door of the double swing doors broke at its mounting points. Examination revealed that the door (2 m long, 70 cm wide, about 8 kg) was fixed by two hinges and a lock bolt; the lock bolt receiver on the right-side door was deformed by stress. The company identified the estimated drop location from video footage and recovered broken door parts in trees at coordinates N 36°23'40", E 138°28'47". No other damage to persons, objects, or the ground was observed. The helicopter itself sustained no damage, and there were no injuries.

Air Pressure and Aerodynamic Considerations

The double swing doors were designed to withstand wind up to approximately 70 knots based on JIS standards. Analysis indicated that the airstream and air pressure induced by flight contributed to the door's detachment. When the hut rotated and the door faced opposite the flight direction, the lower parts of the hut were subject to air pressure parallel to airspeed, while the door area experienced negative pressure from slipstream vortices, causing the door to be forced open and break.

Probable cause

The effect of the airstream and air pressure induced by flying contributed to the drop of the door.

Investigation report by the Japan Transport Safety Board (JTSB). Original record: https://jtsb.mlit.go.jp/eng-air_report/JA6741-AI2015.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.