Casualties unknown

2016-04-10: PILATUS AIRCRAFT LTD. PC-12/47E (HB-FWM) — St. Gallen-Altenrhein Flughafen (LSZR), SG, CH

St. Gallen-Altenrhein Flughafen (LSZR), SG, CH

On April 10, 2016, a PILATUS AIRCRAFT LTD. PC-12/47E (registration HB-FWM) was involved in an aviation accident near St. Gallen-Altenrhein Flughafen (LSZR), SG, CH. Investigators recorded the probable cause as: The serious incident was attributed to operational reasons, with analysis indicating that the wheel brakes were likely lightly applied during touchdown. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785034239Data APIEditorial standards
Aircraft registered HB-FWM
Aircraft registered HB-FWM. Photo: Alec Wilson from Solihull,, United Kingdom / CC BY-SA 2.0, via Wikimedia Commons

On 11 April 2016, a Pilatus PC-12/47E (HB-FWM) veered off the runway after the left main tire burst during landing at St. Gallen-Altenrhein. The pilot and passenger were uninjured; the aircraft sustained light damage.

Incident

On 11 April 2016, at 14:28 local time, a Pilatus PC-12/47E, registered as HB-FWM, was involved in a serious incident during landing at St. Gallen-Altenrhein Regional Airport (LSZR). The aircraft had departed from Schwäbisch Hall-Hessental (EDTY), Germany, at 12:43 on a private flight under instrument flight rules. On board were a German private pilot, born 1985, and one passenger.

During the landing with flaps set to 40° on runway 10, the left main wheel tire burst. The aircraft veered left off the runway during the rollout. The pilot managed to steer the aircraft back onto the runway, and it came to a stop approximately 700 meters past the runway threshold. The weather was dry and sunny with a light wind from 270° at 4 knots, temperature 15 °C, and QNH 1010 hPa.

The pilot held a Private Pilot Licence (Aeroplane) issued by the European Union Aviation Safety Agency. He had accumulated 312 total flight hours, with 80 hours on type.

Aircraft and Runway Information

The HB-FWM was equipped with retractable landing gear, a turboprop engine, and a pressurised cabin. The brake system was operated by pressing the upper edges of the rudder pedals with the balls of the feet. No anti-skid system was installed on this aircraft type.

St. Gallen-Altenrhein's hard-surface runway 10 is 1500 m long and 30 m wide, with a displaced threshold of 100 m, resulting in a landing distance available (LDA) of 1400 m. The landing mass of HB-FWM was approximately 7900 lb, and the pilot's handbook indicated a landing distance over a 50 ft obstacle of 555 m and a landing roll of 250 m.

Findings

The aircraft was equipped with a flight data recorder. Data analysis showed that the aircraft touched down smoothly at 73 KIAS about 90 m past the threshold. The touchdown phase lasted about 3 seconds over 200 m, ending at 68 KIAS. Over the next 9 seconds, speed decreased by 28 knots to 40 KIAS over 290 m. Then, the aircraft began to veer left, and the left main wheel left the runway at 20 KIAS, 110 m later. The pilot then maneuvered back onto the runway, coming to a stop just past the halfway point.

Brake marks from the left wheel were visible from the touchdown point to where the wheel left the runway. The right wheel's brake marks were discontinuous. The pilot could not recall his foot position on the pedals and could not exclude unintentional brake application during and after touchdown.

Damage assessment found the left tire burst, the right tire had abrasions, and a dent on the trailing edge of the left flap. The aircraft was recovered by fitting a replacement wheel and then flown to Buochs (LSZC) for flap replacement. On 15 April 2016, the pilot completed a flight with an experienced PC-12 pilot to practice landing technique and brake usage.

Conclusions

The investigation found no evidence of pre-existing technical defects that could have caused or influenced the serious incident. The incident was attributed to operational reasons. Analysis indicated that during touchdown, the wheel brakes were likely lightly applied, causing the tires to scrub unnoticed until the left tire burst, leading to the veer-off.

Probable cause

The serious incident was attributed to operational reasons, with analysis indicating that the wheel brakes were likely lightly applied during touchdown.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/HB-FWM_sumB.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.