Mechanical failure causes Hiller UH-12A crash at Bern-Belp

Casualties unknown • Bern Flughafen (LSZB), BE, CH

A training flight ended in a sudden roll and crash of a Hiller UH-12A helicopter due to a failure in the rotor control linkage.

What happened

On September 21, 1963, a Hiller UH-12A helicopter, registration HB-XBS, was conducting a training flight at Bern-Belp airfield. The aircraft, operated by Heliswiss Schweiz Helikopter A.G., was being flown by an instructor accompanied by a student pilot. While flying at an altitude of approximately one meter above the airfield, the helicopter suddenly tilted to the left. This sudden movement caused the rotor to strike the ground, leading to a crash. There were no injuries to the two occupants, though the aircraft sustained heavy damage, estimated at roughly 80% of its value.

The investigation

The investigation focused on the mechanical integrity of the rotor control system. The aircraft's control mechanism relies on rods connecting the swashplate to transmission levers to manage cyclic pitch. Investigators examined the condition of the bolts and safety pins at these connection points. During the post-crash inspection, the right rod connecting the transmission lever to the swashplate was found disconnected from its lever. While the rod itself was undamaged, the securing nut and the split pin were missing. The bolt used in this connection showed signs of wear, with its diameter reduced from 6.5 mm to 5.7 mm. Additionally, the front rod was found to be missing its split pin, although the bolt and nut remained in place.

Findings

  • The primary cause of the accident was the failure of a critical rotor control element due to inadequate mechanical securing of a bolt connection.
  • It is highly probable that the split pins had been removed at some point and not replaced, as the deficiency was present on both the right and front control rods.
  • The investigation could not definitively determine when the safety pins were removed, though the worn condition of the bolt thread suggests the nut may have been loose for some time.
  • While recent maintenance and pre-flight inspections were conducted, the investigation noted that the specific nature of these checks might not have focused on these particular internal linkages.

Probable cause

The accident was caused by the failure of the right-hand rotor control rod connection because the securing bolt was not properly immobilized by a nut and split pin.

Frequently asked questions

What happened in the 1963-09-21 FAIRCHILD INDUSTRIES, INC. UH-12A accident near Bern Flughafen (LSZB), BE, CH?

A training flight ended in a sudden roll and crash of a Hiller UH-12A helicopter due to a failure in the rotor control linkage.

What aircraft was involved and where did it happen?

The accident on 1963-09-21 involved a FAIRCHILD INDUSTRIES, INC. UH-12A, registration HB-XBS, at Bern Flughafen (LSZB), BE, CH.

What was the probable cause of the accident?

The accident was caused by the failure of the right-hand rotor control rod connection because the securing bolt was not properly immobilized by a nut and split pin.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/139.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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