No fatalities

8 Nov 2014: MOSIER ROBERT S MOSQUITO XET NO SERIES (N922RM) — Charles Burgoon — Angleton, TX

Angleton, TX, United States

On 8 Nov 2014, a MOSIER ROBERT S MOSQUITO XET NO SERIES (registration N922RM) operated by Charles Burgoon was involved in an aviation accident near Angleton, TX. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain adequate clearance from trees during a precautionary landing. Contributing to the accident was the pilot’s inadequate preflight inspection during which he failed to detect a loose drive belt, which resulted in an in-flight… This summary draws on records from NTSB.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On November 8, 2014, a Composite FX Mosquito XET helicopter, N922RM, struck trees during approach at Bailes Airport in Angleton, Texas. The pilot sustained minor injuries and the helicopter was substantially damaged. Examination revealed a loose drive belt due to excessive pulley wear.

Accident Details

On November 8, 2014, about 1000 central standard time, a Composite FX Mosquito XET helicopter, registration N922RM, impacted trees during approach for landing at Bailes Airport (7R9), Angleton, Texas. The pilot sustained minor injuries and the helicopter was substantially damaged. The helicopter was registered to and operated by the pilot under 14 Code of Federal Regulations Part 91 as a personal flight. Day visual meteorological conditions prevailed, and the local flight departed without a flight plan.

Pilot Account

According to the pilot, while in a crosswind turn at about 300 feet above ground level, the helicopter abruptly shuddered. The pilot lowered the collective control, entered an autorotation, and turned back toward the airport. As he approached the runway area, the helicopter skids passed over a row of trees by about 5 to 10 feet. Immediately after the skids cleared these trees, the pilot began a cyclic flare, which resulted in the tail rotor striking a tree. The helicopter then began to spin violently and impacted the ground several times, damaging the main rotor and tail boom.

Examination Findings

The helicopter was examined by Federal Aviation Administration and Composite FX personnel at the kit manufacturer's facility. The belt for the secondary drive reduction unit was observed to be loose, which allowed the teeth of the drive belt to "jump" the drive cogs on the pulley. The loose belt was due to excessive wear on the pulley. The operating manual pre-flight inspection includes a check for tension of this belt, during which the operator should attempt to deflect the belt by about 3/16 of an inch, with an estimated five pounds of finger pressure in the middle of a long, unsupported span of the belt.

Registration and Operator

The helicopter, N922RM, was registered to and operated by the pilot at the time of the incident.

Contributing factors

PilotAltitude — Not attained/maintainedAwareness of condition