N311RM

Substantial
None

Parker Rotorway 162FS/N: 6271

Accident Details

Date
Wednesday, May 16, 2001
NTSB Number
CHI01LA141
Location
MINNEAPOLIS, MN
Event ID
20010524X01015
Coordinates
45.189682, -93.549232
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The tail rotor drive belt coming off in cruise flight and it not being possible for the student pilot to maintain aircraft control during the emergency landing attempt. Factors relating to the accident were the loose bearing in the secondary drive unit to the tail rotor, the attempted autorotation and run on landing by the student pilot, and the low altitude.

Aircraft Information

Registration
N311RM
Make
PARKER
Serial Number
6271
Model / ICAO
Rotorway 162F

Registered Owner (Historical)

Name
PARKER ROGER L
Address
9356 N 700 W LOT 2
Status
Deregistered
City
ROANN
State / Zip Code
IN 46974-9712
Country
United States

Analysis

On May 16, 2001, at 1110 central daylight time, a Parker Rotorway 162F helicopter, N311RM, operated by a student pilot, sustained substantial damage when it impacted into a field 15 miles northwest of Minneapolis, Minnesota, during an emergency landing. Prior to the emergency landing attempt, the helicopter experienced a tail rotor malfunction. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of 14 CFR Part 91. There was no flight plan on file. The student pilot operating the helicopter reported no injuries. The local flight originated from the pilot's residence at Rogers, Minnesota, at 1045.

In his written statement, the student pilot said that he was returning to Rogers, Minnesota, when he heard a "pop" and then the helicopter yawed left. The student pilot said that he lost pedal control and entered a turning autorotation. He said that at approximately 35 feet above the ground, he introduced some aft cyclic in an attempt to perform a run on landing. He said that the helicopter "spun violently to [the] right". The student pilot said he added full left [control pedal] and down cyclic. The helicopter dropped to the ground.

A Federal Aviation Administration inspector examined the helicopter at the student pilot's residence. The inspector observed that both skids were collapsed, the tail boom was bent upward, the bottom vertical stabilizer was crushed upward, and the tail rotor was bent aft. Control continuity was confirmed. An examination of the helicopter's belt drive system revealed that the lower shaft bearing in the secondary drive unit to the tail rotor was loose and the tail rotor drive belt had come off.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI01LA141