N208WM

Substantial
Serious

ROBINSON HELICOPTER R22 BETAS/N: 4397

Accident Details

Date
Friday, August 17, 2012
NTSB Number
WPR12LA362
Location
Spanish Fork, UT
Event ID
20120818X44210
Coordinates
40.141387, -111.661109
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The flight instructor’s delayed remedial action and inadequate supervision during a practice autorotation, which resulted in a hard landing and rollover.

Aircraft Information

Registration
N208WM
Make
ROBINSON HELICOPTER
Serial Number
4397
Engine Type
Reciprocating
Year Built
2008
Model / ICAO
R22 BETAR22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
ZBURA HELICOPTERS LLC
Address
11202 S LOAFER CANYON RD
Status
Deregistered
City
ELK RIDGE
State / Zip Code
UT 84651-4520
Country
United States

Analysis

On August 17, 2012, at 1642 mountain daylight time, a Robinson R22 Beta II, N208WM, sustained substantial damage subsequent to a hard landing and rollover at the Spanish Fork - Springville Municipal Airport, Spanish Fork, Utah. The certified flight instructor (CFI) sustained serious injuries and the student pilot receiving instruction sustained minor injuries. The helicopter was registered to Zbura Helicopters, LLC, and operated by Utah Helicopters as an instructional flight under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the local flight that departed Spanish Fork about 45 minutes prior the accident.

The purpose of the instructional flight was, in part, to practice autorotations. The student pilot reported that they had completed multiple straight-in autorotations followed by an autorotation from a 180-degree turn. He reported that during the turning maneuver, the main rotor RPM decayed and the helicopter's descent rate increased; the helicopter subsequently touched down hard and rolled over.

In a written statement the CFI reported they began the autorotation at 5,200 feet MSL at 65 knots. He reported the student started the maneuver by initiating a descending "hard" right turn. Shortly thereafter, the low rotor light illuminated and the low rotor horn sounded. In response, the CFI instructed the student through the maneuver by adding left cyclic and decreasing the airspeed and sink rate. He reported they recovered the horn, however, the helicopter's sink rate was excessive and he took the controls. He reported the rotor seemed as if it was not responding to inputs and the helicopter's sink rate was "pretty fast." The helicopter lost considerable altitude in the turn and unable to reach the intended touchdown point the CFI rolled the throttle "on" and flared in the short amount of distance between the helicopter and the ground. The helicopter subsequently touched down hard and rolled over.

A pair of sun glasses worn by the CFI was found at the accident site. The I-KAM XTREME Video Glasses contained a digital camera incorporated into the bride of the frame. The sunglasses were shipped to the NTSB's Vehicle Recorder Division for video and audio file extraction. Five individual files, one that captured the accident sequence, were extracted. The On Board Image Recorder Factual Report outlining the data can be found in the docket for this accident case file.

The CFI reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR12LA362