N993RW

Substantial
None

Robinson R22 Beta IIS/N: 3507

Accident Details

Date
Tuesday, June 7, 2005
NTSB Number
DEN05CA085
Location
Wallsburg, UT
Event ID
20050707X00956
Coordinates
40.235000, -111.231109
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the flight instructor's inadequate in-flight planning and decision making and failure to maintain aircraft control. Contributing factor's include the flight instructor's inadequate supervision of the flight, the student pilot's failure to maintain rotor rpm, the high density altitude, and the muddy terrain.

Aircraft Information

Registration
N993RW
Make
ROBINSON
Serial Number
3507
Engine Type
Reciprocating
Year Built
2003
Model / ICAO
R22 Beta IIR22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SILVER STATE HELICOPTERS LLC
Address
PO BOX 95695
Status
Deregistered
City
LAS VEGAS
State / Zip Code
NV 89193-5695
Country
United States

Analysis

On June 7, 2005, approximately 1500 mountain daylight time, a Robinson R22 Beta II, N993RW, operated by Silver State Helicopters LLC., was substantially damaged when it impacted terrain 10 miles southeast of Wallsburg, Utah. Visual meteorological conditions prevailed at the time of the accident. The local instructional flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The commercial certificated flight instructor and commercial certificated pilot receiving instruction (hereafter referred to as the student) reported no injuries. The local flight departed Provo, Utah, approximately 1430.

According to the accident report submitted by the flight instructor, they were practicing confined area approach procedures. In a separate statement s the student, stated that during the approach he "started to pull up on the collective," at which time the rpm began to decay. The flight instructor stated he took control of the helicopter and initiated a low rotor rpm recovery. Normal rotor rpm returned, but a significant loss of altitude had occurred so the flight instructor elected to land. The instructor stated that, after landing, he initiated a vertical climb to "establish power capability" and then descended back down to "start their climb." As a positive climb rate was established, the flight instructor attempted to gain forward speed to help the climb rate. The helicopter began sinking so he maneuvered down to the ground at which time the right skid of the helicopter "sunk into the mud," and the helicopter rolled over.

Both the main rotor and the tail rotor blades were bent, the left skid was bent under the helicopter, and the fuselage was wrinkled. An examination of the helicopter's systems revealed no anomalies.

The accident site elevation was estimated to be 8,000 feet msl. The calculated density altitude varied between 8,916 feet and 9,732 feet.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN05CA085