N780SH

Substantial
None

Robinson Helicopter Company R22S/N: 3612

Accident Details

Date
Tuesday, February 22, 2005
NTSB Number
DEN05LA061
Location
Spanish Fork, UT
Event ID
20050311X00297
Coordinates
40.141666, -111.618614
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the student's failure to maintain control of the helicopter. Contributing factors were high airspeed, high rate of descent, the instructor's delay in taking remedial action, and the instructor's inadequate supervision of the flight.

Aircraft Information

Registration
N780SH
Make
ROBINSON HELICOPTER COMPANY
Serial Number
3612
Engine Type
Reciprocating
Year Built
2004
Model / ICAO
R22R22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
PO BOX 2179
STOKE
Status
Deregistered
City
NELSON 7041
Country
United States

Analysis

On February 22, 2005, approximately 0840 mountain standard time, a Robinson Helicopter Company R22, N780SH, operated by Silver State Helicopters, Inc. was substantially damaged during a hard landing at Spanish Fork-Springville Airport (U77), Spanish Fork, Utah. Visual meteorological conditions prevailed at the time of the accident. The instructional flight was being operated under the provisions of Title 14 CFR Part 91 without a flight plan. The flight instructor and his student reported no injuries. The local flight originated at 0730.

According to the accident report submitted by the flight instructor, he and his private certificated student were practicing 180 degree simulated autorotation maneuvers at U77. The first two maneuvers were performed on runway 12 at 800 feet agl, airspeed 70 knots. As they set up the helicopter for the third simulated autorotation, the instructor noted that the altitude was 700 feet agl and he explained to the student that he "would have to turn it a little bit tighter due to the 100' less of altitude." In the last 90 degrees of turn, the student "allowed the nose to drop and the airspeed increased to 80 knots." The student flared for landing and the "helicopter began to cavitate." The instructor assumed control, trying to dissipate airspeed and decrease the high rate of descent that had developed. As the instructor continued the flare, the helicopter shutter increased and rate of sink continued. The instructor applied forward cyclic and the helicopter contacted the runway and bounced approximately 10 feet into the air. The instructor then hovered the helicopter to a safe location where the engine could be shut down.

The tail boom was bent down during the impact, wrinkling the bottom portion of the number 2 bay. Both skid cross tubes were bent up towards the fuselage and aft. A post-accident examination of the helicopter systems, conducted by the FAA, revealed no anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN05LA061