N1122R

Substantial
None

Robinson R22BS/N: 3197

Accident Details

Date
Sunday, January 16, 2005
NTSB Number
LAX05CA071
Location
Rialto, CA
Event ID
20050216X00198
Coordinates
34.124168, -117.400833
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 pilot's improper use of the cyclic control during a practice autorotation, and the inadequate supervision by the certified flight instructor.

Aircraft Information

Registration
N1122R
Make
ROBINSON
Serial Number
3197
Engine Type
Reciprocating
Year Built
2001
Model / ICAO
R22BR22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
ROBINSON HELICOPTER CO INC
Address
2901 AIRPORT DR
Status
Deregistered
City
TORRANCE
State / Zip Code
CA 90505-6115
Country
United States

Analysis

On January 16, 2005, at 1340 Pacific standard time, a Robinson R22B, N1122R, experienced main rotor contact with the tailboom during a practice full-touchdown autorotation at the Rialto Municipal Airport, Rialto, California. Universal Air Academy was operating the helicopter, registered to a private company, under the provisions of 14 CFR Part 91. The certified flight instructor (CFI) and the commercial pilot-undergoing-instruction (PUI) were not injured; the helicopter sustained substantial damage. The CFI and PUI departed from the El Monte Airport, El Monte, California, about 1300 for the local area instructional flight. Visual meteorological conditions prevailed, and no flight plan had been filed.

The CFI submitted National Transportation Safety Board (NTSB) Form 6120.1/2, the Pilot/Operator Report. He said that the purpose of the flight was to prepare the PUI for his CFI checkride, and they were performing full touchdown autorotations. The helicopter was aligned with the centerline of the south taxiway. Approximately 200 feet above ground level (agl), the CFI noted the following performance indications: main rotor rpm "in the green," airspeed 6 knots; and descent rate 1,300 feet per minute. At 60 feet agl, the PUI flared the helicopter and then leveled it for a full touchdown autorotation. When the helicopter was 1 foot agl, the PUI pushed the cyclic forward and the forward tips of the skids touched the ground. The helicopter then rotated aft, and the CFI assumed the controls and leveled the helicopter. Upon touchdown, the main rotor blades contacted the tailboom. The CFI noted no mechanical malfunctions with the helicopter.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX05CA071