CEN09CA180

NTSB accident investigation · Robinson Helicopter R22 Beta · O'Donnell, TX · February 25, 2009

Accident · Minor injuriesData collectionFinal report
Date
February 25, 2009, 14:00 local (20:00 UTC)
Place
O'Donnell, TX
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N387ACRobinson Helicopter R22 Beta
Defining event
Maneuvering-hover: Loss of lift
Weather
Visual (VMC) · Day
Status
Completed · report May 12, 2009
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration, FSDO
FAA report
20090225001419A
Case key
73410

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot's failure to maintain control while performing a quick stop maneuver to an out of ground effect (OGE) hover. Contributing to the accident was the high density altitude and near calm wind condition.

Findings · 6

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Temp/humidity/pressure: high density altitudeEnvironmental issues › Conditions/weather/phenomena · Effect on operationRobinson Helicopter R22 BETA: 7 casesAll aircraft: 278 casesProbable cause
WindEnvironmental issues › Conditions/weather/phenomena · Effect on operationRobinson Helicopter R22 BETA: 1 caseAll aircraft: 110 casesProbable cause
Performance/control parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedRobinson Helicopter R22 BETA: 20 casesAll aircraft: 1,269 casesProbable cause
AircraftAircraft › Aircraft propeller/rotor · Capability exceededRobinson Helicopter R22 BETA: 1 caseAll aircraft: 11 cases

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot was conducting a predator control mission when he spotted wild hogs in an approximate 20-acre field of Salt Cedar trees. The pilot made a quick stop at an out-of-ground effect (OGE) hover in an attempt to move the hogs out in the open. The pilot stated that the low rotor RPM horn and light activated. He immediately stopped to regain rotor RPM. As the aircraft approached the edge of the trees towards an open field, the wind stopped and the rotor dropped to approximately 90 percent. The pilot observed an increase in airframe vibration followed by a hard left roll. The helicopter main rotor blades struck the ground in a 90-degree bank and came to rest on its left side. The pilot was not injured and the passenger sustained minor injuries. The pilot stated that the approximate gross weight at the time of the accident was 1,370 pounds. The helicopter performance charts indicated maximum weight for out of ground effect hover was 1,320 pounds for the weather conditions.

Factual narrative

The pilot was conducting a predator control mission when he spotted wild hogs in an approximate 20-acre field of Salt Cedar trees. The pilot made a quick stop at an out-of-ground effect (OGE) hover in an attempt to move the hogs out in the open. The pilot stated that the low rotor RPM horn and light activated. He immediately stopped to regain rotor RPM. As the aircraft approached the edge of the trees towards an open field, the wind stopped and the rotor dropped to approximately 90 percent. The pilot observed an increase in airframe vibration followed by a hard left roll. The helicopter main rotor blades struck the ground in a 90-degree bank and came to rest on its left side. The pilot was not injured and the passenger sustained minor injuries. The pilot stated that the approximate gross weight at the time of the accident was 1,370 pounds. The helicopter performance charts indicated maximum weight for out of ground effect hover was 1,320 pounds for the weather conditions.

Aircraft

Registration
N387AC
Reported as
Robinson Helicopter R22 Beta
Category
Helicopter
Serial number
1631
Airframe hours
1,756
Engine
Lycoming 0-320 SERIES, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Other work use · Part 91
Airworthiness certificate
Standard, Normal
Departed
2F5 · Lemesa, TX
Destination
2F5 · Lemesa, TX
Flight plan
Unknown
Airport
2F5 · Lamesa Municipal Airport

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
59
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, With waivers/limitations
Last flight review
November 1, 2008
Seat
Right
Flight hours
16,000 total · 4,000 in this make and model · 10 in the last 90 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 45 °F
Altimeter
30.00 inHg
Observed at
KGNC, 37 nm away

Docket · 1

The files NTSB released with the investigation on April 1, 2009, on NTSB’s docket system: statements, records, photos and specialists’ reports. 266 KB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.