CEN09CA271

NTSB accident investigation · Robinson Helicopter R22 Beta · Harlingen, TX · April 29, 2009

Accident · No injuriesData collectionFinal report
Date
April 29, 2009, 13:52 local (18:52 UTC)
Place
Harlingen, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Standing
Aircraft
N2560QRobinson Helicopter R22 Beta
Defining event
Standing-engine(s) operating: Miscellaneous/other
Weather
Visual (VMC) · Day
Status
Completed · report August 13, 2009
Report
Approved by Office Director
NTSB office
Central Region
Parties
FAA FSDO
Case key
73752

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 decision to leave the helicopter unattended with the engine running in gusty wind conditions.

Findings · 3

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.

Performance/control parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedRobinson Helicopter R22 BETA: 20 casesAll aircraft: 1,269 casesProbable cause
Wind: gustsEnvironmental issues › Conditions/weather/phenomena · Effect on operationRobinson Helicopter R22 BETA: 13 casesAll aircraft: 1,199 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

After landing the helicopter, the pilot set the cyclic and collective friction locks and left the helicopter "running" while he and his passenger disembarked the helicopter. After being left unattended for about two minutes, the helicopter began to lift-off and subsequently impacted terrain resulting in substantial damage. The pilot reported that the friction locks were still found engaged after the helicopter impacted the terrain. Winds in the vicinity of the accident were from the southeast at 21 gusting to 30 knots. According to the manufacturer, the cyclic and collective frictions are designed to allow the pilot to remove their hands from the controls to perform the cockpit portion of the preflight and post flight operations. A "caution" in the manufacturer's pilot operating handbook states, "Never leave helicopter flight controls unattended while engine is running." In addition the pilot operating handbook has a safety notice issued November 1984, which states, "Never exit helicopter with engine running. Several accidents have occurred when pilot momentarily left their helicopters unattended with the engine running and rotors turning. The collective can creep up, increasing both pitch and throttle, allowing the helicopter to lift off or roll out of control."

Factual narrative

After landing the helicopter, the pilot set the cyclic and collective friction locks and left the helicopter "running" while he and his passenger disembarked the helicopter. After being left unattended for about two minutes, the helicopter began to lift-off and subsequently impacted terrain resulting in substantial damage. The pilot reported that the friction locks were still found engaged after the helicopter impacted the terrain. Winds in the vicinity of the accident were from the southeast at 21 gusting to 30 knots. According to the manufacturer, the cyclic and collective frictions are designed to allow the pilot to remove their hands from the controls to perform the cockpit portion of the preflight and postflight operations. A "caution" in the manufacturer's pilot operating handbook states, "Never leave helicopter flight controls unattended while engine is running." In addition, the pilot operating handbook has a safety notice issued November 1984, which states, "Never exit helicopter with engine running. Several accidents have occurred when pilot momentarily left their helicopters unattended with the engine running and rotors turning. The collective can creep up, increasing both pitch and throttle, allowing the helicopter to lift off or roll out of control."

Aircraft

Registration
N2560Q
Reported as
Robinson Helicopter R22 Beta
Category
Helicopter
Serial number
0614
Engine
Lycoming O-320 SERIES, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Departed
Harlingen, TX
Destination
Harlingen, TX

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
50
Injuries
None
Certificate
Commercial
Medical
Class 2, With waivers/limitations
Flight hours
14,000 total · 10,000 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
150° at 21 knots, gusting 30
Visibility
10 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 66 °F
Altimeter
29.96 inHg
Observed at
HRL

Docket · 2

The files NTSB released with the investigation on June 4, 2009, on NTSB’s docket system: statements, records, photos and specialists’ reports. 39 KB in all.