WPR11CA264

NTSB accident investigation · Robinson Helicopter R22 Beta · Prescott, AZ · June 18, 2011

Accident · No injuriesData collectionFinal report
Date
June 18, 2011, 11:30 local (18:30 UTC)
Place
Prescott, AZ
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Taxi
Aircraft
N334DCRobinson Helicopter R22 Beta
Defining event
Taxi-into takeoff position: Loss of tail rotor effectiveness
Weather
Visual (VMC) · Day
Status
Completed · report August 11, 2011
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20110618012479A
Case key
80810

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

On this page

Probable cause

The pilot's inadequate compensation for the wind conditions and failure to maintain directional control of the helicopter during taxi, resulting in a loss of tail rotor effectiveness and a subsequent hard landing.

Findings · 4

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.

Wind: tailwindEnvironmental issues › Conditions/weather/phenomena · Effect on equipmentRobinson Helicopter R22 BETA: 5 casesAll aircraft: 594 cases
Wind: tailwindEnvironmental issues › Conditions/weather/phenomena · Response/compensationRobinson Helicopter R22 BETA: 5 casesAll aircraft: 594 casesProbable cause
Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedRobinson Helicopter R22 BETA: 14 casesAll aircraft: 3,958 casesProbable cause

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 instructor reported that his student was taxiing the helicopter in a north direction along a taxiway parallel to the runway with a near direct tailwind of 10 knots with gusts to 19. The student started to lose tail rotor authority over the helicopter. At this time the instructor took control of the helicopter and proceeded to apply full left pedal until he regained tail rotor authority and directional control. Because of the strong wind from the south, the instructor opted to keep control of the helicopter until they were airborne and he proceeded to continue their taxi to the displaced threshold of the runway. Upon reaching the displaced threshold, the instructor started a 220 degree turn to the left in order to line up with a takeoff direction to the south into the wind. The instructor reported that half way through the turn the helicopter violently yawed to the left, and he applied full right pedal to cancel the yaw but was unable to arrest the helicopter's left yawing moment. The helicopter landed hard on the skids, damaging the main rotor and severing the tail boom aft of the tail rotor blades hazard guard and before the tail rotor transmission. The pilot reported no mechanical issues with the helicopter prior to the flight. The wind limitation listed in the Pilot's Operating Handbook for the helicopter is 25 knots including any gust factor.

Factual narrative

The instructor reported that his student was taxing the helicopter in a north direction along a taxiway parallel to runway 12/30 with a near direct tailwind of 10 knots with gusts to 19. The student started to lose tail rotor authority over the helicopter. At this time the instructor took control of the helicopter and proceeded to apply full left pedal until they regained tail rotor authority and directional control. Because of the strong winds from the south, the instructor opted to keep control of the helicopter until they were airborne and he proceeded to continue their taxi to the displaced threshold of runway 12. Upon reaching the displaced threshold, the instructor started a 220 degree turn to the left in order to line up with a takeoff direction to the south into the wind. The instructor reported that half way through the turn the helicopter violently yawed to the left, and he applied full right pedal to cancel the yaw but was unable to arrest the helicopters left yawing moment. The helicopter landed hard on the skids, damaging the main rotor and severing the tail boom aft of the tail rotor blades hazard guard and before the tail rotor transmission. The pilot reported no mechanical issues with the helicopter prior to the flight. The wind limitation listed in the Pilot's Operating Handbook for the helicopter is 25 knots including any gust factor.

Aircraft

Registration
N334DC
Reported as
Robinson Helicopter R22 Beta
Category
Helicopter
Serial number
3511
Airframe hours
4,352
Engine
Lycoming O-360 SERIES, 124 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Guidance Helicopters Inc
Registered owner
Guidance Helicopters Inc
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · May 12, 2011 · 89 hours before
Departed
KPRC · Prescott, AZ
Destination
KPRC · Prescott, AZ
Airport
KPRC · Ernest H Love Field, runway 12, 4,408 × 75 ft, asphalt

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
Flight instructor
Age
31
Injuries
None
Certificate
Commercial
Medical
Class 2, With waivers/limitations
Last flight review
December 1, 2010
Seat
Left
Flight hours
339 total · 187 in this make and model · 234 as pilot in command · 85 in the last 90 days · 49 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
170° at 10 knots, gusting 19
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 19 °F
Altimeter
30.04 inHg
Observed at
KPRC, 1 nm away

Docket · 4

The files NTSB released with the investigation on June 24, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 10.4 MB 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.

Other investigations on N334DC · 1

Matched to the same aircraft by N-number and date.