WPR09CA023

NTSB accident investigation · Robinson Helicopter R22 Beta · Temecula, CA · October 22, 2008

Accident · No injuriesData collectionFinal report
Date
October 22, 2008, 12:00 local (19:00 UTC)
Place
Temecula, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N8356RRobinson Helicopter R22 Beta
Defining event
Landing-flare/touchdown: Hard landing
Weather
Visual (VMC) · Day
Status
Completed · report December 24, 2008
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administrtion
FAA report
20081022850219A
Case key
69346

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 certified flight instructor's failure to maintain adequate rotor rpm during a simulated approach to landing under variable wind, and high density altitude conditions.

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.

Performance/control parameters: prop/rotor parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedRobinson Helicopter R22 BETA: 37 casesAll aircraft: 182 casesProbable cause
Temp/humidity/pressure: high density altitudeEnvironmental issues › Conditions/weather/phenomena · Effect on equipmentRobinson Helicopter R22 BETA: 7 casesAll aircraft: 278 casesProbable cause
Wind: variable windEnvironmental issues › Conditions/weather/phenomena · Response/compensationRobinson Helicopter R22 BETA: 2 casesAll aircraft: 113 casesProbable cause
Use of equip/info: use of equip/systemPersonnel issues › Task performance · Instructor/check pilotRobinson Helicopter R22 BETA: 16 casesAll aircraft: 1,391 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 certified flight instructor (CFI) was showing the student how to make a landing approach to 2,500-foot mean sea level hilly terrain. The student had about 13 hours of total flying experience, and the CFI was handling the controls. According to the CFI, the first approach to the landing site was uneventful. During the second approach the low rotor rpm warning horn activated. The CFI reported that he tried to "milk collective and get it back," but he was not successful. The CFI opined that the wind direction may have changed, and he attempted to redirect the helicopter's course into the wind. The CFI was unable to regain rpm and stop the descent. The helicopter impacted the field and rolled over. The CFI reported that when the accident occurred, the helicopter was operating near its maximum certificated gross weight. The out of ground effect hover ceiling was about 3,000 feet, and the density altitude was about 3,200 feet.

Factual narrative

During the accident flight, the certified flight instructor (CFI) was providing dual instruction to his student. The CFI was showing the student how to make a landing approach over 2,500-foot mean sea level hilly terrain. The student had about 13 hours of total flying experience, and the CFI was handling the controls. According to the CFI, the first approach to the landing site was uneventful. During the second approach the low rotor rpm warning horn activated. In the CFI's original statement to the Federal Aviation Administration and National Transportation Safety Board, the CFI reported that he tried to "milk collective and get it back," but he was not successful. The CFI opined that the wind direction may have changed, and he attempted to redirect the helicopter's course into the wind. The CFI was unable to regain rpm and stop the descent. The helicopter impacted the field and rolled over. The CFI reported that when the accident occurred, the helicopter was operating near its maximum certificated gross weight. The out of ground effect hover ceiling was about 3,000 feet, and the density altitude was about 3,200 feet.

Aircraft

Registration
N8356R
Reported as
Robinson Helicopter R22 Beta
Category
Helicopter
Serial number
2729
Airframe hours
4,276
Engine
Lycoming 0-360-A1D, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
USA Academy of Aviation
Registered owner
Carter Richard K DBA
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · September 7, 2008
Departed
F70 · Murrieta, CA
Destination
F70 · Murrieta, CA

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
57
Injuries
None
Certificates
Commercial, Flight instructor
Medical
Class 2, With waivers/limitations
Last flight review
October 10, 2008
Seat
Left
Flight hours
10,024 total · 9,488 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
350° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
79 °F
Altimeter
30.01 inHg
Observed at
F70

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 N8356R · 1

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