WPR12CA117

NTSB accident investigation · Robinson Helicopter R22 Beta · Randle, WA · March 8, 2012

Accident · No injuriesData collectionFinal report
Date
March 7, 2012, 17:05 local (Mar 8, 2012, 01:05 UTC)
Place
Randle, WA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N54BARobinson Helicopter R22 Beta
Defining event
Landing: Collision during takeoff/land
Weather
Visual (VMC) · Day
Status
Completed · report May 15, 2012
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20120307002609A
Case key
82969

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 exceeded the helicopter's performance, resulting in low rotor rpm and settling.

Findings · 2

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.

Terrain: mountainous/hilly terrainEnvironmental issues › Physical environment · Contributed to outcomeRobinson Helicopter R22 BETA: 3 casesAll aircraft: 329 cases
Aircraft capability: climb capabilityAircraft › Aircraft oper/perf/capability · Capability exceededRobinson Helicopter R22 BETA: 2 casesAll aircraft: 183 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 preparing the flying pilot for his commercial helicopter check flight. They were practicing pinnacle and confined-area landings to a small elevated U.S. Forest Service landing platform located along a 4,750-foot mean sea level (msl) ridgeline. The helicopter performance tables indicated a maximum out-of-ground-effect hover altitude of 6,000 feet msl, based on helicopter weight and environmental conditions. The pilot made a very shallow approach to the landing platform and established a hover. At this time, the engine manifold pressure increased, and the low rotor rpm horn sounded. The helicopter settled onto the landing platform, and the flying pilot said to the CFI that the landing skid on his side was not on the platform. He maneuvered the helicopter forward off the platform and downslope. The low rotor rpm horn stopped sounding, and the helicopter increased its forward speed but did not increase its altitude. The right skid caught some snow, and the helicopter flipped over. The helicopter came to rest facing uphill on its left side with damage to the tailboom and main rotor blades. The CFI stated that the helicopter had no mechanical malfunctions or failures during the flight.

Factual narrative

The certified flight instructor (CFI) was preparing the flying pilot for his commercial helicopter check flight. They were practicing pinnacle and confined area landings to a small elevated Forrest Service landing platform located along a 4,750-foot mean sea level (msl) ridge line. The helicopter performance tables indicated, based on helicopter weight and environmental conditions, a maximum out of ground effect hover altitude of 6,000 feet msl. The pilot made a very shallow approach to the landing platform, and established a hover. At this time the engine manifold pressure increased, and the low rotor rpm horn sounded. The helicopter settled onto the landing platform and the flying pilot said to the CFI that the landing skid on his side was not on the platform. He maneuvered the helicopter forward off the platform, and downslope. The low rotor rpm horn stopped sounding, and the helicopter increased forward speed but did not increase in altitude. The right skid caught some snow and the helicopter flipped over. The helicopter came to rest facing uphill on it's left side with damage to the tail boom and main rotor blades. The CFI stated that the helicopter had no mechanical malfunctions or failures during the flight.

Aircraft

Registration
N54BA
Reported as
Robinson Helicopter R22 Beta
Category
Helicopter
Serial number
1888
Airframe hours
5,640
Engine
Lycoming O-320 SERIES, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Glacier Aviation
Registered owner
Carter Richard K
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · December 13, 2011
Departed
KN55 · Randle, WA
Destination
KN55 · Randle, WA
Flight plan
Unknown
Airport
KN55 · Randal-Kiona

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
47
Injuries
None
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 2, With waivers/limitations
Last flight review
August 1, 2011
Seat
Left
Flight hours
975 total · 569 in this make and model
Role
Pilot
Age
38
Injuries
None
Certificate
Private
Instrument ratings
Helicopter
Medical
Class 2, With waivers/limitations
Seat
Right
Flight hours
158 total · 142 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
340° at 3 knots
Temperature
46 °F, dew point 27 °F
Altimeter
30.43 inHg
Observed at
KPLU, 37 nm away

Docket · 2

The files NTSB released with the investigation on April 4, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 822 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.

Other investigations on N54BA · 1

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