WPR13CA068

NTSB accident investigation · Robinson R22 · Logan, UT · December 15, 2012

Accident · No injuriesData collectionFinal report
Date
December 15, 2012, 13:45 local (20:45 UTC)
Place
Logan, UT
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Emergency descent
Aircraft
N393LERobinson R22
Defining event
Autorotation: Loss of lift
Weather
Visual (VMC) · Day
Status
Completed · report April 3, 2013
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20121215027449A
Case key
85819

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 flight instructor’s delayed remedial action and inadequate supervision during a practice autorotation, which resulted in a failure to maintain adequate main rotor rpm. Contributing to the accident was the wet landing surface.

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
Attention/monitoring: monitoring other personPersonnel issues › Psychological · Instructor/check pilotRobinson Helicopter R22 BETA: 15 casesAll aircraft: 200 casesProbable cause
Action: delayed actionPersonnel issues › Action/decision · Instructor/check pilotRobinson Helicopter R22 BETA: 35 casesAll aircraft: 894 casesProbable cause
Runway/land/takeoff/taxi surface: wet surfaceEnvironmental issues › Physical environment · Contributed to outcomeRobinson Helicopter R22 BETA: 1 caseAll aircraft: 141 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

During the 180-degree autorotation, the student pilot maintained an airspeed of 65 knots, with rotor rpm in the green. As the student rolled out of the turn about 300 feet above ground level and at 70 knots, the rotor rpm continued to remain in the green. However, before the flare, the rotor rpm began to decay and failed to build as the flare was entered. The flight instructor then took control of the helicopter and immediately rolled on throttle to recover engine power and to maintain rotor rpm, but there was insufficient engine power to recover, and the low rotor rpm light and horn activated. Because power was not available for a full-power-on landing, the flight instructor initiated a full-down autorotation to a taxiway. During the landing, the helicopter skidded across and off the wet taxiway into loose gravel and mud before the left skid dug into the ground, resulting in the helicopter rolling over and coming to rest on its left side. The helicopter sustained substantial damage to its welded frames, firewall, and tail cone. The flight instructor reported no preaccident mechanical or malfunctions or failures with the helicopter or flight controls that would have precluded normal operation.

Factual narrative

During the 180-degree autorotation the student maintained 65 knots with the rotor revolutions per minute (RPM) in the green. As the student rolled out of the turn at about 300 feet above ground level and at 70 knots, the rotor rpm continued to remain in the green. However, prior to the flare the rotor RPM began to decay and failed to build as the flare was entered. The flight instructor then took control of the helicopter and immediately rolled on throttle to recover engine [power] and to maintain [rotor] RPM, but there was insufficient engine power to recover the decayed rotor RPM; this was followed by a low rotor RPM light and horn. As power was not available for a full power on landing, the flight instructor initiated a full down autorotation to a taxiway. During the landing the helicopter skidded across and off the wet taxiway into loose gravel and mud before the left skid dug into the ground. This resulted in the aircraft rolling over and coming to rest on its left side. The helicopter sustained substantial damage to its welded frames, firewall, and tail cone. The flight instructor reported no mechanical malfunctions or failures with the helicopter or flight controls that would have precluded normal operation.

Aircraft

Registration
N393LE
Reported as
Robinson R22 (BETA)
Category
Helicopter
Serial number
4393
Airframe hours
3,007
Engine
Lycoming O-360, 145 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Mountain Ridge Helicopters
Registered owner
Mountain Ridge Helicopters
Airworthiness certificate
Standard, Normal
Last inspection
Annual · December 11, 2012 · 27 hours before
Departed
LGU · Logan, UT
Destination
LGU · Logan, UT
Airport
LGU · Logan-Cache Airport, runway 35, 9,010 × 100 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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
23
Injuries
None
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 1, Without waivers/limitations
Last flight review
July 7, 2011
Seat
Left
Flight hours
651 total · 589 in this make and model · 590 as pilot in command · 129 in the last 90 days · 41 in the last 30 days
Role
Student pilot
Age
27
Injuries
None
Certificate
Student
Medical
Class 3, Without waivers/limitations
Seat
Right
Flight hours
62 total · 62 in this make and model · 7 as pilot in command · 62 in the last 90 days · 26 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
5,000 ft overcast
Temperature
43 °F, dew point 28 °F
Altimeter
29.79 inHg
Observed at
LGU

Docket · 4

The files NTSB released with the investigation on January 16, 2013, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.2 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 N393LE · 1

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