ERA12CA137

NTSB accident investigation · Robinson Helicopter R22 Beta · St Petersburg, FL · January 6, 2012

Accident · No injuriesData collectionFinal report
Date
January 6, 2012, 15:53 local (20:53 UTC)
Place
St Petersburg, FL
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Uncontrolled descent
Aircraft
N8066URobinson Helicopter R22 Beta
Defining event
Uncontrolled descent: Miscellaneous/other
Weather
Visual (VMC) · Day
Status
Completed · report November 7, 2012
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
Case key
82632

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 during the pilot-receiving-instruction's practice autorotation that developed a high rate of descent. Contributing to the accident was the pilot-receiving-instruction's improper control inputs during the practice autorotation.

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.

Action: delayed actionPersonnel issues › Action/decision · Instructor/check pilotRobinson Helicopter R22 BETA: 35 casesAll aircraft: 894 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

According to the helicopter flight instructor, he was preparing a helicopter-rated commercial pilot for his helicopter flight instructor check ride. After the pilot receiving instruction completed a straight-in autorotation, the flight instructor demonstrated a throttle-off, 180-degree autorotation from 600 feet above ground level (agl). The pilot receiving instruction then attempted the same maneuver, but during the entry, the helicopter airspeed became slow while the rotor rpm remained "in the green." The pilot receiving instruction lowered the nose of the helicopter, which increased airspeed. As the helicopter turned onto final approach at an altitude of about 300 feet agl, the flight instructor advised the pilot receiving instruction to ease back on the cyclic while raising the collective to maintain rotor rpm. About 150 feet agl, at an airspeed of about 85 knots, and a rate of descent of about 2,000 feet per minute, the flight instructor took over control of the helicopter and began to pull back on the cyclic while raising the collective. Despite the flight instructor’s efforts, the helicopter continued a tail-low descent into the ground, severing the tail boom. Postaccident examination revealed no preexisting mechanical malfunctions or anomalies that would have precluded normal operation.

Factual narrative

According to the helicopter flight instructor, he was preparing a helicopter-rated commercial pilot for his helicopter flight instructor check ride. After the pilot receiving instruction completed a straight-in autorotation, the flight instructor demonstrated a throttle-off, 180-degree autorotation from 600 feet above ground level (agl). The pilot receiving instruction then attempted the same maneuver, but during the entry, the helicopter airspeed became slow while the rotor rpm remained "in the green." The pilot receiving instruction lowered the nose of the helicopter, which increased airspeed. As the helicopter turned onto final approach at an altitude of about 300 feet agl, the flight instructor advised the pilot receiving instruction to ease back on the cyclic while raising the collective to maintain rotor rpm. About 150 feet agl, at an airspeed of about 85 knots, and a rate of descent of about 2,000 feet per minute, the flight instructor took over control of the helicopter and began to pull back on the cyclic while raising the collective. Despite the flight instructor’s efforts, the helicopter continued a tail-low descent into the ground, severing the tail boom. Postaccident examination revealed no preexisting mechanical malfunctions or anomalies that would have precluded normal operation.

Aircraft

Registration
N8066U
Reported as
Robinson Helicopter R22 Beta
Category
Helicopter
Serial number
1273
Airframe hours
4,584
Engine
Lycoming O-320 SERIES, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Bayphoto Helicopter LLC
Registered owner
Bayphoto Helicopter LLC
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · December 16, 2011
Departed
SPG · St Petersburg, FL
Destination
PIE · Clearwater, FL
Airport
SPG · Albert Whitted Field, runway 18, 2,864 × 150 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
27
Injuries
None
Certificates
Commercial, Flight instructor
Medical
Class 1, Without waivers/limitations
Last flight review
April 21, 2010
Seat
Right
Flight hours
1,528 total · 1,485 in this make and model · 1,249 as pilot in command · 193 in the last 90 days · 48 in the last 30 days · 2 in the last 24 hours
Role
Pilot
Age
36
Injuries
None
Certificate
Commercial
Medical
Class 2, With waivers/limitations
Last flight review
October 30, 2011
Seat
Left
Flight hours
276 total · 276 in this make and model · 134 as pilot in command · 35 in the last 90 days · 13 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
200° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
66 °F, dew point 55 °F
Altimeter
30.13 inHg
Observed at
SPG

Docket · 3

The files NTSB released with the investigation on August 29, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.2 MB in all.