ERA11CA162

NTSB accident investigation · Bell 206 · Ridgeland, SC · February 24, 2011

Accident · No injuriesData collectionFinal report
Date
February 24, 2011, 15:45 local (20:45 UTC)
Place
Ridgeland, SC
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N796MBell 206
Defining event
Landing-flare/touchdown: Hard landing
Weather
Visual (VMC) · Day
Status
Completed · report June 8, 2011
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20110224001899A
Case key
78424

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 certified flight instructor's delayed remedial action during a practice autorotation, which resulted in a hard landing.

Findings · 1

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 pilotAll 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 certified flight instructor (CFI), the student pilot was conducting a practice autorotation with a planned power recovery. The helicopter’s rotor rpm was maintained throughout the maneuver and the student pilot initiated the flare during the recovery stage. The student failed to increase the throttle and the CFI did not react in time to add engine power in order to recover. The CFI subsequently took authority of the flight controls and the helicopter landed hard. The main rotor contacted the tail boom, resulting in substantial damage to the tail boom, tail rotor drive shaft, and tail rotor control rod. The CFI stated that there were no preimpact mechanical malfunctions or anomalies with the helicopter.

Factual narrative

According to the certificated flight instructor (CFI), the student pilot was conducting a practice straight-in autorotation with a planned power recovery from an altitude of 1,000 feet. The CFI stated that the helicopter’s rotor rpm was maintained throughout the maneuver. The student pilot initiated the flare during the recovery stage of the maneuver, but did not apply throttle, and the CFI did not react in time to add power in order to recover. The CFI subsequently took the controls and the helicopter landed hard. The main rotor contacted the tail boom, resulting in substantial damage to the tail boom, tail rotor drive shaft, and tail rotor control rod. The CFI stated that there were no mechanical malfunctions or anomalies with the helicopter.

Aircraft

Registration
N796M
Reported as
Bell 206 (B)
Category
Helicopter
Serial number
3396
Engine
Rolls Royce C20B, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Lady Alice Corp
Registered owner
Lady Alice Corp
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 23, 2010 · 51 hours before
Departed
SAV · Savannah, GA
Destination
3J1 · Ridgeland, SC
Airport
3J1 · Ridgeland Airport, runway 21, 2,692 × 70 ft, asphalt

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
39
Injuries
None
Certificates
Flight instructor, Private, Airline transport
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Without waivers/limitations
Last flight review
November 27, 2010
Seat
Left
Flight hours
1,300 total · 421 in this make and model · 1,206 as pilot in command · 35 in the last 90 days · 20 in the last 30 days
Role
Student pilot
Age
53
Injuries
None
Certificate
Student
Medical
Class 3, Without waivers/limitations
Seat
Right
Flight hours
78 total · 78 in this make and model · 11 as pilot in command · 18 in the last 90 days · 16 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
110° at 9 knots
Visibility
10 statute miles
Lowest ceiling
3,500 ft broken
Temperature
66 °F, dew point 57 °F
Altimeter
30.09 inHg
Observed at
NBC, 14 nm away

Docket · 2

The files NTSB released with the investigation on May 2, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.1 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.