N2077E

Substantial
None

SCHWEIZER 269CS/N: S1844

Accident Details

Date
Wednesday, June 15, 2011
NTSB Number
CEN11LA397
Location
Grand Forks, ND
Event ID
20110616X72608
Coordinates
47.961387, -97.400833
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The student pilot's inadequate recovery from an autorotation and the CFI's delayed remedial action.

Aircraft Information

Registration
N2077E
Make
SCHWEIZER
Serial Number
S1844
Engine Type
Reciprocating
Year Built
2003
Model / ICAO
269CH269
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
BUSHIDO LLC
Address
18054 SW CEREGHINO LN
Status
Deregistered
City
SHERWOOD
State / Zip Code
OR 97140-9494
Country
United States

Analysis

On June 15, 2011, at 1450 central daylight time, a Schweizer 269C, N2077E, operated by the University of North Dakota, sustained substantial damage to the tailboom while recovering from a practice autorotation in Grand Forks, North Dakota. The certified flight instructor and the student pilot were not injured. The 14 Code of Federal Regulations Part 91 instructional flight was operating in visual meteorological conditions without a flight plan. The local flight originated from the Grand Forks International Airport (GFK), Grand Forks, North Dakota, at 1430.

The flight instructor and student were performing a simulated forced landing which was to terminate with power when the accident occurred. The student lowered the collective to enter the autorotation and set the trim and pitch to maintain the recommended airspeed. The instructor adjusted the collective during the autorotation in order to prevent an overspeed and the student began the flare at an altitude of about 50 feet above the ground. The instructor stated the rotor revolutions per minute (rpm) were within the green arc and the engine was at 2,600 rpm.

The student used the collective to reduce the forward speed and rate of descent. The engine power was then increased to recover from the autorotation and the instructor noted the engine rpm needle moving up through 3,000 rpm. The instructor reported the helicopter was slightly tail low and it yawed slightly as the power was increased. The instructor took over the controls to level the skids and straighten the heading as the helicopter continued to sink. The helicopter continued to descend making a “light touch down” and run-on landing. The instructor reported that during the level-off and ground contact, they heard a metal on metal type sound.

Postaccident inspection of the helicopter revealed two of the main rotor blades had contacted the tailboom.

The helicopter was equipped with a Appareo RMS-2000 flight data recorder. The data downloaded from the recorder is included in the docket for this report.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11LA397