N7490F

Substantial
None

Hughes 269CS/N: 570596

Accident Details

Date
Sunday, March 24, 2002
NTSB Number
MIA02LA070
Location
Bessemer, AL
Event ID
20020326X00399
Coordinates
33.312778, -86.926109
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the flight instructor to adequately monitor the student's rotorcraft control, resulting in an abrupt cyclic input causing a tail rotor strike of the terrain while entering a hover, and the resulting rollover during an uncontrolled descent.

Aircraft Information

Registration
Make
HUGHES
Serial Number
570596
Engine Type
Reciprocating
Model / ICAO
269C
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
269C

Registered Owner (Current)

Name
DODSON INTERNATIONAL PARTS INC
Address
2155 VERMONT RD
City
RANTOUL
State / Zip Code
KS 66079-9014
Country
United States

Analysis

On March 24, 2002, about 1725 central standard time, a Hughes HU-269C, N7490F, registered to a private individual, operating as a Title 14 CFR Part 91 instructional flight, crashed on the Bessemer Airport, Bessemer, Alabama. Visual meteorological conditions prevailed and no flight plan was filed. The rotorcraft sustained substantial damage, and the flight instructor and student were not injured. The flight originated about 25 minutes before the accident.

According to the instructor, the student was practicing power off autorotations to a power on recovery, terminating in a 3-foot hover over a grassy area between runway 23 and the taxiway. On this particular autorotation, the student did not apply power to accomplish the recovery, and the CFI brought in the power to salvage the maneuver. The student applied abrupt back cyclic, and the tail rotor struck the ground, even though the CFI was riding the cyclic controls with the student. Following the tail rotor strike, the rotorcraft started spinning to the right, the right landing skid dug into the terrain, and the rotorcraft rolled over on its right side. There were no malfunctions of the rotorcraft or its components involved.

According to an FAA inspector, the student induced the tail rotor strike by over controlling the cyclic control in the aft direction. The responsibility for the maintenance of control rests with the CFI, who allowed the maneuver to progress to a point that possibly exceeded his ability to identify and safely recover.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA02LA070