N209LH

Substantial
Serious

Schweizer 269CS/N: S1881

Accident Details

Date
Tuesday, April 18, 2006
NTSB Number
DFW06LA108
Location
Denton, TX
Event ID
20060420X00467
Coordinates
33.200553, -97.197776
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The flight instructor's failure to maintain rotor RPM, resulting in a hard landing.

Aircraft Information

Registration
N209LH
Make
SCHWEIZER
Serial Number
S1881
Engine Type
Reciprocating
Model / ICAO
269CH269
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
PACIFIC AEROMOTIVE CORPORATION
Address
PO BOX 450
Status
Deregistered
City
ERIE
State / Zip Code
CO 80516-0450
Country
United States

Analysis

On April 18, 2006, approximately 1030 central daylight time, a Schweizer 269C single-engine helicopter, N209LH, was substantially damaged during a hard landing following a simulated loss of engine power about three miles west of the Denton Municipal Airport (DTO), near Denton, Texas. The flight instructor and pilot receiving instruction sustained serious injuries. The helicopter was registered to and operated by Longhorn Helicopters, Inc., of Trophy Club, Texas. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 instructional flight. The local flight originated from DTO about 1000.

The 4,000-hour helicopter flight instructor reported that he was demonstrating a simulated forced landing to an open field. The flight instructor initiated an autorotation and, after descending in autorotation to about 200 feet above ground level (agl), he applied engine power to initiate an engine recovery; however, the rotor RPM had decayed “below limits.” Subsequently the helicopter developed a high sink rate. Despite the flight instructor's attempt to regain rotor RPM, the helicopter landed hard on its skid landing gear before rolling over on its side.

According to a Federal Aviation Administration (FAA) inspector who responded to the accident site, the helicopter's main rotor, tail boom, and fuselage sustained structural damage. The inspector further reported that an examination of the helicopter's flight controls and engine revealed no preimpact anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW06LA108