N626LH

Substantial
None

SCHWEIZER 269CS/N: S1917

Accident Details

Date
Saturday, September 5, 2009
NTSB Number
CEN09LA575
Location
Preston, TX
Event ID
20090909X51625
Coordinates
33.882778, -96.628890
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
SCHWEIZER
Serial Number
S1917
Engine Type
Reciprocating
Year Built
2008
Model / ICAO
269CH269
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
269C

Registered Owner (Current)

Name
HELI-TECH INC
Address
3621 FRANKFORD AVE
City
PANAMA CITY
State / Zip Code
FL 32405-1907
Country
United States

Analysis

On September 5, 2009, about 1530 central daylight time, a Schweizer 269C helicopter, N626LH, was substantially damaged following a loss of engine power and subsequent forced landing into Lake Texoma near Preston, Texas. The pilot and the single occupant were not injured. The helicopter was registered to and operated by Longhorn Helicopters Inc., of Denton, Texas. Visual meteorological conditions prevailed and a company flight plan was filed for the 14 Code of Federal Regulations Part 91 local flight. The flight had originated from Cedar Mills Airport (3T0), Gordonville, Texas, at 1300.

According to the pilot, while conducting an aerial survey approximately 350-450 feet above the water, the engine experienced a loss of power. Due to crowded beach conditions, the pilot elected to perform the forced landing off shore. The pilot and passenger were able to exit unassisted and were picked up in a personal watercraft.

The helicopter was recovered from the lake and examined. Investigators removed the engine oil drain plug and drained water and oil from the engine crankcase. The engine's lower spark plugs and valve covers were removed. The engine was manually rotated via the main drive pulley and valve train continuity was established to each cylinder and to the accessory gears. In addition, thumb compression was developed in each cylinder. The magnetos were dried out and produced spark to all posts when tested via a magneto test bench.

The fuel servo and injector nozzles were removed, flow checked, and disassembled for inspection. No pre existing anomalies were found. Both fuel tanks were found to contain a quantity of a blue liquid consistent with 100 low lead aviation fuel. The electric standby fuel pump switch was found in the "ON" position. The pilot reported, that per company policy, when flying at low altitude the standby pump was to be activated at all times. The pilot further verified that the standby fuel pump was on for the entire accident flight.

The reason for the reported loss of engine power could not be determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09LA575