N78616

Substantial
Minor

Enstrom F-28FS/N: 513

Accident Details

Date
Saturday, August 7, 2004
NTSB Number
FTW04LA212
Location
De Leon, TX
Event ID
20040816X01224
Coordinates
32.215278, -98.177780
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
1
Total Aboard
3

Probable Cause and Findings

The pilot's failure to properly secure a fuel line, which resulted in a loss of engine power due to leakage and subsequent fuel starvation.

Aircraft Information

Registration
N78616
Make
ENSTROM
Serial Number
513
Engine Type
Reciprocating
Year Built
1981
Model / ICAO
F-28FEN28
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
ARROWHEAD HELICOPTERS INC
Address
C/O LEE CHRISTENSEN
490 SUNSET CV
Status
Deregistered
City
BLUFF DALE
State / Zip Code
TX 76433-4284
Country
United States

Analysis

On August 7, 2004, approximately 1400 central daylight time, an Enstrom F-28F single-engine helicopter, N78616, sustained substantial damage during a forced landing following a loss of engine power near De Leon, Texas. The commercial pilot was not injured and the two passengers sustained minor injuries. The helicopter was registered to and operated by Arrowhead Helicopters Incorporated, Kingman, Arizona. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight conducted under 14 Code of Federal Regulations Part 91. The flight departed a field near De Leon, Texas, about 1355.

In a written statement, the 9,375-hour pilot stated that he was giving attendees of a local festival 6-7 minute helicopter rides. He departed at 1356 with two passengers, 100 pounds of fuel, and climbed to an altitude of 500 feet above ground level (agl). Shortly after, the engine began firing through the exhaust and began to lose power. The pilot entered an autorotation and prepared to land in a school playground. While maneuvering toward the playground, the engine stopped producing power. During the landing, the helicopter slid forward, the skids collapsed and the main rotor severed the tail boom. The pilot instructed the passengers to exit the helicopter. He then secured the electrical switches, the magnetos, and turned off the fuel shut-off valve before he exited the helicopter.

The engine was examined on October 27, 2004, under the supervision of a Safety Board investigator. The examination revealed that when then fuel shut-off valve was turned on, fuel began to drain from the port where the main fuel line attached to the fuel manifold valve. The b-nut, which secured the line to the manifold, was partially attached to the port and was finger loose. The b-nut was then tightened, and the engine was test run on the airframe. It started immediately and ran at various power settings without interruption.

According to the pilot, he had removed and reassembled the fuel manifold valve approximately nine hours prior to the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW04LA212