N5699N

Substantial
None

ENSTROM HELICOPTER CORP 280CS/N: 1220

Accident Details

Date
Monday, May 25, 2009
NTSB Number
WPR09LA261
Location
Ogden, UT
Event ID
20090525X64809
Coordinates
41.196666, -112.013336
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's improper use of the helicopter's collective both during the takeoff sequence and while attempting remedial action in response to an engine over-boost condition, which resulted in a hard precautionary landing.

Aircraft Information

Registration
Make
ENSTROM HELICOPTER CORP
Serial Number
1220
Engine Type
Reciprocating
Year Built
1981
Model / ICAO
280CEN28
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
280C

Registered Owner (Current)

Name
STYER DAVID B
Address
4906 NW A AVE
City
PENDLETON
State / Zip Code
OR 97801-4632
Country
United States

Analysis

On May 25, 2009, about 1200 mountain daylight time, an Enstrom 280C helicopter, N5699N, impacted the terrain during an attempted precautionary landing just after taking off from Hinckley Airport, Ogden, Utah. The private pilot and his passenger were not injured, but the helicopter, which was owned and operated by the pilot, sustained substantial damage. The local 14 Code of Federal Regulations Part 91 personal pleasure flight was taking place in visual meteorological conditions. No flight plan had been filed.

According to the pilot of the reciprocating engine helicopter, just after he passed through translational lift he noticed that the engine was being over-boosted and that the main rotor blade RPM was drooping. He therefore lowered the collective in an attempt to lower the boost and to regain main rotor rpm, but the helicopter began to sink at a rate that made it necessary for the pilot to immediately transition to a landing. After touching down on the ground, the skids partially collapsed, the helicopter pitched forward, and the main rotor blades flexed downward far enough to sever the tail boom.

According to the pilot, the engine seemed to be running strong and smooth, and there did not appear to be any problems with the flight control system.

A Federal Aviation Administration Inspector inspected the helicopter and monitored a post-accident test run of the engine, and he reported that there were no anomalies with either the airframe or the engine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR09LA261