N130WM

Substantial
Minor

MARLMAN STOL CH 801S/N: 84113

Accident Details

Date
Saturday, March 14, 2009
NTSB Number
CEN09LA214
Location
Fort Morgan, CO
Event ID
20090316X52540
Coordinates
40.333610, -103.802223
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The complete loss of engine power, as reported by the pilot, for undetermined reasons.

Aircraft Information

Registration
N130WM
Make
MARLMAN
Serial Number
84113
Year Built
2001
Model / ICAO
STOL CH 801

Registered Owner (Historical)

Name
FANNING DAN W
Address
5711 CAPISTRANO WAY
Status
Deregistered
City
FREDERICK
State / Zip Code
CO 80504-9716
Country
United States

Analysis

On March 14, 2009, about 1140 mountain daylight time, a single-engine Marlman STOL CH 801 airplane, N130WM, was substantially damaged during impact with the runway, following a complete loss of engine power shortly after takeoff from the Fort Morgan Municipal Airport (FMM), Fort Morgan, Colorado. The private pilot and passenger sustained minor injuries. The airplane was registered to and operated by the pilot. Visual meteorological conditions prevailed and no flight plan was filed for the 14 Code of Federal Regulations Part 91 personal flight. The 60-nautical mile cross-country flight was originating at the time of the accident and was destined for the Erie Municipal Airport (EIK), near Erie, Colorado.

According to the pilot, shortly after rotation and about 50-feet above the runway, the engine experienced a complete loss of power. The pilot pitched the airplane's nose over, but was unable to arrest the descent before impacting the runway. The airplane came to rest on the runway, in a nose down position, and both occupants were able to exit unassisted. Both wings and the fuselage sustained structural damage during the impact.

The airplane was recovered to Beegles Aircraft Services of Greeley, Colorado. An inspector from the Federal Aviation Administration (FAA) inspected the airplane and provided oversight for an engine run. To facilitate the engine run, the damaged propeller and engine oil filter was replaced with serviceable units.

According to the inspector, the engine was started and operated from idle through 2,500 rpm with no observed problems. An examination of the fuel tank, the fuel filter, and the fuel lines failed to reveal any anomalies or obstructions which would have restricted the fuel flow.

The reason for the 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# CEN09LA214