N9778N

Substantial
Minor

Dennis M. Durgin Junior AceS/N: DMD100

Accident Details

Date
Saturday, July 21, 2007
NTSB Number
MIA07LA124
Location
Dover-Foxcroft, ME
Event ID
20070803X01095
Coordinates
44.693054, -69.381225
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The failure of the pilot to maintain airspeed following total loss of engine power due to fuel starvation, resulting in a stall/mush, uncontrolled descent, and in-flight collision with trees.

Aircraft Information

Registration
N9778N
Make
DENNIS M. DURGIN
Serial Number
DMD100
Engine Type
Reciprocating
Year Built
1989
Model / ICAO
Junior AceBPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WILSON FREDERICK N
Address
221 PARK ST
Status
Deregistered
City
DOVER FOXCROFT
State / Zip Code
ME 04426-3700
Country
United States

Analysis

On July 21, 2007, about 1700 eastern daylight time, an amateur built Durgin Junior Ace, N9778N, registered to and operated by a private individual, crashed into a wooded area approximately .13 nautical mile east-southeast of the Charles A. Chase Jr. Memorial Field Airport (44B), Dover-Foxcroft, Maine. Visual meteorological conditions prevailed and no flight plan was filed for the 14 CFR Part 91 personal, local flight. The airplane was substantially damaged and the private-rated pilot, the sole occupant, sustained minor injuries. The flight originated about 1615, from 44B.

The pilot stated that the airplane had 6 gallons of auto fuel on-board when the flight departed. After takeoff, he flew over Dover-Foxcroft, then returned to 44B, where he performed 2 full-stop taxi back landings. The third takeoff was performed from runway 27, and after takeoff, the flight remained in the traffic pattern. He turned crosswind, then onto the downwind leg, where he reduced engine power to 1,700-1,800 rpm. He had an extended downwind leg, turned onto base then final, where the engine experienced a loss of power. The pilot further reported that the next thing he recalled was colliding with trees, and that 1 wing may have stalled. After coming to rest, he secured the airplane, exited it, and walked about 1/2 mile for assistance.

Examination of the accident site by an FAA inspector revealed a portion of the left wing remained suspended in a tree. Another tree located approximately 30 feet away was contacted; the airplane came to rest in a nose-low attitude located at 45 degrees 10.681 minutes North latitude and 069 degrees 14.149 minutes West longitude, or approximately 103.3 degrees magnetic and 790 feet from the approach end of runway 27. The wreckage was recovered for further examination.

Examination of the airframe and engine was performed by an FAA airworthiness inspector following recovery of the airplane. The examination of the airframe revealed no evidence of preimpact failure or malfunction of the flight controls. Examination of the engine revealed crankshaft, camshaft, and valve train continuity. The magnetos sparked normally during hand rotation of the engine, and the spark plugs looked normal. The fuel filters were clean and free of contamination. A minimal amount of fuel was noted in the airplane; the amount was not quantified.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA07LA124