N254AW

Substantial
Minor

de Havilland DHC-3S/N: 254

Accident Details

Date
Friday, September 7, 2001
NTSB Number
ANC01LA138
Location
Cordova, AK
Event ID
20010919X01962
Coordinates
60.033332, -144.466659
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
8
Total Aboard
9

Probable Cause and Findings

The loss of engine power during cruise due to the fracture of an engine cylinder exhaust valve.

Aircraft Information

Registration
Make
DE HAVILLAND
Serial Number
254
Engine Type
Reciprocating
Year Built
1957
Model / ICAO
DHC-3DH2T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
16
FAA Model
DHC-3

Registered Owner (Current)

Name
DESTINATION ALASKA AIR SERVICE LLC
Address
PO BOX 778
City
HOMER
State / Zip Code
AK 99603-0778
Country
United States

Analysis

On September 7, 2001, about 1145 Alaska daylight time, a wheel-equipped de Havilland DHC-3 airplane, N254AW, sustained substantial damage during a forced landing about 53 miles east of Cordova, Alaska. The airplane was being operated as a visual flight rules (VFR) business flight under Title 14, CFR Part 91, when the accident occurred. The airplane was registered to Thomas J. Prijatel, and operated by Alaska Wilderness Outfitting Company, LLC, Cordova, Alaska. The certificated commercial pilot received minor injuries, and the eight passengers were not injured. Visual meteorological conditions prevailed, and VFR company flight following procedures were in effect. The flight originated about 1115, from the airplane owner's remote lodge, located about 100 miles southeast of Cordova , and was en route to Cordova.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge on September 8, the airplane/lodge owner reported that while in level, cruise flight, the accident pilot noted a loud bang as the engine began to run rough and lose power. He said that as the pilot was performing the engine emergency procedures, he smelled smoke in the cabin, and noted that the oil pressure was rapidly decreasing. During the subsequent forced landing in a marshy, muskeg-covered area, the airplane nosed over, and sustained substantial damage to right wing strut, engine firewall, and empennage.

In a letter dated November 5, 2001, a representative from Ray's Aviation, Santa Paula, California, reported that when the engine was disassembled, the exhaust valve within the number one cylinder was found fractured.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC01LA138