N225BL

Substantial
None

NOORDUYN UC-64AS/N: 542

Accident Details

Date
Saturday, July 11, 2009
NTSB Number
ANC09LA065
Location
Akiachak, AK
Event ID
20090715X44125
Coordinates
60.905834, -161.426391
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The loss of engine power due to the failure of a crankshaft component, resulting in an off-airport landing.

Aircraft Information

Registration
N225BL
Make
NOORDUYN
Serial Number
542
Engine Type
Reciprocating
Year Built
1943
Model / ICAO
UC-64ANORS
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RENFRO MICHAEL W
Address
410 TOWER RD
Status
Deregistered
City
BETHEL
State / Zip Code
AK 99559-0872
Country
United States

Analysis

On July 11, 2009, about 1300 Alaska daylight time, a Noordyun UC-64A (Norseman) airplane, N225BL, sustained substantial damage following a loss of engine power and an emergency landing about 300 feet short of runway 1 at the Akiachak Airport, Akiachak, Alaska. The airplane was being operated as a visual flight rules (VFR) passenger flight under Title 14, CFR Part 135, by Renfro's Alaska Adventures, Bethel, Alaska. The pilot and sole passenger were not injured. Visual meteorological conditions prevailed, and company flight following procedures were in effect.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on July 12, the pilot said he was flying from Bethel to Tuluksak, Alaska, when the engine started to run rough. He said he diverted to Akiachak which was near their position. The pilot said the engine quit completely, and he was unable to reach the runway. The airplane collided with terrain about 300 feet short of runway 1. The pilot said the engine had been rebuilt about 100 flight hours prior to the accident, after developing problems following a previous rebuild. He said that the airplane sustained substantial damage to both wings and the fuselage during the accident.

An internal examination of the engine by the NTSB IIC on November 6, showed that a locking screw had backed out of one of the two anti-vibration counterweights on the crankshaft, and scored the interior back surface of the engine case. The locking screw was not located. The engine case and oil passages had fractured metal pieces from piston skirts, piston rings, and ground pieces of connecting rods. A large part of the crankshaft counterweight and half of bolt that normally secures the counterweight halves were found in a piston cylinder. The other half of the counterweight was found in the crankcase; it was fractured into three large and many smaller pieces. The second counterweight was still bolted in its proper place. Piston heads were found in the crankcase, and the engine's master rod was bent.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC09LA065