N48395

Substantial
None

Grumman-Schweizer G-164AS/N: 1628

Accident Details

Date
Saturday, August 6, 2005
NTSB Number
NYC05LA129
Location
Penn Yan, NY
Event ID
20050811X01220
Coordinates
42.636943, -77.052780
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of engine power due to a fatigue fractured pushrod.

Aircraft Information

Registration
N48395
Make
GRUMMAN-SCHWEIZER
Serial Number
1628
Engine Type
Turbo-shaft
Year Built
1976
Model / ICAO
G-164AG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ARKPORT AIR SERVICE INC
Address
8790 OAK HILL RD
Status
Deregistered
City
ARKPORT
State / Zip Code
NY 14807
Country
United States

Analysis

On August 6, 2005, at 0912 eastern daylight time, a Grumman-Schweizer G-164A airplane, N48395, was substantially damaged during a forced landing after takeoff from the Penn Yan Airport (PEO), Penn Yan, New York. The certificated commercial pilot was not injured. Visual meteorological conditions prevailed for the local agricultural application flight conducted under 14 CFR Part 137.

According to the pilot, he had completed two local flights without any abnormalities, and then departed from runway 19, for the third flight of the day. After takeoff, as the pilot turned onto the crosswind leg of the traffic pattern and reduced the power, the engine "went silent." The pilot initiated a descent toward the runway to perform a forced landing. During the landing, the airplane rolled into rough, uneven terrain, resulting in substantial damage to the wings and fuselage.

Examination of the radial engine by a Federal Aviation Administration (FAA) inspector revealed the number 3 exhaust valve was fractured. The fractured valve was sent to the Safety Board Materials Laboratory, in Washington, D.C., for further examination. According to the Materials Laboratory Factual Report, examination of the fracture features on the fitting side of the valve revealed features consistent with fatigue.

A review of the airplane's maintenance records revealed the engine was last overhauled on March 16, 1998. The engine accumulated approximately 963 hours of operation since the overhaul. Additionally, an entry dated July 30, 2005, revealed a bird's nest was removed from the induction system. The next, and final, entry was dated August 5, 2005, and stated, "tightened throttle quadrant friction nut one turn. Ops check good."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC05LA129