N997TB

Substantial
Minor

PIPER PA-32-260S/N: 32-508

Accident Details

Date
Saturday, December 31, 2011
NTSB Number
CEN12LA118
Location
Elk Rapids, MI
Event ID
20111231X42908
Coordinates
44.908889, -85.410003
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
4
Total Aboard
5

Probable Cause and Findings

The loss of engine power due to the failure of the exhaust valve.

Aircraft Information

Registration
N997TB
Make
PIPER
Serial Number
32-508
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
PA-32-260PA32
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BULLDOG AIR LLC
Address
3511 SILVERSIDE RD STE 105
Status
Deregistered
City
WILMINGTON
State / Zip Code
DE 19810-4902
Country
United States

Analysis

On December 31, 2011, about 1220 eastern standard time, a Piper PA-32-260, N997TB, sustained substantial damage during a forced landing to a field after a loss of engine power near Elk Rapids, Michigan. The commercial pilot and three passengers were not injured and one passenger received minor injuries. The airplane was registered to Bulldog Air LLC and operated by the pilot as a personal flight under the provisions of the 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The local flight departed from the Cherry Capital Airport (TVC), Traverse City, Michigan, at 1150.

The pilot reported that the airplane was in cruise flight when the engine started to run rough and vibrate. He adjusted and checked the fuel mixture, throttle, magnetos, boost pump, and carburetor heat, but the vibration continued to get worse. He decided to execute a forced landing to a farmer’s field and touched down with the airplane aligned with the furrows. He reported that the braking was ineffective due to the frozen field, and the airplane impacted a line of trees at the end of the field.

A Federal Aviation Administration airworthiness inspector examined the engine. He determined that the number one and number four cylinders had little to no compression when the propeller was rotated by hand. Both cylinders were removed. The number one cylinder exhaust valve was broken with approximately 50 per cent of the valve face missing. The piston and cylinder head were scarred with impact marks. The number four cylinder’s intact valve and seat were scarred, which was consistent with the compression loss. The upper and lower spark plug electrodes of the number four cylinder were forced closed, and there were impact marks on the piston and cylinder head.

Examination of the airplane’s engine logbooks revealed that the Lycoming O-540-E4B5 engine was overhauled in 1994 by an airframe and powerplant (A&P) mechanic. There was 1,972.3 hours logged on the engine since the last overhaul. There was no indication in the engine logbook that the number one and number four cylinders were repaired or replaced since the engine was overhauled. The most recent annual inspection was completed in April 2011.

The Lycoming Service Instruction No. 1009AT, “Recommended Time Between Overhaul Periods” recommended that the O-540-E4B5 engine be overhauled every 2,000 hours, or after 12 years of service since engine overhaul.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12LA118