N5097P

Substantial
None

Piper PA-24-250S/N: 24-107

Accident Details

Date
Tuesday, October 3, 2006
NTSB Number
NYC07LA001
Location
Hammonton, NJ
Event ID
20061213X01782
Coordinates
39.671665, -74.754997
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Displacement of the idler gear assembly, which resulted in a loss of camshaft timing, and a subsequent engine failure. Contributing to the accident was the swampy terrain condition.

Aircraft Information

Registration
N5097P
Make
PIPER
Serial Number
24-107
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
PA-24-250PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
9935 WESTVILLE RD
Status
Deregistered
City
WYOMING
State / Zip Code
DE 19934
Country
United States

Analysis

On October 3, 2006, about 1230 eastern daylight time, a Piper PA-24-250, N5097P, was substantially damaged when it impacted terrain while approaching Hammonton Municipal Airport (N81), Hammonton, New Jersey. The certificated private pilot was not injured. Visual meteorological conditions prevailed. No flight plan was filed for the flight, from Cross Keys Airport (17N), Cross Keys, New Jersey, to Hammonton. The personal flight was conducted under 14 Code of Federal Regulations Part 91.

According to the pilot, the airplane was on a base leg to the airport when he turned on the auxiliary fuel pump, and the engine lost power. The pilot then performed a forced landing to a swampy area short of runway 21.

A subsequent examination of the Lycoming O-540-A engine revealed that within the accessory section, the idler gear assembly, which normally transferred power from the crankshaft to the left magneto and the camshaft, had been displaced. The mounting shaft had also been displaced, the shaft hole was elongated, and the upper portions of both shaft mounting plate retaining screws were missing. The lower screw appeared to be sheared, while the remains of the upper screw exhibited mechanical damage. The crankcase surface around the upper screw hole exhibited fretting, and the idler gear had missing and damaged gear teeth. Remnants of the retaining screws and screw lockplate were found in the bottom of the crankcase. The failure sequence could not be determined.

The pilot reported 1,393 hours of engine operation since overhaul. The engine logbook revealed that the engine was last overhauled on February 1, 1975.

Lycoming Service Instruction 1009AS, "Recommended Time Between Overhaul Periods," recommended 2,000 hours of operation between overhaul. In addition, "All engines that do not accumulate the hourly period of time between overhauls specified in this publication are recommended to be overhauled in the twelfth year." However, there was no evidence that the calendar time since the previous overhaul contributed to the displacement of the idler gear assembly.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC07LA001