N6846P

Unknown
None

PIPER PA-24-250 S/N: 24-1979

Accident Details

Date
Thursday, October 14, 1993
NTSB Number
CHI94IA017
Location
THIEF RVR FALLS, MN
Event ID
20001211X13527
Coordinates
48.110267, -96.170959
Aircraft Damage
Unknown
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

FATIGUE FAILURE OF THE PROPELLER BLADE, ORIGINATING FROM A CORROSION PIT.

Aircraft Information

Registration
N6846P
Make
PIPER
Serial Number
24-1979
Engine Type
Reciprocating
Model / ICAO
PA-24-250 PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
PELTIER JEFFREY J
Status
Deregistered
City
ARTHUR
State / Zip Code
ND 58006
Country
United States

Analysis

On October 13, 1993, at 1945 central daylight time, a Piper PA-24-250, N6846P, experienced a separation of approximately one foot of the outboard portion of one propeller blade while in cruise flight at 8,500 feet mean sea level. The private pilot made an uneventful forced landing near Thief River Falls, Minnesota. There was no damage to the airplane. The personal flight originated at Warroad, Minnesota, at 1900, with an intended destination of Arthur, North Dakota. No flight plan was filed, and visual meteorological conditions prevailed at the time.

The engine logbook indicated the propeller had been overhauled and reinstalled on April 1, 1986 at airframe total time of 2,942 hours. There were four annual inspection logbook entries stating the propeller had been "dressed and painted." The last inspection was an annual inspection completed on December 1, 1992. The airplane had flown 88 hours since inspection. The total time accumulated since the propeller had been overhauled was 1,000 hours.

The remaining portion of the failed propeller blade was sent to the National Transportation Safety Board Materials Laboratory, Washington D.C., for examination. The metallurgical report stated the fracture was typical of a fatigue separation. The fatigue origin was a corrosion pit on the camber surface of the blade measuring 0.012 inches wide and 0.0014 inches deep.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI94IA017