N8572P

Substantial
None

PIPER PA-24-260 S/N: 24-4029

Accident Details

Date
Saturday, April 16, 1994
NTSB Number
MIA94LA123
Location
SPRING HILL, FL
Event ID
20001206X01161
Coordinates
28.369510, -82.510131
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

UNSUITABLE TERRAIN ENCOUNTERED DURING A FORCED LANDING. CONTRIBUTING TO THE ACCIDENT WAS THE FATIGUE FAILURE OF ONE OF THE PROPELLER BLADE'S PITCH CHANGE KNOB.

Aircraft Information

Registration
Make
PIPER
Serial Number
24-4029
Engine Type
Reciprocating
Year Built
1964
Model / ICAO
PA-24-260 PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-24-260

Registered Owner (Current)

Name
SERVICE DRUG DBA
Address
300 MAIN ST
City
CHADRON
State / Zip Code
NE 69337-2395
Country
United States

Analysis

On April 16, 1994, about 0815 eastern daylight time, a Piper PA-24-260, N8572P, registered to Roger L. Millheim, was substantially damaged during a forced landing near the Pilot Country Airport, Spring Hill, Florida, while on a 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The commercial-rated pilot, the sole occupant, was not injured. The flight originated from the Pilot Country Airport, Spring Hill, Florida, about 7 minutes earlier.

The pilot stated that during cruise flight he felt a severe vibration through the airframe which he attributed to be from the propeller. He attempted a forced landing on a road but during the descent, the airplane collided with the top of a 40-foot-tall dirt embankment. The airplane slid over the top down the other side coming to rest upright.

The propeller was removed for examination which revealed that a pitch change knob on one of the propeller blades was failed. The failed knob and butt end of the propeller blade was sent to the NTSB Metallurgy Laboratory in Washington, DC, for examination.

Metallurgical examination of the failed pitch change knob revealed that it failed due to fatigue.

Review of the aircraft logbooks revealed that the propeller was overhauled on June 28, 1989. At the time of the accident the propeller had accumulated about 397 hours since 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# MIA94LA123