N973BP

Substantial
None

PIETENPOL BIG PIETS/N: BP003

Accident Details

Date
Tuesday, July 16, 2019
NTSB Number
ERA19LA228
Location
Gainesboro, TN
Event ID
20190716X55113
Coordinates
36.395832, -85.641387
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Separation of the spinner cap for reasons that could not be determined based on available evidence, which resulted in contact and subsequent separation of the wooden propeller blade tip.

Aircraft Information

Registration
Make
PIETENPOL
Serial Number
BP003
Engine Type
Reciprocating
Year Built
2009
Model / ICAO
BIG PIETSBM3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
PIETENPOL BIG PIET

Registered Owner (Current)

Name
CLAPP WILLIAM M
Address
3913 ROWELL RD
City
VALDOSTA
State / Zip Code
GA 31606-0631
Country
United States

Analysis

On July 16, 2019, about 1300 central daylight time, an experimental, amateur-built Pietenpol Big Piet airplane, N973BP, was substantially damaged when it was involved in an accident at Jackson County Airport (1A7), Gainesboro, Tennessee. The pilot was not injured. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

According to the pilot, he was about 2 hours into the flight when the airplane experienced a vibration. He intended to land at the nearest airport and investigate the problem; however, as soon as he turned toward 1A7, a section of the propeller departed the airplane. The engine started to "tear itself loose," so he shut the engine off. The pilot then attained best glide speed for 1A7, but the headwind increased, and the airplane landed hard short of the runway, splitting the landing gear split and buckling the lower longerons. The airplane then slid into the airport perimeter fence.

Examination of the airplane by a Federal Aviation Administration (FAA) inspector revealed that the leading edge of the left wing was damaged, and the fuselage frame was bent severely enough to restrict movement of the fuel shutoff linkage. The aluminum propeller spinner was not located at the accident site.

The airplane was equipped with a Culver two-bladed wood propeller. The unpainted spinner cap was attached to the propeller through a bracket attached to the propeller bolt holes. A single screw held the spinner cap. The propeller was sent to the propeller manufacturer for further investigation. The investigation revealed a section of the propeller was missing at the tip with fibers bent backward and a crack radiating from the location of the missing piece toward the hub, consistent with contact from an unidentified object.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA19LA228