NC18252

Substantial
Minor

Rose Parakeet A-1S/N: 107

Accident Details

Date
Friday, June 10, 2005
NTSB Number
DFW05CA158
Location
Boyd, TX
Event ID
20050809X01184
Coordinates
33.166667, -97.633331
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The in-flight separation of the outboard section of the propeller for unknown reasons. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
Make
ROSE
Serial Number
107
Engine Type
Reciprocating
Year Built
1938
Model / ICAO
Parakeet A-1A270
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
PARRAKEET A-1

Registered Owner (Current)

Name
RAILING TERRY L
Address
N5206 HWY G
City
LAKE MILLS
State / Zip Code
WI 53551
Country
United States

Analysis

On June 10, 2005, approximately 1605 central daylight time, a single-engine Rose Parakeet A-1 antique bi-plane, NC18252, was substantially damaged during a forced landing following the de-lamination of the wood propeller near Boyd, Texas. The commercial pilot, sole occupant of the airplane, received minor injures. The airplane was registered to and operated by the pilot. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The cross-country flight originated from the Brownwood Regional Airport (BWD) near Brownwood, Texas, and was destined for the Gainesville Municipal Airport (GLE) near Gainesville, Texas.

The 2,106-hour pilot reported that while in cruise flight at 3,500 feet, with a power setting of approximately 2,150 rpm, the engine developed a severe vibration. The pilot stated that he immediately reduced the power and "cut the magneto switch." He then noticed that the outboard portion of a propeller blade had "splintered" and was missing.

The pilot selected a field to execute a forced landing. During the landing rollout, the airplane went through a barbed wire fence and collided with a metal fence-post. The airplane came to rest in the upright position on its nose.

A Federal Aviation Administration (FAA) inspector, who examined the airplane at the accident site, noted that the airplane's right wing spar sustained structural damage, the fuselage's lower longeron and left wing tip were bent. The wooden propeller's metal leading edge and tip was missing and the propeller showed signs of de-lamination. The pilot also reported that the airplane's cowling, carburetor, and right gear tripod were damaged.

The airplane's wooden propeller was removed and sent to the manufacturer for further examination. The propeller manufacturer could not determine the reason for the failure, and noted no abnormalities existed in the propeller.

At 1545, the automated weather observing system at the Decatur Municipal Airport (LUD), near Decatur, Texas, approximately 10 miles north of the accident site, reported wind from 160 degrees at 15 knots, gusting to 22 knots, 10 miles visibility, sky clear, temperature 88 degrees Fahrenheit, dew point 63 degrees Fahrenheit, and an altimeter setting of 29.74 inches of Mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW05CA158