FTW04LA001

NTSB accident investigation · Bratton Experimental Homebuilt Swearingen SX300 · Floresville, TX · October 2, 2003

Accident · Serious injuriesLimited investigationFinal report
Date
October 2, 2003, 11:09 local (16:09 UTC)
Place
Floresville, TX
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N301SXBratton Experimental Homebuilt Swearingen SX300
Weather
Visual (VMC) · Day
Status
Completed · report June 2, 2004
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20031002023289A
Case key
58077

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The separation of one propeller blade while in cruise flight. A factor contributing to the accident was the lack of suitable terrain for the forced landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionCruise - normal
Propeller system/accessories,hub - failureCause
Forced landingDescent - emergency
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - ground
Terrain condition - none suitableFactor

Analysis

The pilot of an experimental homebuilt single-engine airplane impacted the ground during a forced landing following a loss of engine power due to separation of a propeller blade. The shank connecting the composite propeller to the hub was broken, and one of the three blades was missing from the hub.

Factual narrative

On October 2, 2003, about 1109 central daylight time, a Bratton Swearingen SX300 experimental homebuilt single-engine airplane, N301SX, was substantially damaged when it impacted the ground during a forced landing to an open field following a loss of engine power near Floresville, Texas. The commercial pilot, who was the owner and operator of the airplane, and the passenger sustained serious injuries. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The airplane departed the Corpus Christi International Airport (CRP) near Corpus Christi, Texas. The flight's intended destination was the Gillespie County Airport (T82), near Fredericksburg, Texas.

The 4,000-hour pilot, who was the owner and builder of the airplane, reported to the Federal Aviation Administration (FAA) Inspector that the aircraft was powered by a 300-horsepower Lycoming IO-540 engine, which was driving a 3 bladed composite propeller.

According to information provided by the FAA inspector who responded to the accident site, one of the propeller blades came off while in cruise flight, and the pilot was able to shut the engine down.

Examination of the airplane by an FAA inspector revealed that the shank connecting the composite propeller to the hub was broken, and one of the three blades was missing from the hub.

The pilot/operator failed to provide the Safety Board with a completed Pilot/Operator Aircraft Accident Report (NTSB 6120.1/2) form.

Aircraft

Registration
N301SX
Reported as
Bratton Experimental Homebuilt Swearingen SX300
Category
Airplane, amateur-built
Serial number
5
Engine
Lycoming IO-540, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Marquis P. Bratton
Airworthiness certificate
Special, Experimental (Special)
Departed
CRP · Corpus Christi, TX
Destination
T82 · Fredericksburg, TX
Airport
8TAO · John B Connally Ranch Airport

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
79
Injuries
Serious
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
4,000 total

Weather

Conditions
Visual (VMC) · Day
Wind
90° at 7 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
72 °F, dew point 55 °F
Altimeter
30.19 inHg

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.