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May 25, 2002 · Kendall Blair Rans S-12 · N257BK

Lincolnton, GA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 25, 2002
Injury Outcomes
2 injuries (1 serious injury, 1 minor injury)
Location
Lincolnton, GA
Aircraft
Kendall Blair Rans S-12
Tail Number
N257BK
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
ATL02LA110

The pilot and passenger participated in an ultra-light fly-in at a private airstrip in Lincolnton. After takeoff, the airplane had a loss of engine power and could not maintain altitude. The pilot stated he "could not get any lift" during takeoff. During the forced landing, the airplane landed hard resulting in the collapse of the landing gear. Examination of the airplane showed one of the carbon fiber propeller blades delaminated on the trailing edge. The carbon fiber layers separated at a point several inches outboard from the propeller hub. The engine firewall was buckled, and the front area of the cockpit was deformed. Both wings and the tail boom were damaged.

NTSB Probable Cause

The loss of engine power due to the delamination of the propeller blade during takeoff, and the pilot's improper touchdown flare during the emergency landing resulted in a hard landing.

Full Narrative

On May 25, 2002, at 1500 eastern daylight time, a Blair Kendall, Rans S-12, N257BK, an experimental airplane, owned and operated by the pilot, collided with the ground after takeoff near Lincolnton, Georgia. The personal flight was operated under the provisions of Title 14 CFR part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane was substantially damaged, and the pilot and passenger were seriously injured. The flight departed Lincolnton, Georgia at 1458. The pilot and passenger participated in an ultra-light fly-in at a private airstrip in Lincolnton. After takeoff, the airplane had a loss of power and could not maintain altitude. The pilot stated he "could not get any lift" during takeoff. During the forced landing, the airplane landed hard resulting in the collapse of the landing gear. Examination of the airplane showed one of the carbon fiber propeller blades delaminated on the trailing edge. The carbon fiber layers separated at a point several inches outboard from the propeller hub. The engine firewall was buckled, and the front area of the cockpit was deformed. Both wings and the tail boom were damaged. During the post-accident examination of the propeller assembly, there were no visual cues of a previous propeller blade strike. According to the pilot, he and a friend were looking at the airplane after the accident and noticed that when pressure was applied to the propeller blade it would bend 4-5 inches from the hub area, and would spring back into place when pressure was removed. The pilot stated they could see the propeller blade "coming apart" near the middle. Examination of the FAA Aircraft Registry records, Oklahoma City, Oklahoma, indicated the experimental amateur built airplane was issued an airworthiness certificate on October 22, 1999. The pilot stated that he did not have any airplane or propeller maintenance records. There were only 66 total hours on the airplane and propeller since the airplane was built.

Flight

Event TypeAccident
Event Time15:00 EDT
Nearest AirportPrator Ranch Airport (0nm)
Runway320
Runway Length3200 ft
Runway Width140 ft
Flight Plan FiledVFR
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftKendall Blair Rans S-12
Tail NumberN257BK
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsBombardier · ROTAX · Reciprocating · 110
Seats2

People & Injuries

Injury Summary2 injuries (1 serious injury, 1 minor injury)
Fatal0
Serious1
Minor1
Uninjured0
Total2
Crew 1Age 49 · Third Class · Serious

Conditions

ConditionsVMC
LightDaylight
Wind230° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point54
Altimeter30.04 inHg
Observation Time18:53
Weather SourceWFAC

Appendix: Source Data