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June 8, 2005 · Piper PA-18A-150 · N8680D

Griffin, GA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 8, 2005
Injury Outcomes
2 injuries (1 serious injury, 1 minor injury)
Location
Griffin, GA
Aircraft
Piper PA-18A-150
Tail Number
N8680D
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
ATL05CA096

During the preflight inspection of the airplane, the pilots believed that the left tank was full and the right tank showed one-half full as seen through the wing tank sight gauges. The cockpit fuel selector was positioned on the left fuel tank. After taxiing to the departure runway, the pilots completed an engine run-up and magneto check, and departed to the north. As the flight climbed to approximately 200 feet, the engine lost power and quit. When the pilot turned back to the runway, the right wing collided with a tree, and subsequently the ground. During the post-accident examination of the airplane, approximately two quarts of fuel were recovered from the left fuel tank and about 7 gallons of fuel were recovered from the right fuel tank. Examination of the cockpit found the fuel selector on the left fuel tank. During the functional check of the engine, the engine started and functioned without difficulty and idled for several minutes without any discrepancies noted.

NTSB Probable Cause

The pilot's mismanagement of the fuel supply which resulted in fuel starvation. A contributing factor was the pilot's inadequate preflight preparation which failed to verify the fuel amount.

Full Narrative

On June 8, 2005, at 1515 eastern daylight time, a Piper PA-18A-150, N8680D, registered to Starka Ventures Inc., and operated by the commercial pilot collided with trees shortly after takeoff from a Cider Ridge Airport, in Griffin, Georgia. The flight was operated under the provisions of Title 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed and no flight plan was filed for the local pleasure flight. The Pilot received serious injuries the pilot rated passenger received minor injuries and the airplane sustained substantial damage. The flight originated on June 8, 2005, from the Cedar Ridge Airport in Griffin, Georgia at 1510. According to the pilot, the pilot rated passenger completed the preflight inspection on the airplane. The pilot rated passenger stated that prior to departure the fuel drains were sumped and fuel levels checked. He believes that the left tank was full and the right tank showed one-half full as seen through the wing tank sight gauges. and the fuel selector was on the left tank. They said they taxied out, did a run up and mag check, then departed to the north. As they passed the departure end of the runway at approximately 200 feet AGL the engine quit. The pilot immediately started a left turn back towards the runway. After completing the 180-degree turn, it became apparent that he did not have enough altitude to make it back to the airport. The pilot said he saw a small opening in the trees and attempted to steer in that direction. The last thing he remembered was the plane hitting the trees. The passenger stated that the right wing impacted trees causing the airplane to yaw to the right then impacted the ground. The passenger stated he exited the airplane through the left window and observed fuel leaking from the left wing and the pilot was unconscious. He removed the pilot from the airplane through the left window and waited for assistance. Examination of the airplane found between two trees nose down rolled to the left with the right wing and empennage up. The cockpit window was shattered and the firewall and fuselage wrinkled. Approximately two quarts of fuel was drained into a 10 gallon plastic contained from the left fuel tank and about 7 gallons of fuel was drained from the right fuel tank. Examination of the cockpit found the fuel selector on the left fuel tank. The airplane was recovered and sent to Atlanta Air recovery for further examination. On June 14, 2005, the engine was examined at Atlanta Air Recovery in Griffin, Georgia. Examination of the engine found that the throttle and mixture control when moved worked properly. Further examination of the engine found that it had sustained minor damage to the exhaust pipes. The engine was mounted and a substitute fuel supply was attached. Due to bending noted on the crankshaft propeller flange it was decided to start the engine and run it only at idle for safety reasons. A dummy propeller was attached to the propeller flange and the engine started without difficulty and idled for several minutes without any discrepancies noted.

Flight

Event TypeAccident
Event Time15:15 EDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-18A-150
Tail NumberN8680D
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-C2A · Reciprocating · 180
Seats2

People & Injuries

Injury Summary2 injuries (1 serious injury, 1 minor injury)
Fatal0
Serious1
Minor1
Uninjured0
Total2
Crew 1Age 46 · Second Class · Serious

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility9 sm
CeilingBroken clouds 4300 ft
Temperature / Dew Point66 F
Altimeter29.94 inHg
Observation Time15:51
Weather SourceWFAC

Appendix: Source Data