- Date
- June 8, 2005, 15:15 local (19:15 UTC)
- Place
- Griffin, GA
- Injuries
- 1 serious, 1 minor
- Damage
- Substantial damage
- Phase of flight
- Initial climb
- Aircraft
- N8680DPiper PA-18A-150
- Weather
- Visual (VMC) · Day
- Status
- Completed · report September 13, 2005
- Report
- Approved by Office Director
- Parties
- Atlanta FSDO
- FAA report
- 20050608012669A
- Case key
- 61650
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
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.
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.
Analysis
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.
Factual 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.
Aircraft
- Registration
- N8680D
- Reported as
- Piper PA-18A-150
- Category
- Airplane
- Serial number
- 18-6284
- Airframe hours
- 10,319
- Engine
- Lycoming O-360-C2A, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Standard, Utility
- Last inspection
- Annual · October 1, 2004
- Departed
- GA2 · Griffin, GA
- Destination
- GA2 · Griffin, GA
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
- 46
- Injuries
- Serious
- Certificates
- Commercial, Flight instructor
- Airplane ratings
- Single-engine sea, Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, With waivers/limitations
- Last flight review
- January 1, 2005
- Seat
- Front
- Flight hours
- 1,725 total · 1 in this make and model · 1,617 as pilot in command · 10 in the last 90 days · 2 in the last 30 days · 1 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 0° at 0 knots
- Visibility
- 9 statute miles
- Lowest ceiling
- 4,300 ft broken
- Temperature
- 84 °F, dew point 66 °F
- Altimeter
- 29.94 inHg
- Observed at
- ATL
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.
Other investigations on N8680D · 2
Matched to the same aircraft by N-number and date.