MIA07LA155

NTSB accident investigation · Grumman AA-5A · Worthington, KY · September 22, 2007

Accident · FatalLimited investigationFinal report
Date
September 22, 2007, 14:55 local (18:55 UTC)
Place
Worthington, KY
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N26442Grumman AA-5A
Weather
Visual (VMC) · Day
Status
Completed · report December 28, 2008
Report
Approved by Office Director
Parties
FSDO/FAA
FAA report
20070922020989A
Case key
66739

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 the engine's No. 4 piston from the crankshaft for unidentified reasons and the pilot's continued operation with known equipment deficiencies.

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.

Loss of engine power(total) - mech failure/malfTakeoff - initial climb
Lubricating system - leak
Operation with known deficiencies in equipment - continuedPilot in commandCause
Powerplant - overtemperature
Powerplant - seized
DitchingEmergency descent/landing

Analysis

The pilot replaced the accident airplane’s vacuum pump on the day of the accident. During the airplane's flight to a nearby airport, the engine lost the majority of its oil. At the destination airport, the engine was examined for the leak. According to witness staements, the vacuum pump had been installed incorrectly. The discrepancy was corrected and the pilot added 4 quarts of oil to the engine and attempted to return to his home airport; however, the engine overheated during the initial phase of the flight and the pilot returned to the departing airport. He purchased more engine oil, servicing the engine to the full level. Although several people suggested that the pilot have the engine further examined, he declined saying that he had "Get-Home-Itis." Once again the pilot took off for his home airport, but the engine lost all power during the initial climb. The pilot ditched the airplane in a nearby river in a flat attitude, where it submerged. Examination of the wreckage revealed that the No. 4 engine piston had separated from the crankshaft. The pilot did not hold an airframe and powerplant certificate.

Factual narrative

On September 22, 2007, about 1455 eastern daylight time, a Grumman AA-5A, N26442, registered to and operated by an individual, as a 14 Code of Federal Regulations (CFR) Part 91 personal flight, ditched in the Ohio River near Worthington, Kentucky. Visual meteorological conditions prevailed and no flight plan was filed. The pilot was killed and the airplane incurred substantial damage. The flight departed from the Ashland Regional Airport (DWU), Ashland, Kentucky, about 1453.

Witnesses stated that the pilot arrived at DWU and noticed an engine oil leak, which almost left the engine without oil. After an inspection of the engine, it was discovered that the vacuum pump, which the pilot had installed earlier that day, was installed incorrectly causing the oil leak. He corrected the discrepancy with the pump and added 4 quarts of oil to the engine; 3 quarts less for the required full level. He then took off to fly back to Grayson County Airport (M20), Leitchfield, Kentucky; however, the airplane returned to DWU shortly after departure and parked on the ramp. At that time, the pilot stated to the witnesses that the engine got hot again. The pilot declined to have the engine inspected and stated he had "Get-Home-Itis." He purchased 4 additional quarts of engine oil, which he added to the airplane’s engine. The pilot again departed for M20.

On departure, the engine lost total power. The pilot announced the emergency over the common traffic advisory frequency. A witness, fishing in the river north of the airport, saw the airplane ditch in the river in a flat attitude. The airplane floated for a moment, then nosed over and went completely underwater. The pilot was unable to exit the airplane after it was submerged.

Examination of the wreckage by a Federal Aviation Administration inspector revealed that the No. 4 engine piston had separated from the crankshaft.

The pilot, age 80, held a commercial pilot certificate with ratings for airplane single-engine land, airplane multiengine land, and instrument airplane. He was issued a third-class medical certificate on March 23, 2006, with limitations; must wear corrective lenses for near and distant vision. He had documented 3,560 total hours at that time. He held a repairman experimental aircraft builder certificate with limitations of inspection certificate for experimental aircraft make William G Stevens model Lancair 360, serial number 1109P.

The pilot’s flight logbook and the accident airplane’s maintenance records were not located.

Aircraft

Registration
N26442
Reported as
Grumman AA-5A
Category
Airplane
Serial number
AA5A-0592
Airframe hours
1,522
Engine
Lycoming 0-320, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
William G. Steven
Registered owner
William G. Steven
Airworthiness certificate
Standard, Utility
Departed
DWU · Worthington, KY
Destination
M20 · Leitchfield, KY
Airport
DWU · Ashland Regional

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
80
Injuries
Fatal
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Without waivers/limitations
Seat
Left
Toxicology
Performed
Flight hours
3,560 total

Weather

Conditions
Visual (VMC) · Day
Wind
200° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 63 °F
Altimeter
30.04 inHg
Observed at
HTS, 14 nm away

FAA reports on this event · 1

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