N511JG

Substantial
None

Zenith Zodiac 601 HDSS/N: 6-3331

Accident Details

Date
Thursday, October 17, 2024
NTSB Number
ERA25LA030
Location
Altoona, PA
Event ID
20241029195410
Coordinates
40.296361, -78.320028
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The total loss of engine power due to fuel starvation as a result of a deteriorated gascolator gasket. Contributing was the failure of the mechanic to replace the gasket during the most recent condition inspection.

Aircraft Information

Registration
Make
ZENITH ZODIAC
Serial Number
6-3331
Engine Type
Reciprocating
Year Built
2002
Model / ICAO
601 HDS
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
ZODIAC 601 HDS

Registered Owner (Current)

Name
GOSSELIN MARK J
Address
8793 RIVERVIEW HEIGHTS DR
City
HUNTINGDON
State / Zip Code
PA 16652-8072
Country
United States

Analysis

On October 17, 2024, at 1515 eastern daylight time, an experimental amateur-built Zenith Zodiac 601HDS airplane, N511JG, was substantially damaged when it was involved in an accident near Altoona, Pennsylvania. The private pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The private pilot reported that there were no irregularities noted with the airplane during the preflight inspection, engine run-up, or taxi before departing from runway 3 at Altoona/Blair County Airport (AOO), Altoona, Pennsylvania. The pilot intended to remain in the airport traffic pattern; however, during the initial climb, when the airplane was climbing through 300 ft above ground level, the engine started to “misfire,” then immediately stopped producing power. Unable to troubleshoot due to the low altitude, the pilot lowered the nose and attempted a forced landing on the remaining runway.

The airplane landed hard and the landing gear collapsed, which resulted in the wings and airframe buckling. The airplane then skidded to a stop on the side of the runway.

Examination of the airplane revealed signatures to the propeller that were consistent with a lack of rotation during the impact; the engine was intact. Engine crankshaft and valvetrain continuity was established and compression was attained on each cylinder. Both magnetos produced spark at each of the posts. A subsequent examination of the fuel system revealed 10 gallons of fuel on board. In addition, the fuel gascolator was installed partially outside of the engine compartment, exposing it to the air slipstream. The gascolator exhibited features consistent with a fuel leak. The gascolator bowl was not completely secure to the upper portion of the gascolator and it would leak fuel when lightly touched by hand. The gascolator was opened and the gasket at the top of the bowl was found to be stiff and cracked.

A review of maintenance records documented an annual condition inspection had been completed about 10 days before the accident. The logbook entry did not document any maintenance or inspection to the gascolator specifically, but the fuel system inspection was documented and tested, yielding no leaks.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA25LA030