Zenith Zodiac 601 HDS

Altoona, PA — October 17, 2024

Event Information

DateOctober 17, 2024
Event TypeACC
NTSB NumberERA25LA030
Event ID20241029195410
LocationAltoona, PA
CountryUSA
Coordinates40.29636, -78.32003
AirportALTOONA/BLAIR COUNTY
Highest InjuryNONE

Aircraft

MakeZenith Zodiac
Model601 HDS
CategoryAIR
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor0
None1
Total Injured0

Probable Cause

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.

Full Narrative

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.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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