Casualties unknown

Engine Failure During Final Approach Results in Hard Landing in Parking Lot (N5539W)

Hayward, CA, US

On July 26, 1999, a Piper PA-28-180 (registration N5539W) was involved in an aviation accident near Hayward, CA. Investigators recorded the probable cause as: the pilot's failure to apply carburetor heat to prevent the formation of carburetor ice while operating in IFR conditions which resulted in the loss of engine power. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

While turning left to final approach after descending through an overcast layer, the airplane's engine quit at 500 feet MSL half a mile from the runway. The pilot attempted restart procedures but was unable, leading to a landing in a parking lot.

Incident Description

During a left turn to final approach after descending through an overcast layer, the engine stopped approximately 0.5 miles from the runway at 500 feet MSL. The pilot initiated restart efforts: switching from the right to the left fuel tank, applying carburetor heat, richening the mixture, advancing the throttle, and checking the magneto switch position. He did not report turning on the auxiliary electric fuel pump. Unable to restart the engine, the pilot declared an engine-out emergency and performed an approach to a parking lot, resulting in a hard landing.

Fuel Status

An FAA inspector reported that the right fuel tank was filled nearly to the tab, while the left tank contained approximately 5 gallons. The pilot stated that he had been using the right tank for both legs of the flight and switched to the left tank as he turned final. Fueling records indicated the airplane had been topped off earlier that morning and had flown for 2 hours since then.

Carburetor Icing Conditions

The temperature was 59°F with a dew point of 54°F. According to a carburetor icing probability chart, these conditions were conducive for serious icing at either cruise or climb power. The pilot did not apply carburetor heat until after the power loss occurred.

Checklist Recommendations

The manufacturer recommends that the auxiliary electric fuel pump be on for all takeoffs and landings and when switching tanks. The second item on the 'Engine Power Loss In Flight' checklist is 'Electric Fuel Pump - On.'

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Frequently asked questions

What happened in the 26 Jul 1999 Piper PA-28-180 accident near Hayward, CA?

While turning left to final approach after descending through an overcast layer, the airplane's engine quit at 500 feet MSL half a mile from the runway. The pilot attempted restart procedures but was unable, leading to a landing in a parking lot.

What aircraft was involved and where did it happen?

The accident on 26 Jul 1999 involved a Piper PA-28-180, registration N5539W, at Hayward, CA.

What was the probable cause of the accident?

the pilot's failure to apply carburetor heat to prevent the formation of carburetor ice while operating in IFR conditions which resulted in the loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X19308. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.