No fatalities

Engine Failure During Demonstration Flight Results in Forced Landing (N9003Y)

Miami-Opa Locka, United States of AmericaLanding (descent or approach)

On January 26, 1983, a Piper PA-31-310 Navajo (registration N9003Y) operated by Burt Weech was involved in an aviation accident near Miami-Opa Locka, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Occurrence #1: loss of engine power (partial) - mechanical failure/malfunction. Findings: inadequate maintenance, incorrect magneto timing, improper adjustment, distributor arcing, partially blocked fuel filter, fuel starvation, turbocharger binding, partial… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary report: the U.S. National Transportation Safety Board (NTSB) historical archiveUpdated 2026-07-04Data APIEditorial standards

During a local demonstration flight, the left engine experienced rough running and power loss, followed by the right engine overheating. A wheels-up forced landing was made; both occupants were uninjured.

Accident Details

The pilot and a prospective buyer/passenger were on a local demonstration flight. Prior to this flight, the aircraft had been parked for nearly one year and had flown only 66 hours since its last annual inspection. During the preflight inspection, the pilot found the fuel tanks between 1/4 full and empty. The sumps were drained, the main tanks were filled, then the sumps were drained again.

After takeoff, the pilot leveled the aircraft at 1,500 feet in a cruise configuration. Shortly thereafter, the left engine began running rough, backfiring, and losing power. The pilot turned back toward the airport, but the engine lost all power and the propeller was feathered. While returning, the right engine's cylinder head and oil temperature began rising above the red line. Subsequently, it began losing power, and a wheels-up, forced landing was made in an open field.

Examination

An examination revealed that both engines were out of time, firing was intermittent, and the distributor block on the left engine was burned due to incorrect timing. Additionally, the left turbocharger gate was stuck open, and the left fuel filter was partially clogged.

Probable Cause

The probable cause was determined as occurrence #1: loss of engine power (partial) due to mechanical failure/malfunction. Findings included: inadequate maintenance by other maintenance personnel; incorrect magneto ignition timing; improper adjustment; distributor arcing; partially blocked fuel filter; fuel starvation; binding of the turbocharger; and partial failure of two or more engines.

Frequently asked questions

What happened in the 26 Jan 1983 Piper PA-31-310 Navajo accident near Miami-Opa Locka, United States of America?

During a local demonstration flight, the left engine experienced rough running and power loss, followed by the right engine overheating. A wheels-up forced landing was made; both occupants were uninjured.

Were there any fatalities in the 26 Jan 1983 Piper PA-31-310 Navajo accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 26 Jan 1983 involved a Piper PA-31-310 Navajo, registration N9003Y, operated by Burt Weech, at Miami-Opa Locka, United States of America.

What was the probable cause of the accident?

Occurrence #1: loss of engine power (partial) - mechanical failure/malfunction. Findings: inadequate maintenance, incorrect magneto timing, improper adjustment, distributor arcing, partially blocked fuel filter, fuel starvation, turbocharger binding, partial failure of two or more engines.