Casualties unknown

Piper PA-28 Crashes After Steep Turn Following Wake Turbulence Caution (N3063T)

Palm Springs, CA, US

On October 6, 1989, a Piper PA-28RT-201T (registration N3063T) operated by Tuomela, Clyde was involved in an aviation accident near Palm Springs, CA. Investigators recorded the probable cause as: IMPROPER IN-FLIGHT PLANNING/DECISION BY THE PILOT, AND HIS FAILURE TO FOLLOW WAKE TURBULENCE AVOIDANCE PROCEDURES, WHICH RESULTED IN A VORTEX TURBULENCE ENCOUNTER. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

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

A Piper PA-28 collided with terrain after entering a steep bank and descending turn on final approach to runway 12. The aircraft was over maximum gross weight and had an aft CG. No preimpact mechanical issues were found.

Accident Details

The accident involved a Piper PA-28 and a Boeing 727 operated by Alaska Airlines as Flight 192, both on approach to land on runway 12 at an undisclosed airport. The runway was 8,500 feet long with a 1,200-foot displaced threshold. Winds were variable at 6 knots.

Sequence of Events

The Piper PA-28 pilot entered a left traffic pattern to land on runway 12. Around the same time, Alaska Flight 192 was also on approach to the same runway. The tower controller advised the PA-28 pilot of the other traffic and cautioned about wake turbulence. The PA-28 was abeam the approach end of the runway on a close downwind when the Boeing 727 landed.

The PA-28 pilot was cleared to land and subsequently entered an immediate steep bank and descending turn. Reportedly, the PA-28 was maneuvered onto final approach at an altitude of about 100 to 200 feet above ground level (AGL), then began oscillating excessively and crashed. No preimpact mechanical problem was evident.

Weight and Balance

A weight and balance computation showed the PA-28 was approximately 150 pounds over its maximum gross weight limitation, and its center of gravity (CG) was 3.86 inches behind the aft limit.

Frequently asked questions

What happened in the 6 Oct 1989 Piper PA-28RT-201T accident near Palm Springs, CA?

A Piper PA-28 collided with terrain after entering a steep bank and descending turn on final approach to runway 12. The aircraft was over maximum gross weight and had an aft CG. No preimpact mechanical issues were found.

What aircraft was involved and where did it happen?

The accident on 6 Oct 1989 involved a Piper PA-28RT-201T, registration N3063T, operated by Tuomela, Clyde, at Palm Springs, CA.

What was the probable cause of the accident?

IMPROPER IN-FLIGHT PLANNING/DECISION BY THE PILOT, AND HIS FAILURE TO FOLLOW WAKE TURBULENCE AVOIDANCE PROCEDURES, WHICH RESULTED IN A VORTEX TURBULENCE ENCOUNTER. A FACTOR RELATED TO THE ACCIDENT WAS: THE PILOT'S FAILURE TO ASSURE THE AIRCRAFT WAS LOADED WITHIN ITS WEIGHT AND BALANCE LIMITATIONS.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X29623. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.