2 fatalities

2002-03-17: Piper PA-31-310 Navajo (N125TT) — Floopie Flight Corporation — Anderson-Darlington Field, United States of America

Anderson-Darlington Field, United States of AmericaLanding (descent or approach)

On March 17, 2002, a Piper PA-31-310 Navajo (registration N125TT) operated by Floopie Flight Corporation was involved in an aviation accident near Anderson-Darlington Field, United States of America during landing or approach. 2 people were killed. Investigators recorded the probable cause as: The pilots failure to maintain control of the airplane during the instrument approach. The low overcast ceiling and the pilot's in-flight decision to execute the instrument approach in below minimum weather conditions were factors. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781201975Data APIEditorial standards

An airplane was destroyed by impact forces and fire after crashing about 3.7 miles from the destination airport while executing an ILS approach. Weather conditions included a 100-foot overcast ceiling and 1 statute mile visibility. No pre-existing anomalies were found in the airframe, engine, or gyroscopic instruments.

Accident Overview

An airplane was destroyed when it struck the ground approximately 3.7 miles from the destination airport, resulting in impact forces and a post-crash fire. The aircraft had been cleared for an Instrument Landing System (ILS) approach to the airport.

On-Scene Examination

Investigators conducted an on-scene examination of the airframe, engine, and gyroscopic flight instruments. No anomalies that could be associated with a pre-existing condition were found.

Approach Details

The minimum descent altitude for the ILS approach is 243 feet above ground level. The inbound course for the instrument approach is 298 degrees magnetic. Radar data indicated that the airplane was heading in a northerly direction before commencing a left turn onto the inbound course. The last radar return was received before the airplane reached the locator outer marker for the approach. Altitude returns showed the airplane descending from a pressure altitude of 4,000 feet to a pressure altitude of 2,800 feet, which was the final return recorded.

Wreckage Distribution

The wreckage path was distributed on a magnetic heading of approximately 145 degrees.

Weather Information

Approximately 20 minutes before the accident, the weather reporting station at the destination airport recorded a 100-foot overcast ceiling with 1 statute mile of visibility. This current weather was available to the pilot via the Automated Weather Observing System (AWOS) at the destination airport.

Communications

No communications were received from the airplane after controllers authorized the pilot to switch to the destination airport's advisory frequency.

Probable cause

The pilots failure to maintain control of the airplane during the instrument approach. The low overcast ceiling and the pilot's in-flight decision to execute the instrument approach in below minimum weather conditions were factors.