Piper PA-31-T2 accident near Jackson, TN

On June 3, 2001, a Piper PA-31-T2 (airplane) was involved in an accident near Jackson, TN. 5 people died. Damage to the aircraft: destroyed.

Date
June 3, 2001
Place
Jackson, TN
Aircraft
Piper PA-31-T2 · Airplane
Injuries
5 fatal, 0 serious, 0 minor
Damage
Destroyed
Position
35.496°N, 88.904°W
NTSB ID
20010608X01129

NTSB summary

HISTORY OF FLIGHT On June 3, 2001, about 1611 central daylight time, a Piper PA-31-T2, N31XL, registered to Falcon Communications, Inc., crashed near Jackson, Tennessee, while on a 14 CFR Part 91 corporate flight. Visual meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed. The airplane was destroyed and the commercial-rated pilot and four passengers were fatally injured. The flight originated from Malden, Missouri, the same day, about 1525. Transcript of communications, from the FAA Memphis Air Route Traffic Control Center, show that at 1526:49, the pilot of N31XL reported to the controller that they were off Malden, Missouri, and requesting a instrument flight rules clearance to Fulton County Airport, Atlanta, Georgia. The pilot was given the clearance and told to climb and maintain 23,000 feet. At 1550:52, the pilot reported the flight was level at 23,000 feet. At 1552:15, the pilot of N31XL reported that he had a problem with an engine and needed to shut it down and find somewhere to land. The controller reported to the pilot that the flight was over the McKellar-Sipes Regional Airport, Jackson, Tennessee, and that the flight could descend to 7,000 feet. At 1553:42, the pilot was told that the airport was seven miles behind him. The pilot responded that he was trying to get down and would keep circling. The controller cleared the flight to circle as necessary and to descend to 2,500 feet. At 1601:47, the pilot reported that the flight was descending through 8,000 feet and request that the flight be set up for the instrumen

Probable cause

The pilot's shutting down the left engine following loss of control of the left propeller resulting in an in-flight loss of control of the airplane due to the windmilling propeller. Factors in the accident were the failure of the propeller control bracket assembly due to fatigue, the pilot's lack of experience in the type of airplane (turbo propeller) and the absence of a procedure for loss of pro

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