No fatalities

20 Mar 2008: PIPER PA32 260 (N3304W) — COOPER ELECTRICAL CONTROLS INC — New Albany, MS

New Albany, MS, United States

On 20 Mar 2008, a PIPER PA32 260 (registration N3304W) operated by COOPER ELECTRICAL CONTROLS INC was involved in an aviation accident near New Albany, MS. No fatalities were reported. Investigators recorded the probable cause as: A loss of engine power for undetermined reasons. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On March 20, 2008, a Piper PA-32-260 (N3304W) experienced a total loss of engine power during initial climb, resulting in a forced landing and post-crash fire. The pilot and passenger were not injured.

Accident Details

On March 20, 2008, at approximately 0750 central daylight time, a Piper PA-32-260, registration N3304W, was substantially damaged during a forced landing at the Union County Airport (M72) in New Albany, Mississippi. The airplane had experienced a loss of engine power during the initial climb after takeoff. The certificated private pilot and a passenger were not injured. Visual meteorological conditions prevailed, and no flight plan had been filed. The flight was destined for Roscoe Turner Airport (CRX) in Corinth, Mississippi, and was conducted under 14 Code of Federal Regulations Part 91 as a business flight.

Aircraft Information

The airplane was owned by the pilot and based at M72. According to the pilot, a preflight inspection and a normal engine run-up were performed prior to departure from Runway 36, a 3,900-foot-long asphalt runway. The airplane lifted off normally and climbed to an altitude of about 75 feet above the runway, when it began to "sputter" and then experienced a total loss of engine power. The airplane touched down hard on the remaining runway before going off the end, coming to a stop about 50 feet beyond the runway. Both occupants exited the airplane before a post-crash fire consumed a majority of the fuselage and the right wing.

Examination

A Federal Aviation Administration inspector examined the engine but did not identify evidence of any mechanical malfunctions. The pilot reported that the airplane had flown for 1.3 hours since it was refueled to its maximum capacity of 84 gallons, 9 days prior to the accident. Fuel recovered from the airplane’s left wing was absent of contamination. The airplane had been operated for about 40 hours since its most recent annual inspection, which was performed on August 9, 2007.

Contributing factors

Power plant