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N513AU accident description

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Crash location Unknown
Nearest city Aliquippa, PA
40.636733°N, 80.240061°W
Tail number N513AU
Accident date 08 Sep 1994
Aircraft type Boeing B-737-300
Additional details: None

NTSB Factual Report

On September 8, 1994, USAir flight 427, a Boeing 737-300, N513AU, crashed near Aliquippa, PA at about 1903 eastern daylight time. The airplane was destroyed by impact and post crash fire. The 2 pilots, 3 flight attendants and 127 passengers were fatally injured. The flight was being conducted under 14 CFR Part 121. Visual meteorological conditions prevailed at the time of the accident and an IFR flight plan was filed.

The flight crew was in contact with the local controller and was being maneuvered to enter a right downwind pattern for runway 28R at Pittsburgh International Airport, Pittsburgh, PA. The flight crew did not report any problems with the airplane and radar data indicates that the closest other traffic was about 4.5 miles and 1,500 feet vertically separated from flight 427 at the time of the accident.

The airplane struck the ground at an angle of descent of about 80 degrees, in a slight roll to the left, and the airspeed was about 260 knots at impact. The airplane was severely fragmented by the impact. There was an intense postcrash fire. Both engines were producing power at impact and were running symmetrically. The thrust reversers were stowed at impact.

The flaps were at a "Flap 1" setting. At this setting, the leading edge slats and Kreuger flaps are extended. The spoilers were retracted and the landing gear were retracted. These are the expected positions forthe airplane during the initial approach. The horizontal stabilizer was in an intermediate position, consistent with a speed of about 190 knots. The elevator power control unit was at 14 degrees nose up. The rudder was determined to be 2 degrees to the right (airplane nose right) at impact.

Additional Persons (continued)

Mr. Paul Mingler CFM International Flight Safety Office One Neumann Way MD J60 Cincinnati, OH 45215-6301

Mr. Paul M. Rehder AVIALL Technical Services Dallas Engine Services 9311 Reeves Street Dallas, Texas 75235-2095

Mr. William West National Air Traffic Controllers Association Suite 701 1150 17th Street, N.W. Washington, D.C. 20036

Mr. Juergen-Peter Schuetz Transportation Workers Union #545 Operations Coordination/Dispatch 2018 Broad Hill Farms Road Coraopolis, PA 15108

Mr. Terry Kleiser International Association of Machinists and Aerospace Workers 73 Auburn Street Saugus, MA 01906

Ms. Nancy Gilmer Association of Flight Attendants 2244 Commissary Circle Odenton, MD 21113

Mr. Wally Walz Parker Berta Aerospace Parker Hannifin Corporation 14300 Alton Parkway Irvine, CA 92718-1814

Mr. Frank P. Jakse Senior Research Specialist Monsanto 800 N. Lindbergh Boulevard St. Louis, MO 63167

Mr. Harvey Patrick PATS, Inc. 9570 Berger Road Columbia, MD 21046-1569

Mr. Jim Eichenlaub Manager Hopewell Township Municipal Building Clark Boulevard Aliquippa, PA 15001

LT James R. Nevill Station Commander Pennsylvania State Police 1400 Brighton Road Beaver, PA 15009

Mr. Joseph L. LaFleur Director Pennsylvania Emergency Management Agency Box 3321 Harrisburg, PA 17105-3321

Mr. Wayne N. Tatalovich Coroner Beaver County Courthouse Third Street Beaver, PA 15009

NTSB Probable Cause

A loss of control of the airplane resulting from the movement of the rudder surface to its blowdown limit. The rudder surface most likely deflected in a direction opposite to that commanded by the pilots as a result of a jam of the main rudder power control unit servo valve secondary slide to the servo valve housing offset from its neutral position and overtravel of the primary slide.

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