132 fatalities

1994-09-08: Boeing 737-300 (N513AU) — USAir - US Airways — Aliquippa, United States of America

Aliquippa, United States of AmericaLanding (descent or approach)

On September 8, 1994, a Boeing 737-300 (registration N513AU) operated by USAir - US Airways was involved in an aviation accident near Aliquippa, United States of America during landing or approach. 132 people were killed. Investigators recorded the probable cause as: A loss of control of the airplane resulting from the movement of the rudder surface to its blowdown limit. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 16 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781208724Data APIEditorial standards
Aircraft registered N513AU
Aircraft registered N513AU. Photo: Paul Denton / CC BY 4.0, via Wikimedia Commons

USAir Flight 427 crashed near Aliquippa, Pennsylvania, while maneuvering to land at Pittsburgh International Airport, killing all 132 on board. The accident was caused by a rudder control system malfunction.

Accident Overview

On a scheduled domestic passenger flight from Chicago-O'Hare International Airport, Illinois, to Pittsburgh, Pennsylvania, the aircraft entered an uncontrolled descent and impacted terrain near Aliquippa, about 6 miles northwest of the destination airport. The flight, operating under 14 Code of Federal Regulations Part 121, had departed Chicago around 1810 with 2 pilots, 3 flight attendants, and 127 passengers. All 132 people on board were killed, and the airplane was destroyed by impact forces and fire.

Meteorological and Flight Conditions

Visual meteorological conditions prevailed for the flight, which operated on an instrument flight rules flight plan. The accident occurred while the aircraft was maneuvering to land at Pittsburgh International Airport.

Probable Cause

The official investigation determined the probable cause to be 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.