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December 1999
Business
              Jet Overruns Wet Runway After Landing Past Touchdown Zone 6 pages. [PDF 66K]
Recorded radar data showed groundspeeds of more
              than 160 knots when the Cessna Citation 500 was on final approach.
              The aircraft struck a navigational-aid-support structure, terrain
              and two mobile homes off the departure end of the runway. The three
              occupants were injured during the impact, but they exited the aircraft
              before it was destroyed by fire.
November 1999
Unaware
              of Strong Crosswind, Fokker Crew Loses Control of Aircraft on Landing
              6 pages. [PDF 62K]
During approach to Guernsey, United Kingdom, the
              pilots of the Fokker F27 received a report containing an average
              of wind-speed values recorded over a two-minute period. They did
              not request a report of instantaneous wind speed. Thus, the pilots
              did not know that sudden, strong gusts exceeded the crosswind limit
              in the company operations manual. The aircraft touched down about
              mid-field, according to witnesses, then overran the end of the runway,
              veered left and struck an embankment.
October 1999
Erroneous
              Airspeed Indications Cited in Boeing 757 Control Loss 8 pages. [PDF 69K]
Investigators concluded that the airplane had a
              blocked pitot tube and that, during departure, the flight crew became
              confused by false indications of increasing airspeed and did not
              respond to a stall warning. All the occupants were killed when the
              airplane struck the Caribbean Sea off the northern coast of the
              Dominican Republic.
September 1999
Rudder
              Malfunction Causes Loss of Control of Boeing 737 16 pages. [PDF 208K]
All 132 occupants were killed when the airplane
              struck terrain near Pittsburgh, Pennsylvania, U.S. The investigation
              report said that, following an encounter with wake turbulence, the
              airplane’s rudder moved to the limit of its travel, in a direction
              opposite to that commanded by the flight crew. The report said that
              the rudder-control anomaly most likely was caused by a malfunction
              of the rudder’s main power control unit.
August 1999
Double
              Engine Failure Leads to Ditching of Cessna 402C 6 pages. [PDF 52K]
The investigation concluded that fuel exhaustion
              might have caused both engines to fail while the airplane was on
              a scheduled flight in New Zealand. Five of the 10 occupants were
              rescued. Four occupants were unable to find their life jackets and
              died before rescuers arrived. Another occupant was missing and presumed
              dead.
July 1999
Airplane’s
              Low-energy Condition and Degraded Wing Performance Cited in Unsuccessful
              Go-around Attempt 12 pages. [PDF 118K]
The Canadair Regional Jet’s airspeed was
              decreasing, and its engines were producing idle thrust when the
              crew rejected the landing 33 feet (10 meters) above the runway.
              The Transportation Safety Board of Canada said that there was insufficient
              time for the engines to spool up to go-around thrust, and that a
              thin accumulation of ice was a major factor in causing the airplane
              to stall at a lower-than-normal stall angle-of-attack. The crew
              lost control of the airplane, and the airplane struck the runway
              and terrain.
June 1999
Learjet
              Strikes Terrain When Crew Tracks False Glideslope Indication and
              Continues Descent Below Published Decision Height 12 pages. [PDF 120K]
The U.S. National Transportation Safety Board said
              that the flight crew did not follow standard operating procedures
              while conducting an instrument landing system approach. The investigation
              prompted the board to recommend acceleration of a proposed schedule
              for requiring installation of terrain awareness and warning systems
              in all turbine airplanes with six or more passenger seats.
May 1999
B-757
              Damaged by Ground Strike During Late Go-around from Visual Approach
              8 pages. [PDF 76K]
Deviations from standard operating procedures,
              deficient crew resource management and crew distraction were cited
              as factors in a controlled-flight-into-terrain accident that caused
              substantial airplane damage but no injuries.
April 1999
Jammed
              Elevator Prompts Twin-turboprop Rejected Takeoff, Runway Over-run
              8 pages. [PDF 93K]
The investigating authority said that deficiencies
              in the Hawker Siddeley 748 flight control gust-lock system might
              have caused the elevator gust lock to re-engage when the flight
              crew checked the flight controls at the beginning of the takeoff.
March 1999
Thin,
              Rough Ice Accumulation Causes Twin-turboprop Aircraft Upset
              12 pages. [PDF 82K]
The U.S. National Transportation Safety Board said
              that the absence of adequate aircraft-certification standards and
              operating procedures for flight in icing conditions was a probable
              cause of the accident, and that the flight crew’s acceptance
              of a relatively low airspeed restriction while operating in icing
              conditions was a contributing factor.
February 1999
Ice
              Ingestion Causes Both Engines to Flame Out During Air-taxi Turboprop’s
              Final Approach 8 pages. [PDF 62K]
The accident was attributed to the flight crew’s
              failure to comply with procedures requiring the use of continuous
              engine ignition during and after an encounter with icing conditions.
January 1999
Attempted
              Go-around with Deployed Thrust Reversers Leads to Learjet Accident
              6 pages. [PDF 49K]
The pilot said that he rejected the landing when
              the aircraft veered left after touchdown. He said that although
              the thrust levers were positioned full forward, the aircraft did
              not accelerate after lifting off the runway.