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Dec. 9, 2001 Lawrence, Kansas, U.S. Dassault Falcon 100 substantial 2 none
During a visual approach in daytime VMC, the airplane pitched nose-down about 20 feet AGL. Both pilots said that they applied nose-up pitch control but were not able to adjust the pitch attitude for a normal landing.The airplane landed hard, breaking the left-main landing-gear strut, which penetrated the upper wing skin. After the accident, the pilots observed that the horizontal-stabilizer-trim indicator indicated full-nose-down trim and that the horizontal stabilizer appeared to be trimmed full-nose-down.The report said that a preliminary examination of the airplane showed that the horizontal stabilizer was positioned four degrees nose-down.The report said that the probable cause of the accident was “the copilot’s failure to maintain aircraft control during the landing” and that contributing factors were “the copilot’s improper in-flight decision not to execute a go-around, … inadequate crew coordination prior to landing … and the improperly set stabilizer trim.”
Jan. 6, 2002 Canary Islands, Spain Boeing 737-400 substantial 86 minor/none
The airplane touched down hard while landing at Puerta del Rosario International Airport in daytime IMC. Strong winds were reported at the airport.
Feb. 1, 2002 London, England Airbus A300B4 minor 3 none
A captain-in-training was the pilot flying during a nighttime positioning flight with no cargo aboard the airplane. The flight crew conducted an ILS approach to Runway 26L at London Gatwick Airport. Surface winds were reported from 210 degrees at 18 knots, gusting to 30 knots. At about 1,000 feet, the commander observed an inertial reference system (IRS) wind-speed readout of 70 knots. When the pilot flying began the flare, the left wing lowered; he applied right-aileron control and increased power. The airplane touched down first on the left-main landing gear, then on the right-main landing gear, and bounced. The pilot flying applied nose-down pitch control, and the airplane touched down hard on the nose landing gear and the right-main landing gear, causing the right-engine nacelle to strike the runway.
Feb. 14, 2002 West Palm Beach, Florida, U.S. Gulfstream V substantial 2 none
Soon after departure, the flight crew requested clearance to return to the airport because the landing gear had not retracted on command. As the airplane was flared for landing, the ground spoilers deployed. The airplane landed hard, and the right-main landing gear collapsed. The report said that wooden sticks were found in the weight-on-wheels switches for both main landing gear. The airplane was on jacks for a tire change when a maintenance technician used the sticks to disable the weight-on-wheels system so that he could access the maintenance-data-acquisition unit to check an overspeed message. The sticks were not removed after maintenance was completed. As a result, the airplane remained in ground mode, and the ground spoilers deployed when the crew moved the throttle levers to idle during the flare.
　
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