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Original report numbering: Original p. 9; page may span adjacent original pages. PDF rendering page 4.
rotation being equivalent of circumferential speed of 72 kts began to operate after about 4 seconds. Rollout of the aircraft progressed in conditions of heavy rain and with a layer of water on the runway. Aircraft was decelerated according toOpen report transcription at PDF page 4Report on the Accident to Airbus A320-211 Aircraft in Warsaw on 14 September 1993
Original report numbering: Original p. 35, 36; page may span adjacent original pages. PDF rendering page 31.
brakes, dependent on the rotation gain to circumferential speed of 72 kts began to operate about 4 seconds later. Rollout, as well as the whole landing and final approach progressed in the heavy rain and with the presence of theOpen report transcription at PDF page 31Report on the Accident to Airbus A320-211 Aircraft in Warsaw on 14 September 1993
Original report numbering: Original p. 28; page may span adjacent original pages. PDF rendering page 22.
35°), with manual operation of flight controls and thrust. During the final approach (about MM) momentary decrease of airspeed from the value CAS = 154 kts by 12 kts was recorded on DFDR and QAR with duration of about 15Open report transcription at PDF page 22Report on the Accident to Airbus A320-211 Aircraft in Warsaw on 14 September 1993