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Original report numbering: Original p. 9; page may span adjacent original pages. PDF rendering page 4.
deceleration decreased by about 30 %. Residual length of the runway (left from the moment when braking systems had begun to work) was to small to enable the aircraft to stop on the runway. Seeing the approaching end of runway,Open 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. 15; page may span adjacent original pages. PDF rendering page 10.
OFF position by the crew. 1.6.4 Automatic equipment Automatic operation of aircraft braking systems was described in 1.6.3 above. 1.6.5 Other relevant aircraft systems The aircraft is fitted with two independent EFIS (Electronic Flight Instrument system). The system prOpen report transcription at PDF page 10Report 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.
Airbus A320 automatic systems dependent on compression of oleo struts armed all three braking systems only at the moment of recorded contact of the left main landing gear assembly with the runway (15:33:57). Systems began to work, spoilers were deployedOpen 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. 44; page may span adjacent original pages. PDF rendering page 38.
design features of the aircraft which limited the feasibility of applying available braking systems as well as by insufficient information in the aircraft operations manual (AOM) relating to the increase of the landing distance. 44 4. Recommendations 4.1 For operatorOpen report transcription at PDF page 38Report on the Accident to Airbus A320-211 Aircraft in Warsaw on 14 September 1993