Airbus 319, 320, 321 Flight Crew Operating Manual1 Systems by PDF

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1 SYSTEMS DESCRIPTION HIGHLIGHTS REV035 V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1 22 20 006 110 REV026 CODE 0072 - DELETION OF MOD 30635 1 22 20 008 100 REV026 CODE 0072 - DELETION OF MOD 30635 1 22 20 014 110 REV028 CODE 0207 - INCORPORATION OF MOD 24852 - DELETION OF MOD 24582 1 22 20 023 001 REV035 CODE 0358 - TECHNICAL AMENDMENT 1)No technical change.

New page created for repagination purposes. 1 22 30 071 200 REV025 CODE 0389 - INCORPORATION OF MOD 25346 - DELETION OF MOD 24414 1 22 40 005 120 REV035 - 1 23 20 005 24215=24588=25534 CFM:ALL INCORPORATION OF MOD 24215 INCORPORATION OF MOD 25534 VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers. 100 REV035 27699=(27699+31907) - TECHNICAL AMENDMENT 1)Note added to explain the procedure to couple the DME reception to the ILS or MLS reception.

75 PAGE 6 318/319/320/321 FCOM VOL. 1 SYSTEMS DESCRIPTION HIGHLIGHTS REV035 V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1)Suppression of the Geometric Altitude description that was inadvertently introduced on this page. 2)TAD and TCF have been added to the list of events that can cause the GPWS light to come on. 3)Text modified for improved technical understanding.

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