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When HYD G + B failed, extend landing gear at 200 kt to improve controllability on single
elevator.
In the case of a dual hydraulic failure, ECAM will give information on the STATUS page
concerning inoperative systems. Approach speed and landing distance increments will also
be shown on ECAM. However the figure given on ECAM for multiplying landing distance is
calculated on flap handle position and may be incorrect until the final CONF selection has
been made. The landing distance factors are available in QRH 2.25, along with speed
increments. Speed increments are based on VREF CONF FULL in all cases. When
calculating VAPP, see QRH 2.24 for information on the use of wind correction in failure
cases. Do not rush these calculations.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.29 Page 2
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
DUAL HYDRAULIC FAILURE
CHAP03\29
06 - COMPLETION STANDARDS
· Maintains a safe flight path.
· Ensures strict application of task sharing requirements.
· Ensures correct application of ECAM, QRH and FMGS procedures.
· Handles the aircraft smoothly without major deviations from required trajectory (+/- 200 ft ;
+/- 10 º ; +/- 10 kt).
· Makes correct determination of VAPP and landing distance.
· Performs accurate approach within standard limits for instrument approach.
· Lands within the landing zone and uses correct braking technique.
· Abnormal configuration approach procedure.
· Specific approach and go around briefing.
· Ensures any special requirements are communicated to ATC and cabin crew.
07 - COMMON ERRORS
· No emergency declared to ATC.
· Incorrect use of selected speed.
· Incorrect prioritization of tasks.
· Incomplete approach and go around briefing for abnormal configuration.
· FD not followed precisely due to over controlling.
· Confusion between VAPP/VREF/VLS for corrected speed.
· Approach initiated before completion of all necessary tasks.
· Not using QRH for gravity gear extension.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.29 Page 3
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
DUAL HYDRAULIC FAILURE
CHAP03\29
PAGE LEFT INTENTIONALLY BLANK
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.29 Page 4
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
DUAL HYDRAULIC FAILURE
CHAP03\29
PHILOSOPHY AND NORMAL USE
01 - TRAINING OBJECTIVE
· To fully understand the philosophy and normal use of the ECAM.
· To understand ECAM use for abnormal and emergency operations.
02 - SCHEDULE
Briefing duration : 15 minutes
03 - EQUIPMENT
DOC references :
· FCOM 1.31 10 to 1.31.30 (ECAM Description)
· FCOM 3.02.01(ABN and EMER PROCEDURES)
04 - INSTRUCTOR’S ACTIONS
Briefing of the following key points.
MAIN
· Warning levels and associated master lights.
· ECAM control panel.
· Switching.
· ECAM display philosophy.
· MEMO display.
SECONDARY
· Use of RCL and EMER CANC.
· Flight phases and associated displays.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.31 Page 1
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
ECAM
CHAP03\31
PHILOSOPHY AND NORMAL USE (CONT’D)
05 - TRAINEES’ ACTIONS
The Electronic Centralised Aircraft Monitoring (ECAM) system monitors and displays all
information concerning aircraft systems and system failures. It is a system which, through
text and graphic displays, enables the crew to do most things from ensuring passenger
comfort by monitoring cabin temperature to dealing with multiple system failures without the
need for paper checklists.
Essentially the ECAM provides the following :
· System indications - temperatures, pressures etc.
· System monitoring - display of system failure, level 1 to 3 or advisory.
· Memo - displays use of systems by the crew e.g. anti-ice and also take off and landing
memo.
· Crew actions - in case of failures the E/WD indicates crew action necessary to deal with the
failure, replacing the traditional QRH.
· Status - the status page provides the crew with an operational summary of the aircraft
systems at any stage of the flight. If STS is displayed on E/WD, when CONF 1 is selected,
the STATUS page is automatically displayed.
Display of system failures and take off / landing memo is flight phase sensitive. Take off and
landing memo are only displayed at the appropriate time. Before announcing "no
　
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