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FCOM 19 AUG 10
FCOM PROCEDURE LAYOUT
Applicable to: ALL
INTRODUCTION
The presentation of procedures is, as far as practicable, identical to the presentation on ECAM.
The abbreviations are identical to those used on the cockpit panels. All actions and information
displayed on ECAM are provided in large letters. Other information, not on ECAM, is provided in
small letters.
Expanded information, when inserted in the procedure, appears in italics. This information:
‐ Identifies the particular failures
‐ Explain actions for which the reason is not self-evident
‐ Furnishes additional background.
PROCEDURE TITLE
The title of an abnormal or emergency procedure, that appears on the ECAM is:
‐ Red for a warning
‐ Amber for a caution
The title of an abnormal or emergency procedure, that does not appear on the ECAM is:
‐ Red for a warning
‐ Amber for a caution
‐ On a grey background.
SEVERAL ALERTS UNDER THE SAME TITLE
When applicable, several alerts may be grouped under the same procedure title. However,
depending on the failure, the actions that the flight crew should perform may differ.
CONDITIONS
BLACK SQUARE
When several procedures appear under the same title, a black square marks the starting point
of each procedure.
Only one procedure is applicable at a time.
For example:
ANTI-ICE CAPT (F/O) (STBY) PROBES
■ CAPT PROBES } a
■ F/O PROBES } b
■ STBY PROBES } c
procedure to be applied:
a or b or c
Black squares also indicate parts of a procedure among wich only one is applicable.
For example:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
INTRODUCTION
A318/A319/A320/A321 FLEET PRO-ABN-01 P 4/4
FCOM 19 AUG 10
F/CTL ADR DISAGREE
AIR SPD ...................X CHECK } a
■ IF NO SPD DISAGREE } b
■ IF SPD DISAGREE } c
procedure to be applied:
(a + b) or (a + c)
The ECAM does not display black squares.
BLACK DOT
If an action depends on a precondition, a black dot identifies the precondition. If the precondition
appears on ECAM, it appears in LARGE LETTERS. If not, it appears in small letters.
For example:
F/CTL FLAPS FAULT
FLAPS LEVER ............RECYCLE
• If unsuccessful
GPWS FLAP MODE ......OFF
"If unsuccessful" is not displayed on ECAM
INDENTATION
Indentation is use in order to identify when an action depends on a precondition/flight
phase/procedure.
For example:
■ IN FLIGHT
• If Flaps locked
APPR SPEED .....................................Vref + 30
MAX SPEED ....................................................250 kt
INCREASED FUEL CONSUMP
The APPR SPEED is equal to VREF +30 kt only ‐ if the flaps are locked, because "APPR
SPEED......VREF +30" is indented below "• If flaps locked".
‐ The MAX SPEED of 250 kt does not depend on the flaps locked condition because it is
aligned with "• If flaps locked". Therefore, MAX SPEED has to be respected whether the flaps
are locked or not.
‐ INCREASED FUEL CONSUMP is aligned with IN FLIGHT. Therefore, this information is valid
in flight and on ground.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 1/22
FCOM 19 AUG 10
REJECTED TAKEOFF
Applicable to:
,
,
MSN,,,,
GENERAL
The decision to reject the takeoff and the stop action is made by the Captain.
It is therefore recommended that the Captain keeps his hand on the thrust levers until the aircraft
reaches V1, whether he is Pilot Flying (PF) or Pilot Not Flying (PNF). As soon as he decides to
abort, he calls “stop”, takes over control of the aircraft and performs the stop actions.
It is not possible to list all the factors that could lead to the decision to reject the takeoff.
However, in order to help the Captain to make a decision, the ECAM inhibits the warnings that
are not essential from 80 kt to 1 500 ft (or 2 min after lift-off, whichever occurs first).
Experience has shown that rejected takeoffs can be hazardous even if the performance is
correctly calculated, based on flight tests.
This may be due to the following factors:
Delay in Performing ‐ the stopping procedure.
‐ Damaged tires.
‐ Brakes worn, brakes not working correctly, or higher than normal initial brakes temperature.
‐ The brakes not being fully applied.
‐ A runway friction coefficient lower than assumed in computations.
‐ An error in gross weight calculation.
　
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