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GEN
12/14
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
GENERAL
30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , , ,
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X Abbreviation Term
XBLD Crossbleed
XCVR Transceiver
XFR Transfer
XMTR Transmitter
XPDR Transponder
XTK Crosstrack Error
Y Abbreviation Term
Z
Abbreviation Term
ZFCG Zero Fuel Center of Gravity
ZFW Zero Fuel Weight
IMPORTANT
SCOPE
The QRH contains some specific procedures which are not displayed on the ECAM.
As a general rule, the procedures displayed on the ECAM are not provided in the
QRH (refer to FCOM
PRO/ABN).
TASKSHARING FOR ABN/EMER PROC
For all abnormal/emergency procedures, the tasksharing is as follows :
‐ PF - Pilot flying - Responsible for the :
• Thrust levers
• Flight path and airspeed control
• Aircraft configuration (request configuration change)
• Navigation
• Communications
‐ PNF - Pilot non flying - Responsible for the :
• Monitoring and reading aloud the ECAM and checklists
• Performing required actions or actions requested by the PF, if applicable
• Using engine master switches, IR and guarded switches with PF's confirmation.
ECAM CLEAR
DO NOT CLEAR ECAM WITHOUT CROSS-CONFIRMATION OF BOTH
PILOTS.
ABN/EMER PROC INITIATION
Procedures are initiated on pilot flying command.
No action will be taken (apart from audio warning cancel through MASTER WARN
light) until :
‐ The appropriate flight path is established, and
‐ The aircraft is at least 400 ft above the runway, if a failure occurs during takeoff,
approach, or
go-around. (In some emergency cases, provided the appropriate flight path is
established, the pilot
flying may initiate actions before this height).
NORMAL CHECKLIST
Normal C/L are initiated by the PF and read by the PNF.
The PF shall respond after having checked the existing configuration. When both
pilots have to respond,
"BOTH" is indicated.
GEN
13/14
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
GENERAL
30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , , ,
, , , , ,
USE OF SUMMARIES
GENERAL
In case of an electrical emergency configuration, or a dual hydraulic failure :
The ECAM should be applied first.
This includes both the procedure, and the STATUS section.
Only after announcing "ECAM ACTIONS COMPLETED", should the Pilot Non
Flying (PNF) refer to the
corresponding QRH summary.
When a failure occurs, and after performing the ECAM actions, the PNF must refer to
the bottom of the
applicable Summary page (below the Go-Around section), in order to determine the
landing distance that
takes into account the failure.
For dry and wet runways, the Actual Landing Distances with failure are provided in
the SUMMARIES.
These Actual Landing Distances with failure are based on the following assumptions:
The approach speed ‐ is VREF + ΔVREF (Refer to ABN-24-SUM ELEC EMER
CONFIG Summary -
Cruise). The speed increment "APPR COR" (when applicable), and the corresponding
landing distance
penalties that are required when the A/THR is used, or in the case of ice accretion on
surfaces that are
not heated, are not taken into account.
‐ These distances are computed without the benefit of the reverse thrust (i.e. using
the LDG DIST
Factors 'WITHOUT REV" )
. If the flight crew wants to take into account the benefit of the reverse thrust at
landing, the Actual
Landing Distance with failure must be computed by multiplying the two following
parameters:
• The LDG DIST Factor "WITH REV" (refer to QRH PRO/ABN 80), and
• The Actual Landing Distance without failure (Refer to FPE-IFL Landing Distance
Without
AUTOBRAKE - CONF FULL)
For contaminated runways, the LDG DIST Factors provided in the SUMMARIES are
the LDG DIST
Factors "WITHOUT REV" .
Depending on the actual landing distance with failure, the PNF can decide whether or
not a diversion is
necessary.
APPROACH PREPARATION
As always, approach preparation includes a review of the ECAM STATUS.
After reviewing the STATUS, the PNF should refer to the "CRUISE" portion of the
summary (Refer
to ABN-24-SUM ELEC EMER CONFIG Summary - Cruise), to determine the VREF
correction, and
compute the VAPP.
A VREF table is provided in the summary, for failure cases leading to the loss of the
MCDU.
The LANDING and GO-AROUND portions of the summary should be used for the
　
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