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— THR LEVERS   IDLE
— OPTIMUM RELIGHT SPD   300 KT
In case of a speed indication failure (volcanic ash) the pitch attitude for optimum relight speed is —4.5° (for weights above 50000 kg/110000 lb add 1° for each 10 000 kg/ 22 000 lb).
At 300 knots, the aircraft can fly up to about :
. 2 NM/1000 feet at 50 000 kg/110 000 lb
. 2.2 NM/1000 feet at 60 000 kg/132 000 lb
. 2.4 NM/1000 feet at 70 000 kg/154 000 lb
— EMER ELEC PWR (if EMER GEN not in line)   MAN ON
— VHF1/HF1 ()/ATC1   USE
. Notify traffic control of the nature of the emergency, and state intentions.
If there is no contact with air traffic control, switch to code A7700, or transmit a distress
message on one of the following frequencies : VHF 121.5 MHz, HE 2182 KHz or 8364 KHz.
— FAC 1   OFF THEN ON
The aircraft is out of trim due to right aileron upfloat.
Resetting FAC 1 permits rudder trim recovery, even if no indication is available.
* IF NO RELIGHT AFTER 30 SEC : — ENG MASTERS   OFF 30 S/ON
* WHEN APU AVAIL FL < 200 :
If the APU is available, it may be started when below FL 250, and the APU BLEED used for engine start below FL 200.
— APU BLEED   ON
— ENG MASTERS   OFF 30 S/ON
Start one engine at a time.
— OPTIMUM SPEED   G DOT
Green dot is displayed on the Captain's PFD. It represents the best lift-to-drag ratio.
* EARLY IN APPR (If ditching is foreseen, apply the DITCHING procedure, instead of the following) :
— CAB SECURE   ORDER
— USE RUDDER WITH CARE
As hydraulic power is available from RAT only, avoid large or rapid rudder deflection.
— FOR LDG   USE FLAP 3
As only blue hydraulic power is available, only the slats will extend, and operating times noticeably increase.
* AT 5000 FT AGL :
— L/G   GRVTY EXTN
— TARGET SPEED   150 KT
* AT TOUCHDOWN :
— ENG MASTERS   OFF
— APU MASTER SW   OFF
— EVAC   INITIATE
— BAT 1 +2
(If time permits before leaving aircraft)   OFF
Batteries are left ON, until leaving the aircraft, to ensure cabin communications.
NOTE: Keep batteries on for at least 10 seconds, after switching the ENG MASTERS to OFF, to allow complete closure of the fuel LP valves.A319/A320/A321
ovilm.i.
EMERGENCY PROCEDURES
REV 36
„
1 . 15

SEQ 105

 Traffic advisory : "TRAFFIC" messages
— Do not maneuver based on a TA alone. — Attempt to see the reported traffic.
— Preventive resolution advisory : "MONITOR VERTICAL SPEED"
message
— Maintain or adjust the vertical speed, as required, to avoid the red area of the vertical speed scale.
— Attempt to see the reported traffic. — Notify ATC.
— When "CLEAR OF CONFLICT" is announced :
Resume normal navigation in accordance with ATC clearance.
R Corrective resolution advisory : All "CLIMB" and "DESCEND"
or "MAINTAIN VERTICAL SPEED MAINTAIN" or "ADJUST
VERTICAL SPEED ADJUST" type messages.
— Respond promptly and smoothly to an RA.
— AP (if engaged)   OFF
— BOTH FDs   OFF
— Adjust the vertical speed, as required, to that indicated on the green area of the vertical speed scale.
NOTE : Avoid excessive maneuvers while aiming to keep the vertical speed just outside
the red area of the VSI, and within the green area. If necessary, use the full speed range between Vamax and Vmax.
— Respect stall, GPWS, or windshear warning. — Attempt to see the reported traffic.
— Notify ATC.
— When "CLEAR OF CONFLICT" is announced :
. Resume normal navigation in accordance with ATC clearance. . AP/FD can be re-engaged as desired.
• GO AROUND procedure must be performed when an RA "CLIMB" or "INCREASE CLIMB" is triggered on final approach.
NOTE: Resolution Advisories (RA) are inhibited below 900 feet.
A319/A320/A321
ovilm.i.
EMERGENCY PROCEDURES
REV 36
„
1 . 16

SEQ 219
ENG DUAL FAILURE
LAND ASAP
— ENG MODE SEL   IGN
— THR LEVERS   IDLE
— OPTIMUM RELIGHT SPD   300 KT
In case of a speed indication failure (volcanic ash), the pitch attitude for optimum relight speed is —4.5° (for weights above 50000 kg/110000 lb, add 1° for each 10000 kg/22000 lb). At 300 knots, the aircraft can fly up to about :
. 2 NM/1000 feet at 50000 kg/110000 lb
. 2.2 NM/1000 feet at 60000 kg/132000 lb
　
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