A320 Guide

1. AIRBUSFLIGHT INSTRUCTOR MEDIA
PREPARED BASED ONAIRBUSFLIGHT INSTRUCTOR MEDIA REV 13 DATED 08 AUG 2016
CPT. C.SANCAK
* AIRBUS STD OPERATING PROCEDURES
* SYSTEM RELATED PROCEDURES
* ABNORMAL AND EMERGENCY PROCEDURES
* HOW TO USE

7. CONTENTS OF AIRBUS STD OPERATING PROCEDURES
2. COCKPIT PREPARATION
3. BEFORE START, ENGINE SATART, AFTER START
4. TAXI&BEFORE TAKEOFF
5. TAKEOFF
6. CLIMB
7. CRUISE
8. DESCENT
8. AFTER LANDING, PARKING, SECURING THE A/C
1. A320 FLOW PATTERN
MAIN MENU

169. CONTENTS OF SYSTEM RELATED PROCEDURES
1. MODE REVERSION
2. NORMAL LAW PROTECTION
4. GROUND SPEED MINI
5. ILS APPROACH
6. GLIDE SLOPE INTERCEPTION FROM ABOVE
7. VOR/NDB USING FINAL APPROACH
8. LOC/VOR/NDB APP USING TRK-FPA
9. RNAV(GNSS) APP WITH LNAV/VNAV MIN
10. USE OF FPV-ILS RAW DATA
11. GO-AROUND
12. VISUAL CIRCUIT
13. CIRCLING
14. LOW VISIBILITY OPERATIONS
3. RECONFIGURATION LAW
15. RWY OVERRUN PREVENTION SYSTEM
16. AIRBORNE TRAFFIC SIT AWARENESS
MAIN MENU

451. CONTENTS OF ABNORMAL AND EMERGENCY PROCEDURES
2. ECAM MANAGEMENT
3. ENGINE START FAULT
4. REJECTED TAKEOFF AND EMC EVACUATION
5. ENGINE FAILURE AFTER V1
6. FLAPS LOCKED DURING RETRACTION
8. WINDSHEAR
9. TCAS
10. EGPWS
11. FLIGHT CREW INCAPACITATION
12. UNRELIABLE SPEED INDICATION
13. TOTAL LOSS OF FCU
14. SMOKE
15. FUEL LEAK
16. ELEC EMER CONFIG
17. EIS FAILURE SWITCHING
18. DUAL RADIO ALT FAILURE
19. DUAL FMGC FAILURE
20. HYD G+Y SYS LO PR
21. HYD G+B SYS LO PR
22. ENG FAILURE IN CRUISE
23. ALL ENGINE FLAME OUT
24. EMERGENCY DESCENT
25. LOW ENERGY AURAL ALERT
26. STALL RECOVERY
1. MEL-MMEL USE
7. SLATS FAULT DURING EXTENSION
MAIN MENU

525. A318/A319/A320/A321
FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
WINDSHEAR
Ident.: PRO-ABN-80-00012271.0002001 / 10 JUN 13
Applicable to: ALL
A red flag “WINDSHEAR” is displayed on each PFD associated with an aural synthetic voice
“WINDSHEAR” repeated three times.
If windshear is detected either by the system or by pilot observation, apply the following recovery
technique:
 At Takeoff:
 If before V1:
The takeoff should be rejected only if significant airspeed variations occur below indicated
V1 and the pilot decides that there is sufficient runway remaining to stop the airplane.
 If after V1:
THR LEVERS...............................................................................................................TOGA
REACHING VR........................................................................................................ROTATE
SRS ORDERS........................................................................................................ FOLLOW
If necessary the flight crew may pull the sidestick fully back.
Note: If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °.
Then, if necessary, to prevent a loss in altitude, increase the pitch attitude.
 Airborne, initial climb or landing:
THR LEVERS AT TOGA.............................................................................. SET OR CONFIRM
AP (if engaged)............................................................................................................ KEEP ON
SRS ORDERS...............................................................................................................FOLLOW
If necessary the flight crew may pull the sidestick fully back.
Note: 1. Autopilot disengages if the angle of attack value goes above α prot.
2. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °.
Then, if necessary, to prevent a loss in altitude, increase the pitch attitude.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF
WINDSHEAR.
CLOSELY MONITOR FLIGHT PATH AND SPEED.
RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF WINDSHEAR.
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540. 34.08A
A318/A319/A320/A321
QUICK REFERENCE HANDBOOK
ABNORMAL AND
EMERGENCY PROCEDURES
22 MAR 16
TCAS WARNINGS
 Traffic advisory: “TRAFFIC” messages:
Do not perform a maneuver based on a TA alone.
 Resolution advisory : All “CLIMB” and “DESCEND” or “MAINTAIN
VERTICAL SPEED MAINTAIN” or “LEVEL OFF, LEVEL OFF” or “MONITOR
VERTICAL SPEED” type messages:
AP (if engaged)................................................................................................ OFF
BOTH FDs........................................................................................................OFF
Respond promptly and smoothly to an RA by adjusting or maintaining the pitch,
as required, to reach the green area and/or avoid the red 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 Vαmax and VMAX.
Respect stall, GPWS, or windshear warning.
Notify ATC.
 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 ft.
 When “CLEAR OF CONFLICT” is announced:
Resume normal navigation in accordance with ATC clearance.
AP/FD can be re-engaged as desired.
THY MSN 5584 TC-JSI
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561. A318/A319/A320/A321
FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
EGPWS WARNINGS
Ident.: PRO-ABN-34-00016878.0019001 / 17 MAR 16
Applicable to: MSN 2156, 2395-2401, 2522, 2609-2626, 2738-3126, 3185-3257, 3283-3303, 3341-3350, 3405-3738, 4629-7299
 "PULL UP" - "TERRAIN AHEAD PULL UP" - "OBSTACLE AHEAD PULL UP"
Simultaneously:
AP.......................................................................................................................................... OFF
PITCH............................................................................................................................PULL UP
L2
Pull to full backstick and maintain in that position.
L1 THRUST LEVERS..............................................................................................................TOGA
SPEED BRAKES lever............................................................................. CHECK RETRACTED
BANK................................................................................................WINGS LEVEL or ADJUST
L2
Aircraft achieve the best climb performance when the wings are as level as possible.
If the "TERRAIN AHEAD PULL UP" or "OBSTACLE AHEAD PULL UP" aural alert triggers, a
turning maneuver can be initiated if the flight crew concludes that turning is the safest action.
The PULL UP maneuver must be performed before the turn towards the safe direction, as
climbing increases the terrain clearance.
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587. A318/A319/A320/A321
FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
THY A318/A319/A320/A321 FLEET PRO-ABN-34 P 123/128
FCOM AU → 07 JUN 16
UNRELIABLE SPEED INDICATION
Applicable to: MSN 4643-4654, 4682, 4698-4706, 4761, 4779-4788, 5077-7299
Ident.: PRO-ABN-34-AM-00017720.0002001 / 30 NOV 15
 If the safe conduct of the flight is impacted:
AP/FD.................................................................................................................................... OFF
A/THR.................................................................................................................................... OFF
PITCH/THRUST:
Below THRUST RED ALT.........................................................................................15° / TOGA
Above THRUST RED ALT and Below FL 100.............................................................10° / CLB
Above THRUST RED ALT and Above FL 100...............................................................5° / CLB
FLAPS (if CONF 0(1)(2)(3)).......................................................... MAINTAIN CURRENT CONF
FLAPS (if CONF FULL)........................................................ SELECT CONF 3 AND MAINTAIN
SPEEDBRAKES........................................................................................CHECK RETRACTED
L/G........................................................................................................................................... UP
When at, or above MSA or Circuit Altitude: Level off for troubleshooting.
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742. 80.05A
A318/A319/A320/A321
QUICK REFERENCE HANDBOOK
ABNORMAL AND
EMERGENCY PROCEDURES
07 JUN 16
EMER DESCENT
CREW OXY MASKS............................................................................................USE
SIGNS.....................................................................................................................ON
EMER DESCENT..........................................................................................INITIATE
 If A/THR is not active:
THR LEVERS................................................................................................. IDLE
SPD BRK............................................................................................................ FULL
WHEN DESCENT ESTABLISHED
SPEED.....................................................................................MAX/APPROPRIATE
CAUTION Descend at the maximum appropriate speed. If structural damage
is suspected, use the flight controls with care and reduce speed as
appropriate.
Landing gear may be extended. In such a case, speed must be reduced to VLO/VLE.
ENG MODE SEL.................................................................................................IGN
ATC...............................................................................................................NOTIFY
Notify ATC of the nature of the emergency, and state intention. The flight crew can communicate with
the ATC using voice, or CPDLC when the voice contact cannot be established or has a poor quality.
EMER DESCENT (PA)......................................................................... ANNOUNCE
The flight crew must inform the cabin of emergency descent on the PA system.
ATC XPDR 7700.....................................................................................CONSIDER
Squawk 7700 unless otherwise specified by ATC.
‐ To save oxygen, set the oxygen diluter selector to the N position
‐ If the oxygen diluter selector remains set to 100 %, oxygen quantity may be insufficient to cover the
entire emergency descent profile
‐ Ensure that crew communication is established with oxygen masks. Avoid the continuous use of the
interphone to minimize interference with the breathing noise in the oxygen mask.
MAX FL........................................................................................... 100/MEA-MORA
 If CAB ALT is above 14 000 ft:
PAX OXY MASKS................................................................................. MAN ON
This action confirms that the passenger oxygen masks are released.
Note: Notify the cabin crew when the aircraft reaches a safe flight level, and when cabin oxygen
is no more necessary.
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758. A318/A319/A320/A321
FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
THY A318/A319/A320/A321 FLEET PRO-ABN-10 P 27/28
FCOM I to J 07 JUN 16
STALL RECOVERY
Ident.: PRO-ABN-10-00013768.0001001 / 18 MAR 11
Applicable to: ALL
As soon as any stall indication (could be aural warning, buffet...) is recognized, apply the immediate
actions:
NOSE DOWN PITCH CONTROL.............................................................................................APPLY
This will reduce angle of attack
Note: In case of lack of pitch down authority, reducing thrust may be necessary.
BANK............................................................................................................................WINGS LEVEL
 When out of stall (no longer stall indications) :
THRUST...........................................................................INCREASE SMOOTHLY AS NEEDED
Note: In case of one engine inoperative, progressively compensate the thrust asymmetry
with rudder.
SPEEDBRAKES.........................................................................................CHECK RETRACTED
FLIGHT PATH.........................................................................................RECOVER SMOOTHLY
 If in clean configuration and below 20 000 ft :
FLAP1........................................................................................................................SELECT
Note: If a risk of ground contact exists, once clearly out of stall (no longer stall
indications), establish smoothly a positive climb gradient.
STALL WARNING AT LIFT-OFF
Ident.: PRO-ABN-10-00013769.0001001 / 18 MAR 11
Applicable to: ALL
Spurious stall warning may sound in NORMAL law, if an angle of attack probe is damaged. In this
case, apply immediately the following actions:
THRUST..................................................................................................................................... TOGA
At the same time:
PITCH ATTITUDE..........................................................................................................................15 °
BANK............................................................................................................................WINGS LEVEL
Note: When a safe flight path and speed are achieved and maintained, if stall warning
continues, consider it as spurious.
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