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CIRCLING ONE ENGINE INOPERATIVE 14/16
ONE ENGINE INOPERATIVE GO-AROUND 15/16
Thrust Levers Management in Case of Inoperative Reverser(s) 15/16
AO-022. AUTOFLIGHT
FMGC FAILURE 1/2
AO-024. ELECTRICAL
INTRODUCTION TO EMERGENCY ELECTRICAL CONFIGURATION 1/4
TECHNICAL BACKGROUND 1/4
GENERAL GUIDELINES 1/4
REMAINING SYSTEMS 2/4
RESTORATION FROM EMER ELEC 3/4
AO-026. FIRE PROTECTION
PREFACE 1/6
SMOKE DETECTION AND PROCEDURE APPLICATION 1/6
COORDINATION WITH CABIN CREW 2/6
SMOKE/FUMES/AVNCS SMOKE PAPER PROCEDURE 3/6
CARGO SMOKE 5/6
TABLE OF CONTENTS
AO-27. FLIGHT CONTROLS
ABNORMAL FLAPS/SLATS CONFIGURATION 1/6
ELEVATOR REDUNDANCY LOST 3/6
AO-28. FUEL
FUEL LEAK 1/2
AO-29. HYDRAULIC
HYDRAULIC GENERATION PARTICULARITIES 1/4
DUAL HYDRAULIC FAILURES 2/4
REMAINING SYSTEMS 3/4
AO-032. LANDING GEAR
LDG WITH ABNORMAL L/G 1/4
Nose Wheel Steering Fault 2/4
LOSS OF BRAKING 2/4
AO-034. NAVIGATION
ADR/IRS FAULT 1/8
UNRELIABLE AIRSPEED INDICATIONS 1/8
ADR CHECK PROC / UNRELIABLE SPEED INDICATION QRH PROCEDURE 3/8
DUAL RADIO ALTIMETER FAILURE 8/8
AO-070. POWER PLANT
ALL ENGINE FLAMEOUT 1/2
AO-090. MISCELLANEOUS
EMERGENCY DESCENT 1/4
OVERWEIGHT LANDING 3/4
CREW INCAPACITATION 4/4
SUMMARY OF HIGHLIGHTS
Localization
Title Page ID Reason
AO-010
Vapp DETERMINATION 1/6 1 Revised to clarify the VAPP determination according to the new methodology regarding the calculation of the landing distance with failure.
Anchored part F.00004115.0001001.033 moved from
F.00004115.0001001.002 to F.00004115.0001001.002
AO-010
IN FLIGHT LANDING DISTANCE CALCULATION FOLLOWING FAILURES 4/6 2 Deleted part inside
AO-010
IN FLIGHT LANDING DISTANCE CALCULATION FOLLOWING FAILURES 4/6 3 Deleted textual part
Revised to introduce the new methodology regarding the calculation of the landing distance with failure.
Deleted part inside
AO-020
INTRODUCTION TO EMERGENCY EVACUATION 4/16 1 Deleted textual part
AO-020
Thrust Levers Management in Case of Inoperative Reverser(s) 15/16 2 Text modified for improved technical understanding and for clarification.
AO-024
GENERAL GUIDELINES 1/4 1 To specify that ILS1 is recovered when LAND RECOVERY is set to ON only if Multi-Mode Receiver (MMR) is not installed.
AO-024
REMAINING SYSTEMS 2/4 2 Solution revised to indicate that the DME1 is available in the case of an electrical emergency configuration when the emergency generator is powered by the EDP.
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A330/A340 机组训练手册 FCTM Flight Crew Training Manual 2(18)
