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PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 62/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 63/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 64/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 65/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 66/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 67/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 68/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 69/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - IN CRUISE QUICK CHECK
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ICQ-50 P 70/70
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ONE ENGINE INOPERATIVE - GENERAL
A318/A319/A320/A321 FLEET PER-CRZ-OEI-GEN-05 P 1/2
FCOM 19 AUG 10
GENERAL
INTRODUCTION
Applicable to: ALL
This chapter provides the single engine performance data to be used for the conduct and monitoring
of the flight following an engine failure.
The diversion strategy (descent and cruise speed schedules) shall be selected, and specified in the
operator’s routes specifications, as a function of the prevailing operational factors (e.g. obstacles
clearance requirements and/or ETOPS operation).
FLIGHT PREPARATION
Applicable to: ALL
In readiness for a possible engine failure occurring during the flight, any flight shall be planned so as
to comply with any of the following requirements, as applicable :
• obstacle clearance,
• oxygen,
• maximum diversion distance (ETOPS operation).
The following FCOM sections provide flight preparation and fuel planning information :
• PER FPL-FLP, for Standard Fuel Planning,
• PRO SPO-40, for Extended Range Operation (ETOPS) and associated fuel requirements.
STRATEGY
Applicable to: ALL
Depending on the prevailing operational constraints, the most appropriate diversion strategy shall be
selected, out of the following options :
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ONE ENGINE INOPERATIVE - GENERAL
A318/A319/A320/A321 FLEET PER-CRZ-OEI-GEN-05 P 2/2
FCOM 19 AUG 10
STANDARD FIXED SPEED STRATEGIES
STRATEGY
OBSTACLE
STRATEGY 320 kt VMO
DESCENT
TO CEILING
• M .78/300 kt
• MCT
• Green Dot Speed
• MCT
• M .78/320 kt
• MCT
• M .80/350 kt
• MCT
CRUISE LR ceiling
LR speed
‐ Obstacle not
cleared:
Maintain Green Dot
Speed at MCT
‐ Obstacle cleared :
Revert to standard
strategy
FL per Refer to
PRO-SPO-40-60 ONE
ENGINE OUT-CRUISE
AT 320KT
MCT/320 kt
FL per Refer to
PRO-SPO-40-60 ONE
ENGINE OUT-CRUISE
AT 350KT
MCT/350 kt
DESCENT
TO LANDING IDLE/M .78/300 kt/250 kt
Approx increase in
fuel consumption
compared with both
engines operative
+33 %
For ETOPS operations, any of the above diversion strategies can be used provided that the selected
strategy and speed schedule is used in :
establishing the area of operation (maximum diversion distance), ‐ as described in PRO SPO 40,
‐ calculating the diversion fuel requirements for the single engine ETOPS critical scenario, as
provided in PRO SPO 40,
‐ demonstrating the applicable obstacle clearance requirements (net flight path and net ceiling).
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 6(5)
