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A330/A340 FLEET PER-THR-MCR P 4/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
THRUST RATINGS
N1 MODE THRUST CONTROL
A330/A340 FLEET PER-THR-N1 P 1/6
FCOM 19 AUG 10
N1 MODE THRUST CONTROL
Applicable to: ,
In case of no EPR available, the thrust control automatically reverts to N1 mode (rated or unrated).
See PRO ABN 70, ENG EPR MODE FAULT.
If the N1 rated mode is lost on both engines, refer to the power management tables given on the
following pages.
The herebelow table gives the N1 to be set in cruise to maintain M 0.82
FLIGHT LEVEL
WEIGHT
(1 000 kg)
290 310 330 350 370 390 410
130 72.5 72.2 72.1 72.0 72.3 73.2 74.3
140 72.7 72.5 72.4 72.4 72.9 74.0 75.2
150 73.0 72.9 72.8 72.9 73.6 74.8 76.1
160 73.3 73.2 73.3 73.5 74.3 75.7 77.2
170 73.6 73.6 73.8 74.2 75.1 76.6 78.5
180 74.0 74.1 74.4 75.0 75.9 77.7 80.5
190 74.4 74.6 75.1 75.7 76.8 79.0 83.2
200 74.8 75.2 75.8 76.5 77.9 80.9
210 75.3 75.8 76.5 77.3 79.2 83.5
220 75.9 76.5 77.2 78.3 81.0
230 76.5 77.2 78.0 79.5 83.3
240 77.2 77.9 78.9 81.1 N1 (%)
Drift down ceilings are decreased by 4 000 ft
• Go-around weights must be decreased by the following values
Normal go-around
weight (1 000 kg ) 150 160 170 180 190 200 210 220 230 240
Weight penalty (1 000 kg) 25.5 27.2 28.9 30.6 32.3 34.0 35.7 37.4 39.1 40.8
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
THRUST RATINGS
N1 MODE THRUST CONTROL
A330/A340 FLEET PER-THR-N1 P 2/6
FCOM 19 AUG 10
TAKEOFF N1
Applicable to: ,
Note: Corner point temperature :
ISA +22 °C for pressure altitude ≤ 2 000 ft
ISA +15 °C for5 000 ft ≤ pressure altitude ≤ 8 000 ft
linear interpolation in between
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
THRUST RATINGS
N1 MODE THRUST CONTROL
A330/A340 FLEET PER-THR-N1 P 3/6
FCOM 19 AUG 10
GO AROUND N1
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
THRUST RATINGS
N1 MODE THRUST CONTROL
A330/A340 FLEET PER-THR-N1 P 4/6
FCOM 19 AUG 10
Note: Corner point temperature :
ISA +22 °C for pressure altitude ≤ 2 000 ft
ISA +15 °C for5 000 ft ≤ pressure altitude ≤ 8 000 ft
linear interpolation in between
MAXIMUM CONTINUOUS N1
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
THRUST RATINGS
N1 MODE THRUST CONTROL
A330/A340 FLEET PER-THR-N1 P 5/6
FCOM 19 AUG 10
MAXIMUM CLIMB N1
Applicable to: ,
Note: Corner point temperature : ISA + 10 °C
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
THRUST RATINGS
N1 MODE THRUST CONTROL
A330/A340 FLEET PER-THR-N1 P 6/6
FCOM 19 AUG 10
MAXIMUM CRUISE N1
Applicable to: ,
Note: Corner point temperature : ISA + 10 °C
PERFORMANCE
TAKEOFF
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A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
PRELIMINARY PAGES - TABLE OF CONTENTS
A330/A340 FLEET PER-TOF-PLP-TOC P 1/6
FCOM 19 AUG 10
PER-TOF-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/6
PER-TOF-THR THRUST OPTIONS
PER-TOF-THR-DRT DERATED TAKEOFF
DEFINITION OF DERATED TAKEOFF..............................................................................................................1/16
USE OF DERATED TAKEOFF.........................................................................................................................1/16
TAKEOFF PERFORMANCE IMPROVEMENT BY DERATING THE ENGINES................................................1/16
DETERMINATION OF THE MAXIMUM TAKEOFF WEIGHT AND ASSOCIATED SPEEDS.............................2/16
DETERMINATION OF DERATED TAKEOFF N1/EPR...................................................................................... 3/16
D04.................................................................................................................................................................... 5/16
D08.................................................................................................................................................................... 7/16
D12.................................................................................................................................................................... 9/16
D16.................................................................................................................................................................. 11/16
　
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