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RPM
Applicable to: ,
N1 max.........................................................................................................................................99 %
Note: The N1 limit depends upon ambient conditions and engine airbleed configuration.
These may limit the N1 to a value lower than that given above (Refer to PER-THR-MTO
MAXIMUM TAKEOFF).
N2 max.................................................................................................................................... 103.3 %
N3 max....................................................................................................................................... 100 %
STARTER
Applicable to:
• 4 consecutive cycles, each of 2 min duration, maximum
• 20 s between cycles to allow for starter relubrication
• After 4 cycles, 15 min to allow starter to cool before attempting a new start or motoring.
• No running engagement of the starter when the N2 is above 20 %.
Note: High tailwinds (higher than 25 kt) may have an adverse effect on start. It may be necessary
to reposition the airplane into the wind.
STARTER
Applicable to: ,
Starter maximum ‐ continuous operation is 5 min .
‐ Two 3–minute duty cycles and a consecutive 1–minute cycle is permitted with run down to zero N3
between each cycle.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
POWER PLANT
A330/A340 FLEET LIM-70 P 4/6
FCOM 19 AUG 10
‐ After one continuous operation, or the three cycles wait 30 min to allow the starter to cool.
‐ No running engagement of the starter when the N3 is above 10 % on ground, or 30 % in flight.
REVERSE THRUST
Applicable to:
• Selection of reverse thrust in flight is prohibited
• Backing the aircraft with reverse thrust is not permitted.
• Maximum reverse should not be used below 60 kt (or when indication starts to fluctuate). Idle
reverse is allowed down to aircraft stop.
REVERSE THRUST
Applicable to: ,
• Selection of reverse thrust in flight is prohibited
• Backing the aircraft with reverse thrust is not permitted.
• Maximum reverse should not be used below 70 kt (or when indication starts to fluctuate). Idle
reverse is allowed down to aircraft stop.
REDUCED THRUST TAKEOFF
Applicable to:
Takeoff at reduced thrust is only permissible if the airplane ‐ meets all applicable performance
requirements at the planned takeoff weight, with the operating engines at the thrust available for
the assumed temperature.
‐ Thrust reduction must not exceed 25 % of the full rated takeoff thrust. To meet this requirement,
the flexible temperature must not be higher than ISA +40 °C (T MAX FLEX).
‐ The assumed temperature must not be lower than the flat rating temperature, or the actual OAT.
‐ Takeoff reduced thrust is not permitted on contaminated runways.
‐ Takeoff at reduced thrust is only allowed with any inoperative item affecting the performance, if the
associated performance shortfall has been applied to meet all performance requirements at the
takeoff weight, with the operating engines at the thrust available for the flex temperature.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
POWER PLANT
A330/A340 FLEET LIM-70 P 5/6
FCOM 19 AUG 10
REDUCED THRUST TAKEOFF
Applicable to: ,
‐ Takeoff at reduced thrust is only permissible if the airplane meets all applicable performance
requirements at the planned takeoff weight, with the operating engines at the thrust available for
the assumed temperature.
‐ Thrust reduction must not exceed 25 % of the full rated takeoff thrust. To meet this requirement,
the flexible temperature must not be higher than ISA +48 °C (T MAX FLEX).
‐ The assumed temperature must not be lower than the flat rating temperature, or the actual OAT.
‐ Takeoff reduced thrust is not permitted on contaminated runways.
‐ Takeoff at reduced thrust is only allowed with any inoperative item affecting the performance, if the
associated performance shortfall has been applied to meet all performance requirements at the
takeoff weight, with the operating engines at the thrust available for the flex temperature.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
POWER PLANT
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A330/A340 FLEET LIM-70 P 6/6
FCOM 19 AUG 10
LIMITATIONS
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A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
PRELIMINARY PAGES
TABLE OF CONTENTS
A330/A340 FLEET LIM-PLP-TOC P 1/2
FCOM 19 AUG 10
LIM-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
　
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