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flown clear of cloud and in sight of the ground or water at not less than the
altitude and with not less than the flight visibility for circling.
Compliance with Visual Circling procedures, as laid down in relevant
documentation, is mandatory when accomplishing this manoeuvre.
A minimum altitude of 1,000ft above the landing threshold is maintained until
intercept of a 3º visual approach path.
Note: At night, descent below the circling MDA is permitted only when
intercepting a 3º visual approach path.
During a Circling Approach, at or prior to the MAP, inside the circling area
with the required visual reference established, the PF will announce “Circling”.
During circling, both pilots shall be Head Free.
Once “Circling” is nominated, the PNF should continue with monitoring
applicable to the circling manoeuvre. Any remaining Instrument Procedure calls
are cancelled. Only Standard Approach calls need be made.
During Circling Approaches, it is accepted that under some circumstances, a
change of control while circling may be required due to airport or environment
limitations. This is only permitted when the Captain has to be the landing pilot
(such as when First Officer crosswind limits are exceeded) and where circling
restrictions exist that make it more practical for the First Officer to fly the
circling approach.
Due to the specific altitude and tracking restrictions associated with circling
approaches, Visual Procedures are not to be nominated while circling.
A Circling Approach will be flown as a visual flight manoeuvre. It is used when
an instrument approach is completed, to align the aircraft with the landing
runway. When an Instrument Approach Procedure specifies a visual segment
“LIMITS” (JUN 08) – NOT AN OFFICIAL DOCUMENT
PAGE 2
from the point where the MDA is reached to the circling area of the airport of
intended landing, a Missed Approach shall be executed unless the visual
segment can be flown clear of cloud and in sight of the ground or water at not
less than the altitude and with not less than the flight visibility for circling.
Compliance with Visual Circling procedures, as laid down in relevant
documentation, is mandatory when accomplishing this manoeuvre.
AEROPLANE LIMITATIONS
All variants, as listed.
Certification
Public transport category (passengers and freight)
- Day and night operations
- VFR and IFR
- Extended over water
- Icing conditions
Maximum Number of Seats
375 (-200)
440 (-300)
Weight Limitations
(201 EBA-EBD)
Maximum Taxi Weight 202,900 kg
Maximum Takeoff Weight 202,000 kg
(at brakes release)
Maximum Landing Weight 180,000 kg
Maximum Zero Fuel Weight 168,000 kg
Minimum Weight 116,000 kg
(203 EBG)
Maximum Taxi Weight 233,900 kg
Maximum Takeoff Weight 233,000 kg
(at brakes release)
Maximum Landing Weight 182,000 kg 
Maximum Zero Fuel Weight 170,000 kg 
Minimum Weight 116,000kg
(203 EBH-EBI)
Maximum Taxi Weight 233,900 kg
Maximum Takeoff Weight 233,000 kg
(at brakes release)
Maximum Landing Weight 180,000 kg
Maximum Zero Fuel Weight 168,000 kg
(203 EBJ-EBK)
Maximum Taxi Weight 202,900 kg *
Maximum Takeoff Weight 202,000 kg *
(at brakes release)
Maximum Landing Weight 182,000 kg 
Maximum Zero Fuel Weight 170,000 kg 
* QF operational applied limits due domestic traffic charges containment
(these a/c in the domestic config)
(301)
Maximum Taxi Weight 233,900 kg
Maximum Takeoff Weight 233,000 kg
(at brakes release)
Maximum Landing Weight 187,000 kg
Maximum Zero Fuel Weight 175,000 kg
Minimum Weight 121,000 kg
Note: In exceptional circumstances (in-flight turnback or diversion) an
immediate landing above the maximum landing weight is permitted,
provided the pilot follows the overweight landing procedure.
Flight Manoeuvring Load Acceleration Limits
Clean configuration -1g to +2.5g (normal law)
Slats extended 0g to +2g (normal law)
Minimum Flight Crew Component 2 pilots
Maximum Aircraft Altitude 41,450'
Environmental Operating Envelope
0' 55 C
Up to 16,600' ISA+40 deg C
From 16,600 to 41,000' ISA+35 deg C
Lower temperature limits apply (below -54 deg C and proportional to
altitude)(See chart in limitations section)
Airport Operations
Runway slope (mean) ±2%
Runway altitude 12,500'
Wind Limitations
Maximum demonstrated crosswind - 32 kt with gusts up to 40 kt (dry or
damp runway)
Maximum tailwind 15 kt (manual landing)
　
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