曝光臺 注意防騙
網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者
(still air, ISA)
or max time
diversion
Area for take off alternate
A project supported by AIRBUS and the CAAC
Date of the module
Three and four engined aircraft
DEPARTURE
120 mn at OEI
cruise speed
(still air, ISA)
Area for take off alternate
A project supported by AIRBUS and the CAAC
Date of the module
Determination of OEI cruise speed
For all type of aircraft, the OEI cruise speed is based on the
TOW according to the AFM performance.
When AFM doesn’t contain this speed, the speed used is the
achieved speed with the maximum continuous thrust set up on the
remaining engine.
A project supported by AIRBUS and the CAAC
Date of the module
Destination alternate requirements
Two alternates must be selected when:
the meteorological conditions are below the
applicable planning minimas 1 hour before until 1
hour after the ETA
no meteorological information are available
A project supported by AIRBUS and the CAAC
Date of the module
1 - Selection of aerodromes
2 - Planning minima for IFR flights (JAR OPS 1.297)
Table of Contents
A project supported by AIRBUS and the CAAC
Date of the module
Take off alternate
1 hour before until 1 hour after ETA
the meteorological conditions are above the
operating minimas
For a non-precision or circling approach, the ceiling
must be taken in account
A project supported by AIRBUS and the CAAC
Date of the module
Destination
1 hour before until 1 hour after ETA
the meteorological conditions are above the
following operating minimas:
– RVR/Visibility
– For a non-precision or circling approach, the ceiling at
or above MDH
A project supported by AIRBUS and the CAAC
Date of the module
Destination and en route alternate
1 hour before until 1 hour after ETA
the meteorological conditions are above the
operating minimas in accordance with the table of
the next page.
A project supported by AIRBUS and the CAAC
Date of the module
A project supported by AIRBUS and the CAAC
Date of the module
ETOPS en route alternate
1 hour before until 1 hour after ETA
the meteorological conditions are above the
operating minimas in accordance with the table of
the next page
A project supported by AIRBUS and the CAAC
Date of the module
Date of the module
A project supported by AIRBUS and the CAAC
Maximum weight check
A project supported by AIRBUS and the CAAC
Date of the module
Maximum weights check - Payload Calculation
Comparison point = Brake release
A project supported by AIRBUS and the CAAC
Date of the module
Comparison point = Brake release
Maximum allowed take-off weight is the lowest of
:
Maximum weights check - Payload Calculation
A project supported by AIRBUS and the CAAC
Date of the module
Comparison point = Brake release
Maximum allowed take-off weight is the lowest of
:
Maximum take-off weight
Maximum weights check - Payload Calculation
A project supported by AIRBUS and the CAAC
Date of the module
Comparison point = Brake release
Maximum allowed take-off weight is the lowest of
:
Maximum take-off weight
Maximum landing weight + trip fuel
Maximum weights check - Payload Calculation
A project supported by AIRBUS and the CAAC
Date of the module
Comparison point = Brake release
Maximum allowed take-off weight is the lowest of
:
Maximum take-off weight
Maximum landing weight + trip fuel
Maximum zero fuel weight + take-off fuel
Maximum weights check - Payload Calculation
A project supported by AIRBUS and the CAAC
Date of the module
Max allowed take-off weight
=
Maximum weights check - Payload Calculation
A project supported by AIRBUS and the CAAC
Date of the module
Max allowed take-off weight
=
Operating weight + Payload
Maximum weights check - Payload Calculation
A project supported by AIRBUS and the CAAC
Date of the module
Max allowed take-off weight
=
Operating weight + Payload
= dry operating weight + take-off fuel
Maximum weights check - Payload Calculation
A project supported by AIRBUS and the CAAC
Date of the module
PAYLOAD
=
Maximum weights check - Payload Calculation
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flight operation 飛行運行概述(18)
