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Date of the module
Table of contents
• Flight operations duties
• JAA and JAR OPS 1
• General aircraft limitations
• Payload Range
• Operating limitations
• In flight performance
• One engine inoperative performance
• Flight planning
A project supported by AIRBUS and the CAAC
Date of the module
1 - Principle
2 - Engine-out regulations
3 - ETOPS principle
4 - Obstacles to consider
5 - Engine-out limitations
6 - In flight procedure
Table of Contents
A project supported by AIRBUS and the CAAC
Date of the module
1 - Principle
2 - Engine-out regulations
3 - ETOPS principle
4 - Obstacles to consider
5 - Engine-out limitations
6 - In flight procedure
Table of Contents
A project supported by AIRBUS and the CAAC
Date of the module
V(L/Dmax)
Fa (all eng.) cruis.
Given
m, Zp, t°C
Cruise
speed
Thrust
Fa (1 eng.inop) cruis.
Fr
A project supported by AIRBUS and the CAAC
Date of the module
R/C<0
Given
m, Zp, t°C
Cruise
speed
Thrust
Speed
Fa (1 eng.inop) cruise
Fa(1eng inop) Maxi cont.
V(L/Dmax)
Fr
A project supported by AIRBUS and the CAAC
Date of the module
Engine
failure
A project supported by AIRBUS and the CAAC
Date of the module
R/C<0
m' < m
Given
m, Zp, t°C
Fa(1 eng.inop) Maxi cont.
Fa (1 eng.inop) cruis.
Thrust
Cruise Speed
V(L/Dmax) speed
Fr
A project supported by AIRBUS and the CAAC
Date of the module
1 - Principle
2 - Engine-out regulations
3 - ETOPS principle
4 - Obstacles to consider
5 - Engine-out limitations
6 - In flight procedure
Table of Contents
A project supported by AIRBUS and the CAAC
Date of the module
A B
D1 D2 D3
D4
D1, D2, D3, D4 suitable aerodromes
All aircraft
En route - one engine inoperative regulations (JAR OPS 1.500)
A project supported by AIRBUS and the CAAC
Date of the module
A B
A, B, C, adequate aerodromes
Twin engined aircraft
60 mn C
1 eng.inop.
ETOPS
Approval
En route - one engine inoperative regulations - ETOPS (JAR OPS
1.245)
A project supported by AIRBUS and the CAAC
Date of the module
Adequate aerodrome for ETOPS flight (IEM OPS 1.220)
The aerodrome is satisfactory taking in account
the performance requirements and runway
characteristics
The aerodrome is available and equipped with
necessary ancillary services
At least one letdown aid for instrument
approach is available (ground radar would so
qualify)
An ATC facility is available
A project supported by AIRBUS and the CAAC
Date of the module
Maximum distance from an adequat airport (JAR OPS
1.245)
Based on one engine inoperative TAS
ISA
FL = Gross ceiling (maxi FL 170)
Thrust MCT
aircraft weight (see after)
A project supported by AIRBUS and the CAAC
Date of the module
Maximum distance to an adequate airport (JAR OPS
1.245)
Reference weight
tow = RTOW
(sea level)
optimum Altitude
« Long Range »
MLR
1 h
Reference weight
A project supported by AIRBUS and the CAAC
Date of the module
60 minutes
A project supported by AIRBUS and the CAAC
Date of the module
NBO
JIB
SLL
KHI
BOM
CMB
A project supported by AIRBUS and the CAAC
Date of the module
NBO
JIB
SLL
KHI
BOM
CMB
ETOPS
Flight
A project supported by AIRBUS and the CAAC
Date of the module
A B
90 mn C
All eng.
Three or four engined aircraft
2 engines
inop.
A, B, C, suitable aerodromes
En route - two engines inoperative regulations (JAR OPS 1.505)
A project supported by AIRBUS and the CAAC
Date of the module
Suitable aerodrome
It is adequate
Weather reports and forecast indicating that
the weather conditions are above the planning
minimas
Reports indicating that the landing will be safe
A project supported by AIRBUS and the CAAC
Date of the module
1 - Principle
2 - Engine-out regulations
3 - ETOPS principle
4 - Obstacles to consider
5 - Engine-out limitations
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flight operation 飛行運行概述(44)