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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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