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 1.4% for a three engined aircraft
 1.6% for a four engined aircraft
 2 engines inoperative
 0.3% for a three engined aircraft
 0.5% for a four engined aircraft
Engine-out limitations (JAR OPS 1.500 et 1.505)
A project supported by AIRBUS and the CAAC
Date of the module
1000ft
A
tow<= mmaxiA + TF burn off
Gross
flight path
net
flight path
P
Level flight clearance rule 1 engine inoperative
Engine-out limitations “DRIFT DOWN” (JAR OPS 1.500 et 1.505)
A project supported by AIRBUS and the CAAC
Date of the module
DIVERSION
1500ft
P
tow <= mmaxiP + TF burn off
2000ft
Gross
flight path
net
flight path
Descent clearance rule 1 or 2 engines inoperative
P
Engine-out limitations “DRIFT DOWN” (JAR OPS 1.500 et 1.505)
A project supported by AIRBUS and the CAAC
Date of the module
FL mini
incertitude
2000ft 2000ft
Given
m, t°C
P
En route limitation calculation
A project supported by AIRBUS and the CAAC
Date of the module
FL mini
incertitude
2000ft 2000ft
Given
m, t°C
m’ > m P
En route limitation calculation
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
 With obstacles
flight path
Engine
failure
- Maxi continuous
thrust
- Drift down speed
Climbing cruise
In flight procedure
A project supported by AIRBUS and the CAAC
Date of the module
 Without obstacle
flight path
Engine
failure
-Normal descent
-Steady cruise
level after descent
In flight procedure

　
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