032-04 PERFORMANCE CLASS A - AEROPLANES CERTIFICATED UNDER ONLY CS 25

032-04 PERFORMANCE CLASS A - AEROPLANES CERTIFICATED UNDER ONLY CS 25

About this course

Course Information

In this chapter, we will examine the class A aeroplane which is certified under CS 25. The category of Class A includes all multi-engine jet aeroplanes and multi-engine turboprop aeroplanes which have 10 or more passenger seats or a max take-off mass more than 5700 kg. The general performance requirements and factors mentioned in the second chapter are applicable to class A aeroplane, however the requirements and safety factors are improved for this class of aeroplane because they have more carriage capacity and they are operating on a longer range with a higher speed. Courses are constantly monitored and updated when major changes in authority documentation is released.

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Course Information

Course
032-04 PERFORMANCE CLASS A - AEROPLANES CERTIFICATED UNDER ONLY CS 25
Exam
Not included
Course Duration
1:13:23
Slides
95
Tags

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Content of the Course

COURSE START
TAKE – OFF
Forces Acting On Aeroplane During Take-Off
DEFINITIONS OF TERMS USED
Minimum Control Speed With Critical Engine Inoperative, VMC
Take-Off Distances
Accelerate-Stop Distance
THE EFFECT OF RUNWAY SLOPE ON THE ACCELERATE-STOP DISTANCE
Balanced Field Length Concept
Unbalanced Field Length Concept
Runway Length Limited Takeoff Mass (RLTOM)
Take-Off Climb
Obstacle-Limited Take-Off
Performance Limited Take-Off Mass
Takeoff Performance On Wet And Contaminated Runways
Use Of Reduced And Derated Thrust
Takeoff Performance Using Different Take-Off Flap Settings
Takeoff Performance Using Increased V2 Speeds (Improved Climb Performance)
Brake Energy And Tyre Speed Limit
Use Of Aeroplane Flight Data
CLIMB - CLIMB TECHNIQUES
Influence Of Variables On Climb Performance
Use Of Aeroplane Flight Data
CRUISE - CRUISE TECHNIQUES
Max Endurance
Max Range
Long Range Cruise
Influence Of Variables On Cruise Performance
Cruise Altitudes
Cost Index
EN-ROUTE ONE ENGINE INOPERATIVE -DRIFT DOWN
Influence Of Variables On En-Route One Engine Inoperative Performance
Use Of Aeroplane Flight Data
DESCENT - DESCENT TECHNIQUES
Influence Of Variables On Descent Performance
APPROACH AND LANDING
Approach Requirements
Influence Of Variables On Landing Performance
Quick Turnaround Limit
Use Of Aeroplane Flight Data
Example
COURSE END