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

Posted on by

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.

Content of the Course

Slide 95 Duration 1:13:23 Exam No
  • 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