Session 2: One Engine Out Condition

Objective1: To give essential concepts of management of one engine out condition at take off and landing phases

Objective2: To give ideas of critical potential critical problem of the above condition

 

Explanation:

The teaching materials will utilized to give some examples of management and critical problem of one engine out condition in take off and landing problems

Material:

  • Multimedia black board  +  Power Point Like Software
  • Videos
  • Pictures

One Engine Out Conditions

Figure 12 One engine out condition

Main activities

  • By  pictures and (if possible) by videos will be explain the management and the critical problems in the event of one engine out in take off and landing phases.
  • Student will be asked to think about extreme situation for this event

Maximum duration:

30 minutes

Main question to be asked:

  • What is the most important airplane part concerning the capability of one engine out control?
  • What is the above event more critical for each airplane configuration?

Developing Activities

  • To explain that ice accretion could cause stall  problems,  loss of controllability,  engine flame out or even engine explosion, failure on flight instrumentations
  • To show to the students the different devices to face ice accretion 

Results of Activity

  • The force moment (about the Centre of Gravity) of the active propulsive force is balanced by the aerodynamic lateral force on the vertical tail due to rudder deflection
  • It is mandatory that the airplane maintains the runway direction in the take off or the landing phase

Contact coordinator

Dr. Corieri Patricia

von Karman Institute for Fluid Dynamics
Chaussée de Waterloo 72
BE 1640 Rhode-Saint-Genèse

Tel: +32 (0)2 359 96 55
Fax: +32 (0)2 359 96 00

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