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Core Upset Recovery Concepts for Jet Pilots

Course Summary

Training Aircfaft: N/A
Flight Training Hours: N/A
Ground Instruction Hours: 3.0 to 8.0
Duration: Self-Paced
Training Flights: N/A
Price: $299
Core Upset Recovery Concepts for Jet Pilots
What's Included: Access to the APS Core Upset Recovery Concepts for Professional Jet Pilots on-line computer-based training course, 44 Question Evaluation, Certificate of Completion endorsed by APS and CAE
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Web Delivery: Airplane Upset Recovery Training Aid – Revision 2

In the interest of safety and the desire to acknowledge the commonality in recovery techniques, the Airplane Upset Recovery Training Aid (URTA) was created as a reference guide to professional pilots. Aerodynamic principles applied to jet airplanes are similar among all manufacturers, and the recommended techniques for recovering from an upset in an airplane subject to these principles are also compatible. Pilots who understand the conditions of an upset, though such an event is unlikely, will be better prepared to recover from it.

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For Professional Aviators Course: Click Here

This Course Includes:

Causes of Airplane Upsets
  • Environmentally-Induced Airplane Upsets
  • Systems-Anomalies-Induced Airplane Upsets
  • Pilot-Induced Airplane Upsets
High Altitude Operations
  • Stability and Speed Divergence
  • Mechanics of Turning Flight
  • Flight at Extremely Low Airspeeds
  • Flight at Extremely High Speeds
Recovery From Airplane Upsets
  • Situational Awareness of an Airplane Upset
  • Use of Full Control Inputs
  • Counter-Intuitive Factors Upset Recovery Techniques
  • Stall
  • Nose-High, Wings-Level Recovery Techniques
  • Nose-Low, Wings-Level Recovery Techniques
  • High-Bank-Angle Recovery Techniques
  • Consolidated Summary of Airplane Recovery Techniques

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Control Surface Fundamentals
  • Spoiler-Type Devices
  • Lateral and Directional Aerodynamics
  • Angle of Sideslip
  • Wing Dihedral Effects
  • Pilot-Commanded Sideslip
Swept-Wing Aerodynamics
  • Flight Dynamics
  • Energy States
  • Load Factors
  • Angle of Attack and Stall
  • Aerodynamic Flight Envelope
  • Camber
  • Crossover Speed
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