Chapter 13: Transition to Multiengine Airplanes Airplane Flying Handbook (FAA-H-8083-3C) Audiobook

Chapter 13: Transition to Multiengine Airplanes Airplane Flying Handbook (FAA-H-8083-3C) Audiobook New 2021
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00:00:00 Introduction
00:01:39 General
00:02:11 Terms and Definitions
00:09:11 Operation of Systems
00:30:18 Performance and Limitations
00:36:20 Weight and Balance
00:44:13 Ground Operation
00:45:23 Normal and Crosswind Takeoff and Climb
00:54:08 Short-Field Takeoff and Climb
00:55:55 Rejected Takeoff
00:56:46 Level Off and Cruise
00:59:01 Spin Awareness and Stalls
01:12:41 Crosswind Approach and Landing
01:14:51 Short-Field Approach and Landing
01:16:50 Go-Around
01:19:16 Engine Inoperative Flight Principles
01:38:23 Low Altitude Engine Failure Scenarios
01:48:00 Engine Failure During Flight
01:51:13 Engine Inoperative Approach and Landing
01:54:28 Multiengine Training Considerations
02:02:49 Chapter Summary

Chapter Summary.
Small multiengine airplanes handle much like single-engine airplanes as long as both engines are functioning normally.
A competent multiengine pilot, however, acquires the additional knowledge, risk mitigation strategies, and practical skills required to fly a multiengine airplane in case a loss of thrust from one engine actually occurs.
In that case, the pilot will be able to take appropriate action leading to a safe outcome.
Much of this chapter discussed loss of directional control.
How to obtain the best performance with an inoperative engine was also described in detail.
These two considerations correspond to the red radial line (VMC) and the blue radial line (VYSE) on the airspeed indicator.
The actions a pilot takes when dealing with stalls, VMC, or best performance vary greatly.
Understanding these concepts, knowing how to mitigate the risks, and possessing the skills to handle an engine failure in a variety of situations, allows a pilot to enjoy the increased performance and safety provided when flying a multiengine airplane.

Introduction.
This chapter is devoted to the factors associated with the operation of small multiengine airplanes.
For the purpose of this handbook, a “small” multiengine airplane is a reciprocating or turbopropeller-powered airplane with a maximum certificated takeoff weight of 12,500 pounds or less.
This discussion assumes a conventional design with two engines—one mounted on each wing.
Reciprocating engines are assumed unless otherwise noted.
The term “light-twin,” although not formally defined in the regulations, is used herein as a small multiengine airplane with a maximum certificated takeoff weight of 6,000 pounds or less.
There are several unique characteristics of multiengine airplanes that make them worthy of a separate class rating.
The one engine inoperative (OEI) flight information presented in this chapter emphasizes the significant difference between flying a multiengine and a single-engine airplane.
However, all pilots need appropriate knowledge, risk management strategies, and skills to fly safely in any airplane they fly, and mastery of OEI flight is only one aspect of safe multiengine flying.
The modern, well-equipped multiengine airplane can be remarkably capable under many circumstances, but, the performance and system redundancy of a multiengine airplane only increase safety if the pilot is trained and proficient.
The airplane manufacturer is the final authority on the operation of a particular make and model airplane.
Flight instructors and learners should use the Federal Aviation Administration’s Approved Flight Manual (AFM) and/or the Pilot’s Operating Handbook (POH).
The airplane manufacturer’s guidance and procedures take precedence over any general recommendations made in this handbook.
General.
Multiengine and single-engine airplanes operate differently during an engine failure.
In a multiengine airplane, loss of thrust from one engine affects both performance and control.
The most obvious problem is the loss of 50 percent of power, which reduces climb performance 80 to 90 percent.
In some cases after an engine failure, the ability to climb or maintain altitude in a light-twin may not exist.
After an engine failure, asymmetrical thrust also creates control issues for the pilot.
Attention to both these factors is crucial to safe OEI flight.