IL.XIV.C.R6
Risk managementFactors and situations that could lead to loss of control with an inflight powerplant(s) failure.
From the FAA library
- Chapter 6: Flight Controls › Flight Control Systems › Primary Flight Controls
Flight Control Systems Flight Controls Aircraft flight control systems consist of primary and secondary systems. The ailerons, elevator (or stabilator), and rudder constitute the primary control system and are required to control an aircraft safely during flight. Wing flaps, leading ... edge devices, spoilers, and trim systems constitute the secondary control system and improve the performance characteristics of the airplane or relieve the pilot of excessive control forces. Primary Flight Controls Aircraft control systems are carefully designed to provide adequate responsiveness…
- Chapter 9: Techniques of Flight Instruction › Positive Exchange of Flight Controls › Procedure
Procedure During flight training, there should always be a clear understanding between learners and flight instructors about who has control of the aircraft. The preflight briefing should include procedures for the exchange of flight controls. A positive three-step process ... exchange of flight controls between pilots is a proven procedure and one that is strongly recommended. When an instructor is teaching a maneuver to a learner, the instructor normally demonstrates the maneuver first, then has the learner follow along…
- Chapter 6: Flight Controls
addition, in some large and fast aircraft, controls are boosted by hydraulically or electrically actuated systems. In both the fly-by-wire and boosted controls, the feel of the control reaction is fed back to the pilot by simulated means ... Current research at the National Aeronautics and Space Administration (NASA) Dryden Flight Research Center involves Intelligent Flight Control Systems (IFCS). The goal of this project is to develop an adaptive neural network-based flight control system. Applied directly to flight…
- Chapter 5: Aerodynamics of Flight › Axes of an Aircraft
right movement of the aircraft’s nose. The three motions of the conventional airplane (roll, pitch, and yaw) are controlled by three control surfaces. Roll is controlled by the ailerons; pitch is controlled by the elevators; yaw is controlled ... rudder. The use of these controls is explained in Chapter 6, Flight Controls. Other types of aircraft may utilize different methods of controlling the movements about the various axes. For example, weight-shift control aircraft control two axes (roll…
- Chapter 3: Identifying Hazards & Associated Risks › Leading Accident Causes
Other The top four causes of general aviation fatal accidents include loss of control in-flight (LOC-I), controlled flight into terrain (CFIT), system component failure of the powerplant (SCF-PP), and fuel-related issues. These causes often signify ... thread. To begin with, pilots should recognize hazards linked to causes of aircraft accidents as presented below: 11806 1. Loss of Control In-flight (LOC-I)–Examples of loss of control scenarios include continued VFR into IMC, wake turbulence upsets…
- CHAPTER 2. REDUCING GENERAL AVIATION ACCIDENTS › 2.2 Manual Flight After Automation Failure › 2.2.3 Proficiency in Manual Aircraft Control
Proficiency in Manual Aircraft Control. Pilots should be proficient in manual aircraft control and should be able to operate the aircraft without the use of the aircraft’s automation. Advanced avionics and flight automation offer many levels of automation. Pilots ... need to understand that no one level of automation is appropriate for all flight situations. If a flight automation system failure occurs, in whole or in part, the pilot should possess the knowledge to address the situation. This may include…