What is the purpose of the tests required by 23.683 for flight control systems?

The tests required by 23.683 are intended to demonstrate that the control system operates in a satisfactory manner throughout the specified flight envelope and that the controls are not likely to jam, bind, or interfere in any way with the structure or other systems.

What must be demonstrated regarding the operation of the flight control system throughout the flight envelope?

It must be demonstrated that the control system operates in a satisfactory manner throughout the specified flight envelope and that the controls are not likely to jam, bind, or interfere in any way with the structure or other systems.

What is the intent of the requirements for control system stops under 23.675?

The intent is to ensure that the stops are arranged so that the control system cannot be damaged by the pilot's application of maximum force, and that the stops are not likely to be adversely affected by wear, slippage, or take-up of the control system.

What is the purpose of the requirements for trim systems under 23.677(a) and (b)?

The purpose is to ensure that the trim system is designed so that it cannot produce an unsafe condition, and that the trim control is readily accessible and operates in a natural sense.

What is the intent of the requirements for control system locks under 23.679(c)?

The intent is to ensure that the locking device cannot be inadvertently engaged or disengaged, and that it is not possible to engage the lock while the control is in a position that would cause an unsafe condition.

What is the purpose of the requirements for control system details under 23.685?

The purpose is to ensure that the design of the control system details is such that the system is reliable, and that the system is not likely to fail due to wear, corrosion, or other causes.

What is the intent of the requirements for spring devices under 23.687?

The intent is to ensure that the spring devices are designed so that they are not likely to fail due to fatigue, and that they are not likely to be adversely affected by the environment.

What is the purpose of the requirements for wing flap controls under 23.697?

The purpose is to ensure that the wing flap controls are designed so that they are not likely to be inadvertently operated, and that the flap position is indicated to the pilot.

What is the intent of the requirements for flap interconnection under 23.701?

The intent is to ensure that the flaps are interconnected so that they move in a synchronized manner, and that the interconnection is not likely to fail.

What is the purpose of the requirements for the automatic pilot system under 23.1329(b)?

The purpose is to ensure that the automatic pilot system is designed so that it cannot produce an unsafe condition, and that the system is not likely to be inadvertently engaged or disengaged.

What is the intent of the requirements for stability augmentation and automatic and power-operated systems under 23.672(b) and (c)?

The intent is to ensure that the stability augmentation and automatic and power-operated systems are designed so that they cannot produce an unsafe condition, and that the systems are not likely to fail in a manner that would cause loss of control.

What is the purpose of the requirements for primary flight controls under 23.673?

The purpose is to ensure that the primary flight controls are designed so that they are not likely to be inadvertently operated, and that the controls are not likely to jam, bind, or interfere in any way with the structure or other systems.

What is the intent of the requirements for installation under 23.655?

The intent is to ensure that the control system is installed so that it is not likely to be damaged by the pilot's application of maximum force, and that the system is not likely to be adversely affected by wear, slippage, or take-up of the control system.

What is the purpose of the requirements for control systems - general under 23.671(a)?

The purpose is to ensure that the control system is designed so that it is not likely to fail due to wear, corrosion, or other causes, and that the system is not likely to be adversely affected by the environment.

AMC2 23.2300 Flight control systems

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AMC2 23.2300 Flight control systems

ED Decision 2017/025/R

CS-23 Amdt 4

23.655 Installation

23.671(a) Control systems - General

23.672(b), (c) Stability augmentation and automatic and power-operated systems

23.673 Primary flight controls

23.675 Stops

23.677(a), (b) Trim systems

23.679(c) Control system locks

23.683 Operation tests

23.685 Control system details

23.687 Spring devices

23.697 Wing flap controls

23.701 Flap interconnection

23.1329(b) Automatic Pilot System

Details

Source-Title: AMC2 23.2300 Flight control systems View latest amendments

Erulesid: ERULES-1963177438-7003 Compare versions

Domain: Initial airworthiness

Amendedby: CS Issue 1

Applicabilitydate: 21 December, 2017

Entryintoforcedate: 21 December, 2017

Regulatorysource: ED Decision 2017/025/R Navigate

Regulatorysubject: CS-23

Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)

Parentir: CS 23.2300 Flight control systems

Origin: EASA

Category: EAR