Airframe. ATPL Preparation Certificate 021 - ENAC
Airframe. ATPL Preparation Certificate 021 - ENAC
Airframe. ATPL Preparation Certificate 021 - ENAC
Airframe. ATPL Preparation Certificate 021 - ENAC

Airframe. ATPL Preparation Certificate 021 - ENAC


This book is aimed at future pilots willing to study Airframe (021) within the framework of ATPL Theoretical Certificates. It complies with EASA's Learning Objectives for the 021 Certificate. The chapters are all illustrated to facilitate the reader's comprehension. At the end of each chapter, the reader will find key-points highlighting the most important notions. 
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ISBN : 9782364931152
Référence : 1115
Année de parution : 2014
This book is aimed at future pilots willing to study Airframe (021) within the framework of ATPL Theoretical Certificates. It complies with EASA's Learning Objectives for the 021 Certificate. The chapters are all illustrated to facilitate the reader's comprehension. At the end of each chapter, the reader will find key-points highlighting the most important notions. 
 
Laurence Morin is engineer and head of pilot theoretical training at the ENAC. She teaches Airframe, Systems and Electricity to future pilots and engineers at the ENAC. 
 
Mélanie O'Quigley is a former student pilot of the ENAC.

SUMMARY 

INTRODUCTION

 

1STPART:AIRFRAME STRENGTH

 

CHAPTER1:BASICPRINCIPLESOFMECHANICSOFMATERIALS

 

CHAPTER 2: DESIGN METHODS

 

CHAPTER 3: STRUCTURAL MAINTENANCE

 

CHAPTER 4: AERONAUTICAL MATERIALS

 

CHAPTER 5: BASIC NOTIONS OF AEROELASTICITY 

 

 

2ND PART: AIRFRAME

 

CHAPTER 1: WINGS (ATA 57)

 

CHAPTER 2: FUSELAGE (ATA 53)

 

CHAPTER 3: STABILIZERS (ATA 55) AND CONTROL SURFACES

 

CHAPTER 4: PRIMARY FLIGHT CONTROL SYSTEM (ATA 27)

 

CHAPTER 5: SECONDARY FLIGHT CONTROL SYSTEM (ATA 27)

 

CHAPTER 6: LANDING GEAR (ATA 32)

 

CHAPTER 7: TIRES WHEELS - BRAKES (ATA 32)
AIRCRAFT TIRES

 

 

 

 

APPENDIX 1: Methods of inspection for structural parts

 

APPENDIX 2 : Standardized designation of light alloys

 

APPENDIX 3: ATA 100 STANDARD (NON-EXHAUSTIVE)

 

This book is aimed at future pilots willing to study Airframe (021) within the framework of ATPL Theoretical Certificates. It complies with EASA's Learning Objectives for the 021 Certificate. The chapters are all illustrated to facilitate the reader's comprehension. At the end of each chapter, the reader will find key-points highlighting the most important notions. 
 
Laurence Morin is engineer and head of pilot theoretical training at the ENAC. She teaches Airframe, Systems and Electricity to future pilots and engineers at the ENAC. 
 
Mélanie O'Quigley is a former student pilot of the ENAC.

SUMMARY 

INTRODUCTION

 

1STPART:AIRFRAME STRENGTH

 

CHAPTER1:BASICPRINCIPLESOFMECHANICSOFMATERIALS

 

CHAPTER 2: DESIGN METHODS

 

CHAPTER 3: STRUCTURAL MAINTENANCE

 

CHAPTER 4: AERONAUTICAL MATERIALS

 

CHAPTER 5: BASIC NOTIONS OF AEROELASTICITY 

 

 

2ND PART: AIRFRAME

 

CHAPTER 1: WINGS (ATA 57)

 

CHAPTER 2: FUSELAGE (ATA 53)

 

CHAPTER 3: STABILIZERS (ATA 55) AND CONTROL SURFACES

 

CHAPTER 4: PRIMARY FLIGHT CONTROL SYSTEM (ATA 27)

 

CHAPTER 5: SECONDARY FLIGHT CONTROL SYSTEM (ATA 27)

 

CHAPTER 6: LANDING GEAR (ATA 32)

 

CHAPTER 7: TIRES WHEELS - BRAKES (ATA 32)
AIRCRAFT TIRES

 

 

 

 

APPENDIX 1: Methods of inspection for structural parts

 

APPENDIX 2 : Standardized designation of light alloys

 

APPENDIX 3: ATA 100 STANDARD (NON-EXHAUSTIVE)

 

Référence : 1115
Nombre de pages : 180
Format : 17x24
Reliure : Broché

 Table of CONTENTS

 

INTRODUCTION

 

1ST PART:AIRFRAME STRENGTH

 

CHAPTER1:BASICPRINCIPLESOFMECHANICSOFMATERIALS

 

1 Introduction–Mechanicsofmaterials

2 Forcesinvolved

   2.1 Deformationofasolidduetotheappliedforces

3 Stressesinsolids

   3.1 Highlightingthestresses

   3.2.Normalstressandshearstress

   3.3.Sizing–General

 

4 Stress-strainrelationshipexample:tension

   4.1 Fundamentalexperiment

5 Compressionandbuckling

   5.1 Platebuckling

6 Simpleshear

7 Bending

8 Torsion

9 Stressdistributioninthevariouselementsofasimplestructure

   9.1 Normalload

   9.2 Shearingload

   9.3 Bendingmoment

   9.4 Torsionalmoment

   9.5 Distributionofstressonstructuralelements

 

CHAPTER 2: DESIGN METHODS

 

1 Introduction

2 Rupture modes

   2.1 Static rupture

   2.2 Fatigue rupture

   2.3 Dynamic instability

   2.4 Rupture by cracking

   2.5 Parts exposed to high temperatures

3 Certification levels (Paragraph 1309)

   3.1 Failure types

   3.2 Probability of occurrence

   3.3 Conclusion

4 Load calculation – General

   4.1 Loads supported by the aircraft

   4.2 Load types (limit load, ultimate load, in-service load)

5 Static proof

6 Proof of fatigue strength and damage-tolerance

   6.1 1st step: Definition of fatigue loads

   6.2 2nd step: Proof3

7 Design types

   7.1 History

   7.2 Definition of concepts 

 

CHAPTER 3: STRUCTURAL MAINTENANCE

 

1 Introduction

2 The ATA 100 Standard

3 Maintenance modes

  3.1 Introduction

  3.2 Preventive maintenance

4 Issuing the maintenance program for a new aircraft

  4.1 Purpose and actors

  4.2 At the operator’s premises: scheduled maintenance

 

CHAPTER 4: AERONAUTICAL MATERIALS

1 Introduction

2 Main properties

   2.1 Chemical properties

   2.2 Physical properties

   2.3 Mechanical properties

   2.4 Environmental properties

   2.5 Implementation

   2.6 Economical properties

3 Material selection

1ST CATEGORY: METALLIC MATERIALS

4 Steel.

  4.1 Chemicals properties

  4.2 Physical properties

  4.3 Mechanical properties

  4.4 Environmental properties

  4.5 Implementation

  4.6 Economy

  4.7 Conclusion-use

5 Light alloys

  5.1 Chemicals properties

  5.2 Physical properties

  5.3 General properties

  5.4 Main light alloys used in airframes

6 Ultra-light alloys

  6.1 Chemicals properties

  6.2 Physical properties

  6.3 Mechanical properties

7 Titanium and titanium alloys

  7.1 Chemicals properties

  7.2 Physical properties

  7.3 Mechanical properties

2ND CATEGORY: COMPOSITE MATERIALS

8 General

   8.1 Definition

   8.2 Anisotropy and lay-up53

9 Constituents

   9.1 Fibers

   9.2 Matrixes.

10 Advantages and disadvantages of using composite materials

    10.1 Advantages

    10.2 Disadvantages

11 Sandwich materials

    11.1 Definition

    11.2 Properties 

 

CHAPTER 5: BASIC NOTIONS OF AEROELASTICITY

 

1 Static aeroelasticity : aileron reversal

1.1 What is it?

1.2 What happened?

1.3 Remedies

2 Dynamic aeroelasticity

2.1 Calculation of dynamic loads

2.2 Vibrations

2.3 Example of instability: flutter 

 

2ND PART: AIRFRAME 

 

CHAPTER 1: WINGS (ATA 57)

 

1 General

1.1 Wing position

1.2 Wing types

2 Applied loads

2.1 Nature

2.2 General stresses

3 Construction modes

3.1 Spars

3.2 Ribs

3.3 Skin and stringers

4 Stress PICK-UP in the box constituents

4.1 Reminder: Distribution of stresses in a simple structure

4.2 Application to the wing box

5 Special points

5.1 MZFW limitation

5.2 Tanks

 

CHAPTER 2: FUSELAGE (ATA 53)

 

1 The various types of fuselage

1.1 Introduction

1.2 The various types of fuselage

1.3 Pressurized areas

1.4 Different fuselage cross-sections

2 Applied loads

2.1 Nature

2.2 General loads

2.3 Abnormal operation fuselage loads

3 Construction modes

3.1 Frames

3.2 Skin and stringers

3.3 Assemblies

4 Load pick-up in fuselage cross-sections

5 Fuselage openings

5.1 Windshields

5.2 Passenger doors

5.3 Cargo compartment doors

6 Floor

7 Fire Protection

 

CHAPTER 3: STABILIZERS (ATA 55) AND CONTROL SURFACES

 

1 General

1.1 Tail units

1.2 Vertical section

1.3 Horizontal section

1.4 Arrangement of stabilizers

2 Applied loads

3 Control surfaces: General

3.1 Definition

3.2 Ground locking of control surfaces

4 Control surface defects

4.1 Adverse yaw

4.2 Aeroelasticity-related problems

5 Aerodynamic balance

5.1 Inset hinge

5.2 Internal balance

5.3 Tabs

6 Trimming of control surfaces

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Livres de l'auteur Laurence Morin

Livres de l'auteur Mélanie O'Quigley