SAE AIR 4938B-2017 Composite and Bonded Structure Technician Specialist Training Document.pdf
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1、 _ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising ther
2、efrom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2017 SAE International All rights reserved. No part of this
3、publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-49
4、70 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AIR4938B AEROSPACE INFORMATION REPORT AIR4938 REV. B Issued 1996-09 Revised 2017-06 Supersedin
5、g AIR4938A Composite and Bonded Structure Technician/Specialist Training Document RATIONALE This document is intended to outline the minimum training requirements deemed necessary for composite and/or metalbond technicians/specialists. TABLE OF CONTENTS 1. SCOPE 2 2. APPLICABLE DOCUMENTS 2 2.1 SAE P
6、ublications . 2 2.2 FAA and EASA Publications . 2 3. STUDENT PREREQUISITES . 3 4. EXAMINATIONS . 4 5. TEACHING LEVELS . 4 6. PART 1 - General Composite Structural Bonded Repair Curriculum . 5 6.1 Scope 5 6.2 Topics and Objectives . 6 7. PART 2 - Commercial Aircraft Composite Structure Bonded Repair
7、Curriculum . 17 7.1 Scope 17 7.2 Topics and Objectives . 17 8. PART 3 - Commercial Aircraft Composite Structure Bolted Repair Curriculum . 27 9. PART 4 - Commercial Aircraft Structure Metalbond Repair Curriculum . 28 9.1 Scope 28 9.2 Topics and Objectives . 29 10. NOTES 36 10.1 Revision Indicator 36
8、 SAE INTERNATIONAL AIR4938B Page 2 of 36 1. SCOPE This is a general curriculum that has been developed to identify the minimum knowledge and skill requirements of a composite and/or metal bond repair technician/specialist. This revision changes the document from an all-inclusive curriculum into a mo
9、dular set of curricula. Teaching levels have been assigned to the curriculum to define the knowledge, skills, and abilities graduates will need to make repairs to composite or metalbond structure. Minimum hours of instruction have been provided to ensure adequate coverage of all subject matter inclu
10、ding lecture and laboratory. These minimums may be exceeded and may include an increase in the total number of training hours and/or increases in the teaching levels. Each curriculum is a subpart of this document. Part 1 is the General Composite Structure Bonded Repair curriculum, independent of the
11、 application. Part 2 is the Commercial Aircraft Composite Structure Bonded Repair curriculum. Part 3 is the Commercial Aircraft Composite Structure Bolted Repair curriculum. (Under Development) Part 4 is the Commercial Aircraft Structure Metalbond Repair curriculum. This document contains ATA104 lev
12、el IV curricula. 2. APPLICABLE DOCUMENTS The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order. In the event o
13、f conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 2.1 SAE Publications Available from SAE International, 40
14、0 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AIR4844 Composites and Metal Bonding Glossary AIR5719 Teaching Points for an Awareness Class on “Critical Issues in Composite Maintenance and Repair“ AIR6291 Guid
15、elines for Repair Process Evaluation of Aluminum Bonded Structure ARP6262 Basic Composite Repair Technician Certification Standard 2.2 FAA and EASA Publications Available from Federal Aviation Administration, 800 Independence Avenue, SW, Washington, DC 20591, Tel: 866-835-5322, www.faa.gov and from
16、European Aviation Safety Agency, Ottoplatz, 1, D-50679 Cologne, Germany, Tel: +49 221 8999 000, www.easa.europa.eu. Title 14 Code of Federal Regulations, Part 147 EASA AMC 20-29 Composite Aircraft Structure FAA AC 20-107B Composite Aircraft Structure FAA AC 65-33 Development of Training/Qualificatio
17、n Programs for Composite Maintenance Technicians FAA AC 43-214 Repairs and Alterations to Composite and Bonded Aircraft Structure SAE INTERNATIONAL AIR4938B Page 3 of 36 3. STUDENT PREREQUISITES Part 1 - General Composite Structure Bonded Repair Student success will be in part based on the knowledge
18、 and skills possessed prior to course enrollment: Basic technical mathematics Reading comprehension Part 2 - Commercial Aircraft Composite Structure Bonded Repair and Part 4 - Commercial Aircraft Structure Metalbond Repair Student success will be in part based on the knowledge and skills possessed p
19、rior to course enrollment: Successful completion of Part 1 - General Composite Structure Bonded Repair Course or demonstrated mastery (bypass exam of Part 1) AND including the following disciplines: o Basic technical mathematics o Reading comprehension o Fundamentals of engineering and technical dra
20、wings o General shop and hand tool usage o Use of precision measurement tools o Basic physics o Basic chemistry o Aircraft health and safety regulatory awareness (need for PPE (Personal Protection Equipment) Part 3 - Commercial Aircraft Composite Structure Bolted Repair Student success will be in pa
21、rt based on the knowledge and skills possessed prior to course enrollment: Basic aircraft sheet metal skills o Knowledge of heat treatment o Proper forming and bending of aluminum alloys and titanium alloys Basic technical mathematics Reading comprehension Fundamentals of engineering and technical d
22、rawings General shop and hand tool usage Use of precision measurement tools Basic physics Basic chemistry Aircraft health and safety regulatory awareness (need for PPE (Personal Protection Equipment) SAE INTERNATIONAL AIR4938B Page 4 of 36 Basic technical mathematics, physics, and chemistry are cons
23、idered to be high school level courses. Evaluation of prior education can be accomplished by examination of school transcripts, by review of the training received through approved training providers, or by a pre-test. 4. EXAMINATIONS Training Providers will be required to monitor student performance
24、 throughout the program. Students will be administered a written exam following lecture classes and practical assessments in laboratory classes. The minimum passing grade for all written exams shall be 75% and all grades shall be recorded in the individuals training records. It is recommended to use
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