
Aircraft Modification and Repair
Introduction
The responsibility for determining whether a repair is major or minor rests with: CAA Determination Major / Minor It is the installer’s responsibility to determine whether an installation is minor or major. CAA Determination Major / Minor Must be performed by CAA Approved Design Organisation. (Part 21)Due to their inherent criticality, all changes to the design of an aircraft are required to be approved. In particular to assess the STC for Continuing Airworthiness implications Under the CAA regulatory system there are a number of methods to obtain approval for a major modification or repair to a type certified aircraft. A data approval issued by a Designated Engineering Representative which is usually issued on a CAA certification ** Note Part 21 issues with this statement. Acceptable data can be provided by a type certificate (TC ) / supplemental type certificate (STC ) holder or third-party operator.
Objectives
After Successfully completed this course the trainees will be able to:-
- Familiarize with the regulatory framework
- Define key terms and acronyms
- Understand industry-specific terminology
- Understand the joint certification process
- Familiarize with EASA and FAA regulations
- Understand the certification process
- Learn about approval procedures
- Understand CAA certification requirements
- Familiarize with CAA procedures
- Identify key considerations for CAA certification
- Understand regulatory requirements
- Understand Part 21 regulations for aircraft repairs
- Identify key considerations for repair design and approval
- Understand design principles for airworthiness
- Familiarize with regulatory requirements
- Understand the difference between minor and major modifications
- Learn about CAA procedures for modification approval
- Understand the role and purpose of Supplemental Type Certificates (STCs)
- Familiarize with STC application procedures
- Understand implementation procedures for certificates and modifications
- Learn about regulatory requirements
- Understand structural design principles
- Familiarize with crashworthiness considerations
- Understand structural integrity principles
- Learn about ageing aircraft considerations
- Structures and Systems – Safety Assessment CS25.1309
1. Understand safety assessment principles
2. Familiarize with CS25.1309 requirements
- Part 21 Subpart M – Repairs
1. Understand Part 21 Subpart M regulations for repairs
2. Learn about repair design and approval procedures
- Repair Evaluation Guidelines (REG) and Repair Assessment Programme (RAP)
1. Understand REG and RAP principles
2. Familiarize with application procedures
Who Sould Attend
- aircraft maintenance managers
Course Content
- Introduction
- Introduction Role & Purpose of an STC-Supplemental Type
- Certificates and Modifications Implementation-Structure General Introduction
- Crashworthiness Considerations-Structural Integrity & Ageing Aircraft Structures and Systems
- Safety Assessment CS25-1309Part 21 Subpart M
- Repairs-Repair Evaluation Guidelines (REG) and Repair Assessment Programme(RAP)
- Definitions and Acronyms
- The Beginning of EASA / FAA Joint Certification
- Certification and Approval Process
- The CAA Certification Process
- The CAA Certification Process Considerations
- Part 21 Aircraft Repair Considerations
- Design Aspects of Airworthiness
- CAA Modifications Minor & Major
Prerequisite
5 Years Experience in the field
Location
Cairo - EgyptCourse Code
U446Course Duration
10 DayAsk Qustion
Request at your location
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