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IATA Aircraft Lease Guidance

Guidance Material for aircraft leasing

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Guidance Material and Best Practices for Aircraft Leases

Annex VI: Modifications Guidelines

Aircraft Model :

All models

Applicability : EASA and FAA environment

1. Introduction

During the lifetime of an aircraft, various modifications are implemented with the intention to change or

upgrade specific functions or systems of the aircraft. During a transfer of aircraft the Lessor often requires a

consolidated file showing compliance with the applicable regulations and the lease agreement of all

modifications performed. However, this does exclude modifications performed at component level. This annex

provides guidelines for the airline on how to create a modification compliance file. The term modification file

is commonly used to describe two separate files:

The EOs and SBs file

STCs

2. Regulatory Basis

2.1 EASA Procedures

EASA regulations applicable to modifications can be found Part M (M.A 304, 305, 708, 710) and Part 21. In

addition, EASA has published GM and AMC, which provide additional insights into the regulatory

requirements of the modification process.

EASA distinguishes between major and minor for any changes made to the type design of the aircraft. The

determination for major or minor modifications needs to be performed by an organization holding the EASA

design organization approval (DOA), or directly by EASA.

There are different levels of EASA DOA authorizations. For example, a basic DOA allows the holder to classify

major or minor modification, and approve minor modifications only. A TC/STC holder with an EASA DOA can

approve both major and minor modifications.

The process to determine if a change is major or minor is illustrated in Figure 10. The first criteria for the

selection of a major or minor modification is the appreciable effect on weight, balance, structural strength,

reliability, and operational characteristics of the aircraft. If the proposed modification has an impact on one of

these factors, the modification should be classified as major. If this is not the case a second step of

considerations needs to be taken in order to determine the classification of the modification. During this step,

the impact of the modification on the certification basis, Type Certificate, previous performed compliance

demonstration, and the need for reassessment of this compliance data is reviewed. Also, if the modification is

part of an AD, or introduces or affects a function where failure is catastrophic or hazardous, it will be

classified as major. The major classification for modifications linked to an AD may be re-classified as minor

96 4 th Edition 2017

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