Date
Hoofddorp (4-6 July 2012)

Introduction
This 3 day training course will provide a general overview how to certify new cabin interiors, e.g. executive interiors and changes and repairs to existing cabin interiors.
The content of the training course is based on the assumption that a so-called “green aircraft” exists with all necessary structural and systems interface provisions available in the cabin needed for the installation of the change.
It will address the relevant Subparts of Annex Part 21 as outlined in the detailed content of this training course. An overview of CS-23, CS-25, CS-27 and CS-29 paragraphs for the certification of cabin interiors for the different type of aircraft will be provided. This will be followed by a general explanation of the relevant CS-25 paragraphs including information regarding Appendix F testing, and Appendix H, Continued Airworthiness.
EASA Special Conditions applicable  to cabin interior design details will be presented in combination with actual design solutions.

The following subjects will be addressed:

• Introduction: Overview of the training course
• The legal and regulatory basis for the EASA Member States
• EASA
• Explanation of all relevant Annex Part 21 Subparts, e.g. Subpart A, Subpart D, Subpart E, Subpart K, Subpart M, Subpart O, Subpart P and Subpart Q
• Overview of all Cabin Safety Design applicable paragraphs in CS-23; CS-25; CS-27 and CS-29
• Explanation regarding the objectives of the applicable CS-25 paragraphs
• Examples of different design solution regarding executive cabin interiors.
• Example of interface loads, stress analysis and flammability testing for a galley
• Example of passenger seat testing
• Continued Airworthiness
• Discussion EASA Special Conditions

Learning Objectives
At the end of the training course the attendees should have the capability to classify changes to cabin interiors into minor, major or significant and prepare a draft certification programme, e.g. identification of the applicable certification requirements and proposed means of compliance with these requirements.

Target Group
Staff of airline design organizations, as well as staff of airworthiness authorities, in particular from third country aviation authorities who intend to implement or have already implemented national legislation based on Annex Part 21.

Prerequisites
Some knowledge regarding Annex Part 21 and the Certification Specifications is an advantage but not necessary.

Duration
3 days, starting at 9:00 and ending at 17:00.