EASA CS-25.853: Material Test Criteria Interior Compartments Occupied by crew or passengers.
DURATION: HALF DAY
OVERVIEW
This course may be delivered in either an open or closed training format, and is intended to provide an interpretation of CS-25, Certification Specification & Acceptable Means of Compliance for those professionals involved Design Organization Approval (DOA Businesses), or Original Equipment Manufacturers (OEMS).
OBJECTIVES
The objective of the course is to equip the attendees with the basic knowledge of certification requirements for turbine powered large aeroplanes and how to demonstrate compliance with the relevant parts of the certification specification.
This course will not include a workshop examples, except for examples discussed in CS-25 Implementing Rules & AMCs.
COURSE CONTENT
- Average Burn Length, Flame Time, Drippings & Applicable Items
- Motion Picture Film
- Test Criteria & Procedures
- Seat Cushions – Criteria for Acceptance
WHO SHOULD ATTEND
Those organizations and personnel involved in design and production activities involving aircraft and products, parts & appliances fitted to aircraft that have a direct effect on continuing airworthiness.
This will include personnel from regulators, operators and maintainers under EASA Part 21 Subpart G & Subpart J Approvals. These personnel will be involved with the development and delivery of Aircraft or Component repairs & modifications, Service Information, Service Bulletin, Airworthiness Directive Development.
COURSE PRE-REQUISITES
Delegates should have a basic knowledge of Initial & Continuing Airworthiness principles involving Aircraft/Component Design, Compliance & validation techniques. A working knowledge of EASA Part 21.
If this is not the case, this must be advised in advance through the pre-course questionnaires.