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Introduction to Aircraft Interiors Interace Loads and Stress analysis and Certification. (One day course)

The Aircraft Interior Courses:

Aircraft interiors such as Stowage units, Galleys and Flight Crew Rest Compartments (FCRCs) require structural certification for airworthiness. The certification procedure of aircraft interiors includes the major structural documents of;

  • The Interface Loads report
  • The Stress Analysis report
The courses offered include the following:
  • Stowage Unit
    • Determination of Interface Loads and Typical Report structure
    • Stress Analysis of Stowage Unit and typical Report Structure
  • Flight Crew Rest Compartment (FCRC)
    • Model Construction of FCRC
    • Determination of Interface Loads and Typical Report structure
    • Stress Analysis of FCRC and typical Report Structure
  • Galley Structures
    • Model Construction of Galley Structures
    • Determination of Interface Loads and Typical Report structure
    • Stress Analysis of Galley Structures and typical Report Structure
Galley Units

All reports should be detailed, logical and comprehensive enough to provide convincing high quality analytical methodology and data to enable the ever diligent document checking authority to approve the submitted documents with little question. For example, the one day seminar on Stowage unit Interface Load report reveals a progressive methodology, associated FEA and mathematical analysis. FEA model build and quality checks, contents weight, location and centre of gravity determination and analytical confirmation. Body loading and internal contents loading technique, leading to the method of obtaining the all important Interface loads. This presentation should cover most aspects necessary to produce a detailed and confident document.

Internal Loads

Internal Loading (Generic)

9:00Introduction and Refreshments
9:30The Report structure
10:00Materials and joints
11:00Typical Stowage structure
13:15Stowage loading technique
14:00Mass cehck procedure
15:30FEA Stowaage modelling
16:00Interface Loads
14:30Quality control
16:45Course Review and Close

Who should Attend

The seminar is suitable for stress or Certification Engineers, Technical managers and Consultants with little or no experience on producing structural certification documents, in particular if they are experiencing difficulty in obtaining acceptance of the submitted reports

Seminar Leader:

Dr. Warren Leigh has worked on over seven different types of aircraft during his career from the;
  • BAe 146, (1984)
  • Shorts SD360 (1986)
  • T45-Goshawk
  • A320, A330, A340 to the A380 and Boeing 777
  • This includes Aircraft Galleys, Stowage Units and Flight Crew Rest Compartments (FCRC). The composite Crew rest bed on the A380 he designed and is the believed to be the world’s lightest weight at 12kgs. Since 2000 he has worked for British-based aircraft interior companies. He has produced Interface Load and Stress reports for airlines that include Afriqiyah Airways, Air Namibia, Britannia Airways, Cathay Pacific, China Eastern Airlines, Etihad Airways, GECAS, Iberia, Sichuan Airlines, South African Airways, Thai Airways, Thomson and Turkish Airlines.

    He has held meetings with the Certification approval consultancy in their offices Hamburg, Germany to appreciate and implement their strict vetting and high quality requirements for the approval of submitted Certification documents. Dr. Leigh has 40 years engineering experience.


    £450 per person including VAT (Refreshments and lunch included).
    Substitutions may be made at any time. Bookings cancelled less than 14 days prior to the event will be charged in full.

    Payment details.

    BACS Payment. (please enclose a copy of the draft)
    Bank transfers (BACS) can be made to:
    Barclays Bank Plc, 1 Bridge Street, Stockport, SK1 1XU, UK
    IBAN: GB29 BARC 20821463869482

    Enclose a cheque/purchase order £450.
    Make payments to:
    Jura Carbon Ltd,
    1 Coniston Road, High Lane,
    Stockport, SK6 8AW,
    United Kingdom

    Download the brochure and booking form

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