Engineering Jobs for Engineering People   BDP
Register Now! Login to Your Account!

Fatigue & Damage Tolerance Engineer - Bristol

  1. Home
  2. Jobseeker Home
  3. Recruiter Home
  4. Job Search
  5. Urgent Jobs

  1. Job Sites
  2. Graduate Jobs
  3. Exhibitions
  4. Contact Us
  5. Refer a Friend
  6. Industry Links
  7. Bookmark Us


This vacancy is no longer available!

Please search our database for all current vacancies available by Clicking Here


Recruiter: Colbern Limited Colbern Limited
More
View all vacancies for this Recruiter
Job Reference: JEx-851861-1707-893 08
Date Advertised: 12 August 2008
Expiry Date: 26 September 2008
Duration of Employment: Permanent
Start Date: .
Location: Bristol
Salary / Hourly Rate: 26000-34000 Per Annum Salary guide range

Fatigue & Damage Tolerance Engineer
South West - Bristol, Avon
£26-34,000 salary guideline range

We are a specialist recruitment agency and we are currently looking for an experience Fatigue and Damage Tolerance Engineer for our Bristol based client.

We have a number of roles which we are currently recruiting for so please forward a copy of your CV to be kept advised of current and future opportuities.

Fatigue and Damage Tolerance Engineer

Experience working as an engineer, preferably in the aircraft industry, involved in fatigue and crack growth analysis of metallic structures using a broad range of standard hand and computer methods is desired.
An understanding of the fundamental method of analysis for fatigue and crack growth and an ability to develop these methods would be expected. Engineers would also be expected to have an ability to assess structural analysis problems.
Some knowledge of the application of FE analysis and an understanding of aircraft production methods and processes would be beneficial.
Experience of PC and mainframe computer systems would be expected.
A team player with a high regard for internal and external customers, whilst maintaining aircraft integrity as the over-riding principle is expected.


The job involves the analysis of aircraft structure using the standard fatigue and crack growth methods to develop design solutions within the project teams in Airbus UK.
The work will involve liaison with Static Stress, Design and appropriate departments to come up with optimum design solutions for the airline customer and to define maintenance programs.
The engineer will carry out fatigue, crack growth and residual strength calculations to assess design solutions using standard hand and computer methods.
The engineer will be expected to liaise with the Methods and Data group in order to ensure that methods, assumptions, data and procedures reflect on-going developments.


Go Back

This vacancy is no longer live.

Please search our database for all current vacancies available by Clicking Here


Not Registered Yet
Not Registered Yet?
Forgotten Your Password
Forgotten Your Password?
Experiencing Login Problems
Experiencing Login Problems?
Refer to a Friend
Refer to a Friend

Important Note:
There is no need to provide your bank account details when applying for a job. If you are asked for bank account details or see a vacancy requesting such please e-mail support@jobsgroup.net

Rate this Vacancy:

Salary:
Information:
Location:

© 2008 JobsGroup.net