Exams4Pilots Logo
 
Quick Links
Take a Practice Exam
Contribute to the Site
Browse the Exams
About this Site
Privacy Policy
Terms & Conditions
Site Map
New User
Log In
Examine My Cookies
Contact WebMaster
 
Exams4Pilots Forum
Forum Home
- Latest News
- Testimonials
- Tips & Tricks
- Stuck Mike
- Bug Reports
- Feature Request
 

 
SiteMap
You are here: home->amp->B02->B.8.1.5.0.A.1

8150
When the leading edge of a first stage turbine blade is found to have stress rupture cracks, which of the following should be suspected?
A) Faulty cooling shield.
B) Overtemperature condition.
C) Overspeed condition.

 

This site was made possible by:
Linux Logo Apache Logo Perl Logo
 
Validate me