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.8.1.9.3.A.1
8193
The non-rotating axial-flow compressor airfoils in an aircraft gas turbine engine, are called
A) bleed vanes.
B) stator vanes.
C) pressurization vanes.
This site was made possible by:
Validate me