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
->
H02
->H.8.2.9.6.B.1
8296
On an aircraft turbine engine, operating at a constant power, the application of engine anti-icing will result in
A) a false EPR reading.
B) noticeable shift in EPR.
C) an increase in EPR.
This site was made possible by:
Validate me