Wikiposts
Search

Notices
Engineers & Technicians In this day and age of increased CRM and safety awareness, a forum for the guys and girls who keep our a/c serviceable.

CFM 56 questions

Thread Tools
 
Search this Thread
 
Old 22nd June 2012 | 05:44
  #1 (permalink)  
Thread Starter
10 Anniversary
 
Joined: Nov 2011
Posts: 1,305
Likes: 35
From: Vietnam
CFM 56 questions

Hello,

I have a interview soon with a major carrier but don't have any jet time. I was just wondering what is entered into the flight management system for a de rated thrust take off? I thought it was temperature but I have been told also that its pressure height. Which ever one it is would it be a higher value that is entered? If it is how does that produce less thrust?

Also another question is what is meant by the CFM 56 is flat rated at ISA +15?

Thank you,

Last edited by pilotchute; 22nd June 2012 at 05:46.
pilotchute is offline  
Reply
Old 22nd June 2012 | 06:07
  #2 (permalink)  
 
Joined: Sep 2009
Posts: 353
Likes: 0
From: bahrain
Never heard about entering the barometric altitude in the FMS, I know of the flexible tempreture which the pilot enters to reduce the take off thrust at FLX MCT detent to increase engine life.
Flexible tempreture must always be higher than what the tempreture actually is except in hot and high conditions when it has to be the same.
It means engine power rating is reduced at international standard atmospheric temperature 15+.

Last edited by flame_bringer; 22nd June 2012 at 09:11.
flame_bringer is offline  
Reply
Old 22nd June 2012 | 09:43
  #3 (permalink)  
 
Joined: Jun 2010
Posts: 304
Likes: 0
From: Brisbane, Australia
hey pilotchute...
Don't get confused between 'derated power' and 'assumed temperature power', they are two different things!
With derated power, the FMC commands a set decrease in N1 RPM that usually equates to 10% (derate 1) and 20% (derate 2), with an accompanying decreased selection for climb power, (1 & 2) since you don't want to have climb power set at a level greater than takeoff power!
With assumed temperature power, you select a temperature greater than the actual ambient for the takeoff conditions, and the engines simply produce the output equivalent to that temperature, even though no actual temperature increase is felt by the engines. This is simply an alternative way to decrease the takeoff power to preserve the engines. Any decrease in takeoff EGT will extend the life of the engine! This input temperature is selected from examination of the takeoff performance of this airplane at this runway, its not random!
I am not aware of any baro input to this performance calculation, I've never ever seen that done!

As regards 'flat rated power', if an engine is flat rated to ISA+15, then that engine can maintain its rated power output up to ISA+15 degC, (at sea level) with any further increase in temperature resulting in a (usually) linear decrease in power output.

Cheers, EW73

Last edited by EW73; 22nd June 2012 at 09:47.
EW73 is offline  
Reply
Old 24th June 2012 | 11:06
  #4 (permalink)  
Thread Starter
10 Anniversary
 
Joined: Nov 2011
Posts: 1,305
Likes: 35
From: Vietnam
Thank you very much

Cheers for the very informative answers. I appreciate the time you put in. Let you know how it goes.
pilotchute is offline  
Reply

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are Off
Refbacks are Off



Contact Us - Archive - Advertising - Cookie Policy - Privacy Statement - Terms of Service

Copyright © 2026 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.