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TO1;TO2;CLB1 and CLB2

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Old 9th July 2014 | 16:32
  #21 (permalink)  
 
Joined: May 2001
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From: A few degrees South
Look up in Google: "derated climb performance in large civil aircraft" , and you get the whole story. Interesting.
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Old 9th July 2014 | 18:11
  #22 (permalink)  
 
Joined: Mar 2001
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From: I wouldn't know.
@skyjob, we do not fly to the UK, but pretty much everywhere else in europe and get unrestricted climb in the majority of all cases.

Granted, if a low level off altitude is expected we do use reduced climb power.
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Old 18th October 2017 | 20:57
  #23 (permalink)  
 
Joined: Nov 2009
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From: EDDF
Derated Climb Performance In Large Civil Aircraft

Here, try this....

http://www.theairlinepilots.com/foru...erformance.pdf
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Old 19th October 2017 | 12:40
  #24 (permalink)  
 
Joined: Jan 2006
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From: US
TO2 with full derate is only about 60% of max thrust.
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Old 20th October 2017 | 01:31
  #25 (permalink)  
 
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From: US
777-300, at idle, is 737 cruise power. Similar fuel flows - 2700 lbs/hr +/-.
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Old 20th October 2017 | 05:26
  #26 (permalink)  
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Joined: Mar 2006
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From: USA
2700 per engine?! Surely you're joking. Right? That's insanely high. What's the fuel flow during takeoff and at cruise?
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Old 20th October 2017 | 10:05
  #27 (permalink)  
 
Joined: Jul 2014
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From: Germany
fuel capacity for 777-300ER from wikipedia: 320,863 lb / 145,538 kg

so let's say limit is 16h in the air that's 20053lbs/h or 9096kg/h
per engine that would be around 10026lbs/h or 4538kg/h.

now that's probably a bit high because it can stay in the air longer, not sure.
doing the same rough calculation for 7h of endurance of an 737-800 the 3000lbs/h seems realistic.

the 777 idle i would guess he is talking flight idle not ground idle.
but a much more pertinent question: why is this discussion in this thread?
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Old 24th October 2017 | 11:39
  #28 (permalink)  
 
Joined: Apr 2008
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From: by the river
Rick777: One other important concept with using derate is that min control speeds are based on the derate...
Note: V1 is based on the derate, not VMCG. V1 for TASS is based on full thrust TO, therefore in case of engine failure after V1 during TO with TASS you may increase power to MAX, but you may not perform this action during TO with D1 or D2 thrust setting, otherwise you will live RW a lit at bit early and in unpredictable direction.
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