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Old 20th Jun 2008, 16:31
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Droste
 
Join Date: Jun 2008
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Question Question 1
Given the following data what is the maximum assumed temperature which may be used to calculate variable thrust for take-off?
  • Aerodrome PA: 4000ft
  • OAT: +15C
  • 'D' for FLL TOW: 3250m
  • Actual TOW: 170,000kg
  • ACS packs: off
  • Assumed temperature limited by WAT: +37C
a)+30C b)+34C c)+37C d)+26C

What I did: Using (UK-CAP385)(Fig13) 4000ft, 3250m & 170,000kg, I get 37.5C. After that, 37.5C used in Fig 4 to get EPR 1.488. Now, I am stuck...
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