Quote:
Originally Posted by typhoonpilot  Pitch is probably between 1.5 and 3.0 degrees ANU depending on weight. Doug, just look in the QRH for flight with unreliable airspeed. There should be pitch attitudes shown there.
Cost Index is a number derived from a formula. The formula is operating cost ( $/hour ) over fuel cost ( cents/pound ). Only those portions of operating cost affected by trip time should be included in the calcualtion ( i.e. cost of crew/hour, maintenance, etc. ).
Typhoonpilot |
cool, thanks!
so 5 degrees up is too much eh?
lets say operating cost of 300 by fuel (6.48 a gallon, so lbs is .92 cents) comes way off though?