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Home > Exam Questions > ATPL - Airline Transport Pilot Licence > Flight Planning and Monitoring > Use the attached SEP1 training Table 2.3.1 (economy cruise power). At pressure altitude 6000 ft, ISA deviation 0 degrees C and cruise mass 3400 lb, the manifold pressure is set to 21.0 in Hg at 2100 rpm with cruise-lean mixture. What cruise true airspeed and fuel flow in lb/h are read from the table?

57 - ATPL Question Bank in English - Use the attached SEP1 training Table 2.3.1 (economy cruise power). At pressure altitude 6000 ft, ISA deviation 0 degrees C and cruise mass 3400 lb, the manifold pressure is set to 21.0 in Hg at 2100 rpm with cruise-lean mixture. What cruise true airspeed and fuel flow in lb/h are read from the table?

Question 57 - Flight Planning and Monitoring - ATPL - Airline Transport Pilot Licence

Flight Planning and Monitoring - Use the attached SEP1 training Table 2.3.1 (economy cruise power). At pressure altitude 6000 ft, ISA deviation 0 degrees C and cruise mass 3400 lb, the manifold pressure is set to 21.0 in Hg at 2100 rpm with cruise-lean mixture. What cruise true airspeed and fuel flow in lb/h are read from the table?

136 kt and 56,9 lbs/hr

134 kt and 55,7 lbs/hr

125 kt and 55,7 lbs/hr

131 kt and 56,9 lbs/hr

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