See Flight planning Manual SEP 1 Figure 2.3 Table 2.3.1. Using the Power Setting Table, for the single engine aeroplane, determine the cruise TAS and fuel flow (lbs/hr) with full throttle and cruise lean mixture in the following conditions. Given: OAT: 3°C; Pressure altitude: 6000 ft; Power: Full throttle / 21,0 in/Hg./ 2100 RPM - ATPL - ID: 57

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Home > Exam Questions > ATPL - Airline Transport Pilot license > Flight Planning and Monitoring > See Flight planning Manual SEP 1 Figure 2.3 Table 2.3.1. Using the Power Setting Table, for the single engine aeroplane, determine the cruise TAS and fuel flow (lbs/hr) with full throttle and cruise lean mixture in the following conditions. Given: OAT: 3°C; Pressure altitude: 6000 ft; Power: Full throttle / 21,0 in/Hg./ 2100 RPM

Question id 57 - Flight Planning and Monitoring - ATPL - Airline Transport Pilot license

Flight Planning and Monitoring - See Flight planning Manual SEP 1 Figure 2.3 Table 2.3.1. Using the Power Setting Table, for the single engine aeroplane, determine the cruise TAS and fuel flow (lbs/hr) with full throttle and cruise lean mixture in the following conditions. Given: OAT: 3°C; Pressure altitude: 6000 ft; Power: Full throttle / 21,0 in/Hg./ 2100 RPM

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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