Atpl flight planning - Study guides, Class notes & Summaries

ATPL (Philippines) - Flight Performance & Planning 31. Minimum specific fuel consumption of the turboprop engine is normally available in which altitude range? a. 25,000 feet to the tropopause. b. The tropopause to 45,000 feet. c. 10,000 feet to 25,000 feet. - correct answers a. 25,000 feet to the tropopause. 2. What effect would a change in ambient temperature or air density have on gas-turbine- engine performance? a. As temperature increases, thrust increases. b. As air density dec...

ATPL (Philippines) - Flight Performance & Planning 3 1. Minimum specific fuel consumption of the turboprop engine is normally available in which altitude range? a. 25,000 feet to the tropopause. b. The tropopause to 45,000 feet. c. 10,000 feet to 25,000 feet. - correct answers a. 25,000 feet to the tropopause. 2. What effect would a change in ambient temperature or air density have on gas-turbine- engine performance? a. As temperature increases, thrust increases. b. As air density d...

ATPL Flight planning Question and answer 100% solvedBlock Fuel Ramp Fuel Taxi fuel + APU fuel burnt + Take Off Fuel Take Off Fuel Block Fuel - Taxi fuel Trip Fuel Takeoff Climb to cruise level Flight in level cruise including any planned step climb or step descent Flight from the beginning of descent to the beginning of approach, Approach Landing at the destination Contingency Fuel 0.05 x Trip fuel Extra Fuel Commander's discretion Additional Fuel ...

ATPL - FLIGHT PERFORMANCE & PLANNING SET B 2/31. A flight is planned from L to M, distance 850 nm. Wind component out is 35 kt(TWC), TAS 450kt. Mean fuel flow out is 2500kg/hr, mean fuel flow inbound is 1900kg/hr and the fuel available is 6000kg. The time and distance to PSR is: a. 1hr 30 min, 660nm b. 1hr 30 min, 616nm c. 1hr 15 min, 606nm d. 1hr 16 min, 616nm - correct answers d. 1hr 16 min, 616nm 2. Refer to CAP697 MRJT1 Fig. 4.2 & 4.5.3.2 Estimated take-off mass 57,000kg; ground...

ATPL - FLIGHT PERFORMANCE & PLANNING 3/315. (Refer to Figure 11) What would be the approximate true airspeed and fuel consumption per hour at an altitude of 7,500 feet, using 52 percent power? a. 103 MPH TAS, 6.3 GPH b. 105 MPH TAS, 6.6 GPH c. 105 MPH TAS, 6.2 GPH - correct answers c. 105 MPH TAS, 6.2 GPH 20. (Refer to Figure 8) With 38 gallons of fuel aboard at cruise power (55 percent), how much flight time is available with night VFR fuel reserve still remaining? a. 2 hours 34 m...

ATPL - FLIGHT PERFORMANCE & PLANNING SET B 2/3 1. A flight is planned from L to M, distance 850 nm. Wind component out is 35 kt(TWC), TAS 450kt. Mean fuel flow out is 2500kg/hr, mean fuel flow inbound is 1900kg/hr and the fuel available is 6000kg. The time and distance to PSR is: a. 1hr 30 min, 660nm b. 1hr 30 min, 616nm c. 1hr 15 min, 606nm d. 1hr 16 min, 616nm - correct answers d. 1hr 16 min, 616nm 2. Refer to CAP697 MRJT1 Fig. 4.2 & 4.5.3.2 Estimated take-off mass 57,000kg; grou...

ATPL(A) Flight Planning and Preparation / Air Traffic Services (new)Explain requirements for obtaining and considering relevant information prior to flight? - correct answers P-I-C must obtain and become familiar with all information concerning that flight, including: - meteorological information. - fuel requirements. - alternatives available if planned flight cannot be completed. - any known or likely traffic delays notified by ATC. - status of communication and navigation facilities to be...

ATPL - FLIGHT PERFORMANCE & PLANNING 3/3

ATPL - FLIGHT PERFORMANCE & PLANNING SET B 1/3

ATPL (Philippines) - Flight Performance & Planning 4 4. GIVEN: Total Weight . . . . . . . . 4,137 lb CG Location . . . . . . . . Station 67.8 Fuel Consumption . . . . . . . . 13.7 GPH Fuel CG . . . . . . . . Station 68.0 After 1 hour 30 minutes of flight time, the CG would be located at station. a. 68.79 b. 70.78 c. 67.89 - correct answers c. 67.89 2. GIVEN: Weight A - 140 pounds at 17 inches aft of datum Weight B - 120 pounds at 110 inches aft of datum Weight C - 85 pounds at...