Results
Q1. The following data applies to an aeroplane which is about to take off: Certified maximum take-off mass 141500 kg Performance limited take-off mass 137300 kg Dry Operating Mass 58400 kg Crew and crew hand baggage mass 640 kg Crew baggage in hold 110 kg Fuel on board 60700 kg From this data calculate the mass of the useful load.
Correct answer is B – 78900 kg
Q2. Given: Dry operating mass = 38 000 kg Maximum structural take-off mass = 72 000 kg Maximum landing mass = 65 000 kg Maximum zero fuel mass = 61 000 kg Fuel burn = 8 000 kg Take-off Fuel = 10 300 kg The maximum allowed take-off mass and payload are respectively:
Correct answer is D – 71 300 kg and 23 000 kg
Q3. A revenue flight is to be made by jet transport. The following are the airplane’s structural limits: Maximum Ramp Mass: 69 900 kg Maximum Take Off Mass: 69 300 kg. Maximum Landing Mass: 58 900 kg Maximum Zero Fuel Mass: 52 740 kg The performance limited take off mass is 67 450 kg. Performance limited landing mass is 55 470 kg. Dry Operating Mass: 34 900 kg Trip Fuel: 6 200 kg Taxi Fuel: 250 kg Contingency & final reserve fuel: 1 300 kg Alternate Fuel: 1 100 kg The maximum traffic load that can be carried is:
Correct answer is D – 17840 kg
Q4. The crew of a transport aeroplane prepares a flight using the following data: – Block fuel: 40 000 kg- Trip fuel: 29 000 kg- Taxi fuel: 800 kg- Maximum take-off mass: 170 000 kg- Maximum landing mass: 148 500 kg- Maximum zero fuel mass: 112 500 kg- Dry operating mass: 80 400 kg The maximum traffic load for this flight is:
Correct answer is C – 32 100 kg
Q5. The following data applies to a planned flight. Dry Operating Mass 34900 kg Performance limited Take-Off Mass 66300 kg Performance limited Landing Mass 55200 kg Maximum Zero Fuel Mass 53070 kg Fuel required at ramp: -Taxy fuel 400 kg. Trip fuel 8600 kg contingency fuel 430 kg alternate fuel 970 kg holding fuel 900 Kg Traffic load 16600 kg Fuel costs at the departure airfield are such that it is decided to load the maximum fuel quantity possible. The total fuel which may be safely loaded prior to departure is:
Correct answer is A – 12700 kg.
Q6. Prior to departure the medium range twin jet aeroplane is loaded with maximum fuel of 20100 liters at a fuel density (specific gravity) of 0.78. Using the following data – Performance limited take-off mass 67200 kg Performance limited landing mass 54200 kg Dry Operating Mass 34930 kg Taxi fuel 250 kg & Trip fuel 9250 kg Contingency and holding fuel 850 kg Alternate fuel 700 kg The maximum permissible traffic load is :
Correct answer is C – 13090 kg.
Q7. Given: Maximum structural take-off mass= 146 900 kg Maximum structural landing mass= 93 800 kg Maximum zero fuel mass= 86 400 kg Trip fuel= 27 500 kg Block fuel= 35 500 kg Engine starting and taxi fuel = 1 000 kg The maximum take-off mass is equal to:
Correct answer is B – 120 900 kg
Q8. Given: Dry Operating Mass= 29 800 kg Maximum Take-Off Mass= 52 400kg Maximum Zero-Fuel Mass= 43 100 kg Maximum Landing Mass= 46 700 kg Trip fuel= 4 000 kg Fuel quantity at brakes release= 8 000 kg The maximum traffic load is:
Correct answer is B – 12 900 kg
Q9. Given the following: – Maximum structural take-off mass 48 000 kg- Maximum structural landing mass: 44 000 kg- Maximum zero fuel mass: 36 000 kg- Taxi fuel: 600 kg- Contingency fuel: 900 kg- Alternate fuel: 800 kg- Final reserve fuel: 1 100 kg- Trip fuel: 9 000 kg Determine the actual take-off mass:
Correct answer is D – 47 800 kg
Q10. Given that: – Maximum structural take-off mass: 146 000 kg- Maximum structural landing mass: 93 900 kg- Maximum zero fuel mass: 86 300 kg- Trip fuel: 27 000 kg- Taxi fuel: 1 000 kg- Contingency fuel: 1350 kg- Alternate fuel: 2650 kg- Final reserve fuel: 3000 kg Determine the actual take-off mass:
Correct answer is B – 120 300 kg.
Q11. Given are:- Maximum structural take-off mass: 72 000 kg- Maximum structural landing mass: 56 000 kg- Maximum zero fuel mass: 48 000 kg- Taxi fuel: 800 kg- Trip fuel: 18 000 kg- Contingency fuel: 900 kg- Alternate fuel: 700 kg- Final reserve fuel: 2 000 kg Determine the actual take-off mass:
Correct answer is C – 69 600 kg
Q12. Given an aeroplane with: Maximum Structural Landing Mass: 68000 kg Maximum Zero Fuel Mass: 70200 kg Maximum Structural Take-off Mass: 78200 kg Dry operating Mass : 48000 kg Scheduled trip fuel is 7000 kg and the reserve fuel is 2800 kg, Assuming performance limitations are not restricting, the maximum permitted take-off mass and maximum traffic load are respectively:
Correct answer is D – 75000 kg and 17200 kg
Q13. Given an aeroplane with: Maximum Structural Landing Mass: 125000 kg Maximum Zero Fuel Mass: 108500 kg Maximum Structural Take-off Mass: 155000 kg Dry Operating Mass: 82000 kg Scheduled trip fuel is 17000 kg and the reserve fuel is 5000 kg. Assuming performance limitations are not restricting, the maximum permitted take-off mass and maximum traffic load are respectively:
Correct answer is A – 130500 kg and 26500 kg
Q14. A jet transport has the following structural limits: – Maximum Ramp Mass: 63 060 kg Maximum Take Off Mass: 62 800 kg Maximum Landing Mass: 54 900 kg Maximum Zero Fuel Mass: 51 300 kg The aeroplane’s fuel is loaded accordance with the following requirements: – Taxi fuel: 400 kg Trip fuel: 8400 kg Contingency & final reserve fuel: 1800 kg & Alternate fuel: 1100 kg If the Dry Operating Mass is 34930 kg, determine the maximum traffic load that can be carried on the flight if departure and landing airfields are not performance limited.
Correct answer is A – 16 370 kg
Q15. An aeroplane is to depart from an airfield where the performance limited take-off mass is 89200 kg. Certificated maximum masses are as follows: Ramp (taxi) mass 89930 kg Maximum Take-off mass 89430 kg Maximum Landing mass 71520 kg Actual Zero fuel mass 62050 kg Fuel on board at ramp: Taxi fuel 600 kg Trip fuel 17830 kg Contingency, final reserve and alternate 9030 kg If the Dry Operating Mass is 40970 kg, then find the traffic load that can be carried on this flight is
Correct answer is A – 21080 kg
Q16. A revenue flight is to be made by a jet transport. The following are the aeroplane’s structural limits: – Maximum Ramp Mass: 70 000 kg Maximum Take Off Mass: 69 500 kg Maximum Landing Mass: 58 400 kg Maximum Zero Fuel Mass: 54 000 kg Performance limited take off mass is 67 500kg and performance limited landing mass is 55 000 kg. Dry Operating Mass: 32 500 kg Trip Fuel: 6 000 kg Taxi Fuel: 500 kg Contingency& final reserve fuel: 1 500 kg Alternate Fuel: 1 000 kg The maximum traffic load that can be carried is:
Correct answer is C – 20 000 kg
Q17. A revenue flight is to be made by a jet transport. The following are the aeroplane’s structural limits: – Maximum Ramp Mass: 69 900 kg Maximum Take Off Mass: 69 300 kg Maximum Landing Mass: 58 900 kg Maximum Zero Fuel Mass: 52 740 kg Dry Operating Mass: 34 930 kg Trip Fuel: 11 500 kg Taxi Fuel: 250 kg Contingency& final reserve fuel: 1 450 kg Alternate Fuel: 1 350 kg TakeOff and Landing mass are not performance limited. The maximum traffic load that can be carried is:
Correct answer is A – 17 810 kg
Q18. A revenue flight is to be made by a jet transport. The following are the aeroplane’s structural limits: – Maximum Ramp Mass: 69 900 kg Maximum Take Off Mass: 69 300 kg Maximum Landing Mass: 58 900 kg Maximum Zero Fuel Mass: 52 740 kg Take Off and Landing mass are not performance limited. Dry Operating Mass: 34 900 kg Trip Fuel: 11 800 kg Taxi Fuel: 500 kg Contingency& final reserve fuel: 1 600 kg Alternate Fuel: 1 900 kg The maximum traffic load that can be carried is:
Correct answer is C – 17 840 kg
Q19. The flight preparation of a turbojet aeroplane provides the following data: Take-off runway limitation: 185 000 kg Landing runway limitation: 180 000 kg Planned fuel consumption: 11 500 kg Fuel already loaded on board the aircraft: 20 000 kg Knowing that: Maximum take-off mass (MTOM): 212 000 kg Maximum landing mass (MLM): 174 000 kg Maximum zero fuel mass (MZFM): 164 000 kg Dry operating mass (DOM): 110 000 kg The maximum cargo load that the captain may decide to load on board is:
Correct answer is B – 54 000 kg
Q20. Given: Dry operating mass = 38 000 kg maximum structural take-off mass = 72 000 Kg maximum landing mass = 65 000 kg maximum zero fuel mass = 61 000 kg Fuel burn = 8 000 kg Take-off Fuel = 10 300 kg The maximum allowed take-off mass and payload are respectively:
Correct answer is C – 71 300 kg and 23 000 kg
Q21. An aeroplane has a maximum structural take-off mass of 64800 kg and a maximum structural landing mass of 56000 kg. Calculate the maximum traffic load for a flight of three hours duration if each of the four engines consumes 1500 litres of fuel per hour. Performance Limited TOM 62800 kg MZFM 51300 kg DOM 27372 kg Maximum Ramp Fuel 35805 ltr Ramp Fuel 35802.8 ltr @ SG= 0.72 kg/ltr Start/taxi Fuel per engine 350 kg
Correct answer is B – 11050kg
Q22. A twin-engine aeroplane is certified for a Max Structural TOM and a Max LM of 58000 kg and 55000 kg respectively. Given the information below, what is the limiting take-off mass for the aeroplane? Performance Limiting TOM 61000 kg Performance limiting LM 54000 kg MZFM 36000 kg Operating mass 55000 kg Trip fuel 3000 kg Contingency fuel 5% of trip fuel Alternate fuel 500 kg Final reserve 500 kg Flight duration 3 hours Fuel consumption 500 kg per hour per engine
Correct answer is C – 57000 kg
Q23. A scheduled flight of three hours estimated flight time, within Europe, is being planned. Calculate the maximum mass that may be loaded in the following circumstances: Structural limited take-off mass: 62,800 kg Structural limited landing mass: 54,900 kg MZFM: 51,300 kg Dry Operating Mass: 34,960 kg Fuel on board at ramp: 15,800 kg Taxi fuel: 450 kg Trip fuel: 10,200 kg Passengers (adults each 84 kg): 115 Passengers (children each 35 kg): 6 standard baggage for each passenger: 13 kg Flight crew (each 85 kg): 2 Cabin crew (each 75 kg): 3
Correct answer is C – 1,047 kg
Q24. Prior to departure an MRJT is loaded with maximum fuel of 20,000 lt. at an SG of 0.80. Calculate the maximum allowable traffic load that can be carried given the following data: Performance Limited TOM 67 500 kg Performance Limited LM 54 500 kg MZFM: 51,500 kg DOM 35 000 kg Taxi fuel 500 kg Trip fuel 9000 kg Contingency and holding fuel 800 kg. Alternate fuel 700 kg
Correct answer is D – 13000 kg
Q25. An aeroplane takes off as normal on a scheduled flight however, shortly after take-off the aeroplane is diverted to another airfield. Max Structural TOM 14000 kg Performance Limited TOM 12690 kg Max Structural LM 9600kg Trip Fuel to original destination 6000 kg Contingency fuel 200kg Alternate fuel 200 kg Final reserve fuel 750kg Expected landing mass at original destination 4600kg Actual flight duration 2 hour Fuel consumption 1,500 kg per hour Performance Limited LM at diversion airfield 9000 kg
Correct answer is B – The aeroplane can land safely because it is below its PLLM
Q26. Given that: Maximum structural take-off mass: 146 000 kg Maximum structural landing mass: 93 900 kg Actual zero fuel mass: 86 300 kg Trip fuel: 27 000 kg Taxi fuel: 1 000 kg Contingency fuel: 1350 kg Alternate fuel: 2650 kg Final reserve fuel: 3000 kg Determine the actual take-off mass:
Correct answer is C – 120 300 kg
Q27. Determine the Zero Fuel Mass for the following single engine aeroplane. Given: Standard Empty Mass: 1764 lbs Optional Equipment: 35 lbs Pilot + Front seat passenger: 300 lbs Cargo Mass: 350 lbs Ramp Fuel = Block Fuel: 60 Gal. Trip Fuel: 35 Gal. Fuel density: 6 lbs/Gal.
Correct answer is B – 2449 lbs
Q28. A scheduled flight of three hours an estimated duration within Europe is to be conducted. Using the data given within the loading manual for a medium range twinjet aircraft, calculate the maximum mass that may be loaded in the following circumstances: Performance limited take-off mass = 67 900 kg Performance limited landing mass = 56 200 kg Dry operating mass = 34 960 kg Fuel on board at ramp = 15 800 kg Taxi fuel = 450 kg Trip fuel = 10 200 kg Passengers: (adults/each 84 kg) = 115 (children/ each 35 kg) = 6 Standard baggage for each passenger = 13kg Flight crew (each 85kg) = 2 Cabin crew (each 75 kg) = 5
Correct answer is D – 4647 kg
Q29. A flight has been made from London to Valencia carrying minimum fuel and maximum traffic load. On the return flight the fuel tanks in the aeroplane are to be filled to capacity with a total fuel load of 20100 litres at a fuel density of 0.79 kg/ltr. The following are the aeroplane’s structural limits: Maximum Ramp Mass: 69 900 kg Maximum Take Off Mass: 69 300 kg Maximum Landing Mass: 58 900 kg Maximum Zero Fuel Mass: 52 740 kg The performance limited take off mass at Valencia is 67 330 kg The landing mass at London is not performance limited. Dry Operating Mass: 34 930 kg Trip Fuel (Valencia to London): 5 990 kg Taxi fuel: 250 kg The maximum traffic load that can be carried from Valencia will be:
Correct answer is A – 14 331 kg
Q30. Based on actual conditions, an aeroplane has the following performance take-off mass limitations: Flaps: 0° / 10° / 15° Runway: 4100 / 4400 / 4600 (Masses are in kg) Climb: 4700 / 4500 / 4200 (Masses are in kg) Structural limits: Take-off / landing / zero fuel: 4 300 kg The maximum take-off mass is:
Correct answer is D – 4 300 kg
Q31. Determine the Landing Mass for the following single engine aeroplane. Given: Standard Empty Mass: 1764 lbs Optional Equipment: 35 lbs Pilot + Front seat passenger: 300 lbs Cargo Mass: 350 lbs Ramp Fuel = Block Fuel: 60 Gal. Trip Fuel: 35 Gal. Fuel density: 6 lbs/Gal.
Correct answer is C – 2599 lbs
Q32. A scheduled flight of three hours estimated time, within Europe, is to be conducted. Using the data given calculate the maximum mass that may be loaded in the following circumstances: Performance limited take-off mass: 67,900 kg Performance limited landing mass: 56,200 kg MZFM: 51,300 kg DOM: 34,960 kg Fuel on board at ramp: 15,800 kg Taxi fuel: 450 kg Trip fuel: 10,200 kg Passengers: 115 adults (84 kg) + 6 children ( 35 kg ) Flight crew (each 85 kg): 2 Cabin crew (each 75 kg): 5 Allow standard baggage for each passenger (13 kg).
Correct answer is D – 4647 kg.
Q33. MTOM- 48000 Kg MLM- 37000 kg DOM- 24000kg MZFM- 36000 kg Flight Time – 4hr Fuel Consumption – 1600 kg per hr Taxi- 400kg Reserve- 10% of Trip Fuel Diversion Fuel- 30 minutes Holding – 15 minutes Find the maximum traffic load that can be carried:
Correct answer is 11160kg.
Q34. MTOM- 45000 Kg MLM- 36000 kg DOM- 22000kg Flight Time – 5hr Taxi- 500kg Trip fuel – 6000kg Reserve- 10% of Trip Fuel Diversion Fuel- 30 minutes Holding – 15 minutes Find the maximum traffic load that can be carried.
Correct answer is Payload- 12500kg
Q35. MTOM- 60000 Kg MLM- 40000 kg DOM- 25000kg Ground speed- 200knots Distance – 1600Nm Taxi- 500kg Trip fuel – 6000kg Reserve- 10% of Trip Fuel Diversion Fuel- 30 minutes Holding – 15 minutes Find Ramp Mass and the maximum traffic load that can be carried:
Correct answer is Ramp Mass- 46500kg & Payload- 13837.5kg
Q36. MCTOM- 45000 Kg MLM- 37000 kg DOM- 28000kg MZFM- 38000 kg Flight Time – 6hr Fuel Consumption – 1500 kg per hr Taxi- 600kg Reserve- 10% of Trip Fuel Diversion Fuel- 30 minutes Holding – 15 minutes Captain ordered to fill 12000kg fuel. Find Ramp fuel and the maximum traffic load that can be carried:
Correct answer is Fuel at Ramp*- 12000kg & Payload- 5600kg
Q37. MTOM- 60000 Kg MLM- 40000 kg DOM- 30000kg Ground speed- 120knots Distance – 120Nm Taxi- 600kg Trip fuel – 6000kg Reserve- 10% of Trip Fuel Diversion Fuel- 30 minutes Holding – 45 minutes Find Take-off fuel and the maximum traffic load that can be carried?
Correct answer is Payload:1900kg & take off fuel:14100kg.
Q38. DOM – 60000 ZFM- 180000 Certified TOM- 250000 Fuel consumption – 1200 kg/ nm Distance to go – 100Nm. Reserve fuel – 15% of trip fuel Contingency fuel- 5% of trip Certified Landing MASS- 240000kg Find take off mass and the maximum traffic load that can be carried:
Correct answer is actual Take-off mass= 250000 &Pay load= 46000
Q39. In above question if Captain wishes to carry 2000kg more fuel, and taxi fuel is 1200 kg then how much fuel can be loaded and how much payload can be carried.
Fuel must be loaded = 147200 kg, Payload = 44000 kg
