Question 80-1 : The empty mass of an aircraft as given in the weighing schedule is 61300 kg .the operational items including crew is given as a mass of 2300 kg .if the take off mass is 132000 kg including a useable fuel quantity of 43800 kg the useful load is ? [ Exam pilot ]

Question 80-2 : 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 ?

Question 80-3 : 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.the performance limited take off mass is 67 450kg and the ?

Question 80-4 : 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 ?

Question 80-5 : 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 ?

Question 80-6 : The following data is extracted from an aeroplane's loading manifest .performance limited take off mass 93500 kg.expected landing mass at destination 81700 kg.maximum certificated landing mass 86300 kg.fuel on board 16500 kg.during the flight a diversion is made to an en route alternate which is ?

Question 80-7 : With respect to multi engine piston powered aeroplane determine the ramp mass lbs in the following conditions . basic empty mass 3210 lbs.basic arm 88 5 inches.one pilot 160 lbs.front seat passenger 200 lbs.centre seat passengers 290 lbs.one passenger rear seat 110 lbs.baggage in zone 1 100 ?

Question 80-8 : The crew of a transport aeroplane prepares a flight using the following data . dry operating mass 90 000 kg. block fuel 30 000 kg. taxi fuel 800 kg. maximum take off mass 145 000 kg.the traffic load available for this flight is ?

Question 80-9 : Determine the zero fuel mass for the following single engine aeroplane .given .standard empty mass 1799 lbs.pilot + front seat passenger 300 lbs.cargo mass 350 lbs.block fuel 60 gal .trip fuel 35 gal .fuel density 6 lbs/gal ?

Question 80-10 : Given .standard empty mass 1764 lbs.optional equipment 35 lbs.pilot + front seat passenger 300 lbs.cargo mass 350 lbs.block fuel 60 gal .trip fuel 35 gal .taxi fuel 1 7 gal .fuel density 6 lbs/gal.determine the expected landing mass ?

Question 80-11 : The take off mass of an aeroplane is 66700 kg which includes a traffic load of 12500 kg and a usable fuel load of 10200 kg if the standard mass for the crew is 545 kg the dry operating mass is ?

Question 80-12 : The take off mass of an aeroplane is 8600 kg which includes a traffic load of 1890 kg and a usable fuel load of 1230 kg if the standard mass for the crew is 190 kg the dry operating mass is ?

Question 80-13 : The loading for a flight is shown in the loadsheet with the following data applying to the aeroplane .maximum take off mass 150 000 kg.maximum landing mass 140 000 kg.centre of gravity cg limit forward 10 5 m aft of datum.aft 13 0 m aft of datum.estimated trip fuel 55 000 kg . 205 ?

Question 80-14 : 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 ?

Question 80-15 : Dry operating mass is the mass of the aircraft less ?

Question 80-16 : The total mass of the aircraft including crew crew baggage plus catering and removable passenger equipment plus potable water and lavatory chemicals but excluding usable fuel and traffic load is referred to as ?

Question 80-17 : The responsibility for determination of the mass of 'operating items' and 'crew members' included within the dry operating mass lies with ?

Question 80-18 : The dry operating mass is the total mass of the aircraft ready for a specific type of operation but excluding ?

Question 80-19 : The take off mass of an aeroplane is 66700 kg which includes a traffic load of 14200 kg and a usable fuel load of 10500 kg .if the standard mass for the crew is 545 kg the dry operating mass is ?

Question 80-20 : The maximum certificated taxi or ramp mass is that mass to which an aircraft may be loaded prior to engine start .it is ?

Question 80-21 : The maximum mass to which an aeroplane may be loaded prior to engine start is ?

Question 80-22 : The zero fuel mass and the dry operating mass ?

Question 80-23 : A revenue flight is planned for the transport aeroplane take off mass is not airfield limited the following data applies .dry operating mass 34930 kg.performance limited landing mass 55000 kg.fuel on board at ramp . taxi fuel 350 kg. trip fuel 9730 kg. contingency and final reserve fuel 1200 kg. ?

Question 80-24 : The empty mass of an aeroplane is given as 44800 kg .operational items including crew standard mass of 1060 kg are 2300 kg .if the maximum zero fuel mass is given as 65500 kg the maximum traffic load which could be carried is ?

Question 80-25 : The maximum zero fuel mass is a structural limiting mass it is made up of the aeroplane dry operational mass plus ?

Question 80-26 : The take off mass of an aeroplane is 141000 kg .total fuel on board is 63000 kg including 14000 kg reserve fuel and 1000 kg of unusable fuel .the traffic load is 12800 kg .the zero fuel mass is ?

Question 80-27 : 'standard mass' as used in the computation of passenger load establish the mass of a child as ?

Question 80-28 : The maximum certificated take off mass is ?

Question 80-29 : For a particular aeroplane the structural maximum mass without any fuel on board other than unusable quantities is ?

Question 80-30 : On an aeroplane with a seating capacity of more than 30 it is decided to use standard mass values for computing the total mass of passengers .if the flight is not a holiday charter the mass value which may be used for an adult is ?

Question 80-31 : The standard mass for a child is ?

Question 80-32 : On an aeroplane with 20 or more seats engaged on an inter continental flight the 'standard mass' which may be used for passenger baggage is ?

Question 80-33 : 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 ?

Question 80-34 : In determining the dry operating mass of an aeroplane it is common practice to use 'standard mass' values for crew .these values are ?

Question 80-35 : The medium range jet transport aeroplane is to operate a flight carrying the maximum possible fuel load .departure airfield performance limited take off mass 60 400 kg .landing airfield not performance limited.dry operating mass 34930 kg.fuel required for flight .taxi fuel 715 kg.trip fuel 8600 ?

Question 80-36 : An aircraft is to depart from an airfield at a take off mass of 302550 kg .fuel on board at take off including contingency and alternate of 19450 kg is 121450 kg .the dry operating mass is 161450 kg .the useful load will be ?

Question 80-37 : Conversion of fuel volume to mass ?

Question 80-38 : Standard masses may be used for the computation of mass values for baggage if the aircraft ?

Question 80-39 : 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. ?

Question 80-40 : 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/l .the following are the aeroplane's structural limits ?