Question 80-1 : 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...the actual tom can never be higher than ? [ Exam pilot ]

Question 80-2 : The maximum zero fuel mass..1 is a regulatory limitation.2 is calculated for a maximum load factor of +3.5 g.3 is based on the maximum permissible bending moment at the wing root.4 is defined on the assumption that fuel is consumed from the outer wings tank first.5 is defined on the assumption ?

Question 80-3 : At the flight preparation stage, the following parameters in particular are available for determining the mass of the aircraft.1 dry operating mass.2 operating mass..which statement is correct ?

Question 80-4 : Which of the following corresponds to zero fuel mass ?

Question 80-5 : Given that. maximum structural take off mass 146000 kg. maximum structural landing mass 93900 kg. maximum zero fuel mass 86300 kg. trip fuel 27000 kg. taxi fuel 1000 kg. contingency fuel 1350 kg. alternate fuel 2650 kg. final reserve fuel 3000 kg..determine the actual take off mass ?

Question 80-6 : Given. 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 ?

Question 80-7 : The actual take off mass is equal to 41 545 kg.. catering 300 kg. safety and rescue material nil. fly away kit nil. crew inclusive crew baggage 365 kg. fuel at take off 3 000 kg. unusable fuel 120 kg. passengers, baggage, cargo 8 000 kg..the basic empty mass is ?

Question 80-8 : The zero fuel mass of an aeroplane is always ?

Question 80-9 : 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 ?

Question 80-10 : Traffic load is the ?

Question 80-11 : While making mass and balance calculation for a particular aircraft, the term 'basic empty mass' applies to the sum of airframe, engine s , fixed ballast plus ?

Question 80-12 : The term 'maximum zero fuel mass' consist of ?

Question 80-13 : The actual 'zero fuel mass' is equal to the ?

Question 80-14 : The actual 'take off mass' is equivalent to ?

Question 80-15 : With respect to aeroplane loading in the planning phase, which of the following statements is always correct.lm = landing mass.tom = take off mass.mtom = maximum take off mass.zfm = zero fuel mass.mzfm = maximum zero fuel mass.dom = dry operating mass ?

Question 80-16 : 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 ?

Question 80-17 : For the purpose of completing the mass and balance documentation, the traffic load is considered to be equal to the take off mass ?

Question 80-18 : For the purpose of completing the mass and balance documentation, the operating mass is considered to be dry operating mass plus ?

Question 80-19 : When establishing the mass breakdown of an aeroplane, the empty mass is defined as the sum of the ?

Question 80-20 : For the purpose of completing the mass and balance documentation, the dry operating mass is defined as ?

Question 80-21 : An aircraft's weighing schedule indicates that the empty mass is 57320 kg..the nominal dry operating mass is 60120 kg and the maximum zero fuel mass is given as 72100 kg...which of the following is a correct statement in relation to this aeroplane ?

Question 80-22 : 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.maximum zero fuel mass 62050 kg..fuel on board at ramp.taxi fuel 600 ?

Question 80-23 : 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 ?

Question 80-24 : 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 80-25 : 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 80-26 : 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 ?

Question 80-27 : 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 80-28 : 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 80-29 : 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 80-30 : 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 80-31 : 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 80-32 : 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 80-33 : 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 80-34 : 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 80-35 : 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 80-36 : 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 80-37 : Dry operating mass is the mass of the aircraft less ?

Question 80-38 : 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 80-39 : The responsibility for determination of the mass of operating items and crew members included within the dry operating mass lies with ?

Question 80-40 : The dry operating mass is the total mass of the aircraft ready for a specific type of operation but excluding ?