When establishing the mass breakdown of an aeroplane the empty mass is defined ? [ Exam pilot ]

Question 80-1 : Standard empty mass plus specific equipment mass plus trapped fluids plus unusable fuel mass empty mass dry plus variable equipment mass basic mass plus variable equipment mass basic mass plus special equipment mass

For the purpose of completing the mass and balance documentation the dry ?

Question 80-2 : The total mass of the aircraft ready for a specific type of operation excluding all usable fuel and traffic load the total mass of the aircraft ready for a specific type of operation excluding all usable fuel the total mass of the aircraft ready for a specific type of operation excluding all traffic load the total mass of the aircraft ready for a specific type of operation excluding crew and crew baggage

An aircraft's weighing schedule indicates that the empty mass is 57320 kg .the ?

Question 80-3 : Operational items have a mass of 2800 kg and the maximum traffic load for this aeroplane is 11980 kg operational items have a mass of 2800 kg and the maximum traffic load for this aeroplane is 14780 kg operational items have a mass of 2800 kg and the maximum useful load is 11980 kg operational items have a mass of 2800 kg and the maximum useful load is 14780 kg

An aeroplane is to depart from an airfield where the performance limited take ?

Question 80-4 : 21080 kg 21500 kg 21220 kg 20870 kg

The empty mass of an aircraft as given in the weighing schedule is 61300 kg ?

Question 80-5 : 68400 kg 29600 kg 70700 kg 26900 kg

The following data applies to an aeroplane which is about to take off ?

Question 80-6 : 78900 kg 78150 kg 18200 kg 17450 kg

A revenue flight is to be made by a jet transport the following are the ?

Question 80-7 : 17 840 kg 25 800 kg 18 170 kg 13 950 kg

A revenue flight is to be made by a jet transport .the following are the ?

Question 80-8 : 17 810 kg 21 170 kg 21 070 kg 20 420 kg

A revenue flight is to be made by a jet transport the following are the ?

Question 80-9 : 17 840 kg 19 500 kg 19 100 kg 19 200 kg

The following data is extracted from an aeroplane's loading manifest ?

Question 80-10 : Is 87300 kg and excess structural stress could result is 83200 kg which is in excess of the regulated landing mass and could result in overrunning the runway must be reduced to 81700 kg in order to avoid a high speed approach is 87300 kg which is acceptable in this case because this is a diversion and not a normal scheduled landing

With respect to multi engine piston powered aeroplane determine the ramp mass ?

Question 80-11 : 4720 lbs 4120 lbs 4390 lbs 4372 lbs

The crew of a transport aeroplane prepares a flight using the following data . ?

Question 80-12 : 25 800 kg 55 800 kg 25 000 kg 55 000 kg

Determine the zero fuel mass for the following single engine aeroplane .given ?

Question 80-13 : 2449 lbs 2589 lbs 2659 lbs 2414 lbs

Given .standard empty mass 1764 lbs.optional equipment 35 lbs.pilot + front ?

Question 80-14 : 2589 lbs 2599 lbs 2472 lbs 2557 lbs

The take off mass of an aeroplane is 66700 kg which includes a traffic load of ?

Question 80-15 : 44000 kg 54200 kg 56500 kg 43465 kg

The take off mass of an aeroplane is 8600 kg which includes a traffic load of ?

Question 80-16 : 5480 kg 5290 kg 8410 kg 6710 kg

The loading for a flight is shown in the loadsheet with the following data ?

Question 80-17 : Landing cg is out of limits at 10 17 m aft of datum landing cg is out of limits at 11 97 m aft of datum take off cg is out of limits at 10 17 m aft of datum take off cg is out of limits at 12 34 m aft of datum

Given an aeroplane with .maximum structural landing mass 68000 kg.maximum zero ?

Question 80-18 : 75000 kg and 17200 kg 75000 kg and 20000 kg 77200 kg and 19400 kg 77200 kg and 22200 kg

Dry operating mass is the mass of the aircraft less ?

Question 80-19 : Usable fuel and traffic load usable fuel traffic load potable water and lavatory chemicals usable fuel potable water and lavatory chemicals

The total mass of the aircraft including crew crew baggage plus catering and ?

Question 80-20 : Dry operating mass zero fuel mass landing mass maximum zero fuel mass

The responsibility for determination of the mass of 'operating items' and 'crew ?

Question 80-21 : The operator the commander the authority of the state of registration the person compiling the weighing schedule

The dry operating mass is the total mass of the aircraft ready for a specific ?

Question 80-22 : Usable fuel and traffic load the traffic load useful fuel crew and crew baggage

The take off mass of an aeroplane is 66700 kg which includes a traffic load of ?

Question 80-23 : 42000 kg 56200 kg 41455 kg 42545 kg

The maximum certificated taxi or ramp mass is that mass to which an aircraft ?

Question 80-24 : A fixed value which is listed in the flight manual a value which varies with airfield temperature and altitude corrections are listed in the flight manual a value which varies only with airfield altitude standard corrections are listed in the flight manual a value which is only affected by the outside air temperature corrections are calculated from data given in the flight manual

The maximum mass to which an aeroplane may be loaded prior to engine start is ?

Question 80-25 : Maximum certificated taxi ramp mass maximum regulated taxi ramp mass maximum certificated take off mass maximum regulated take off mass

The zero fuel mass and the dry operating mass ?

Question 80-26 : Differ by the value of the traffic load mass are the same value differ by the sum of the mass of usable fuel plus traffic load mass differ by the mass of usable fuel

A revenue flight is planned for the transport aeroplane take off mass is not ?

Question 80-27 : 4530 kg 5400 kg 6350 kg 3185 kg

The empty mass of an aeroplane is given as 44800 kg .operational items ?

Question 80-28 : 18400 kg 20700 kg 23000 kg 19460 kg

The maximum zero fuel mass is a structural limiting mass it is made up of the ?

Question 80-29 : Traffic load traffic load unuseable fuel and crew standard mass unuseable and crew standard mass traffic load and crew standard mass

The take off mass of an aeroplane is 141000 kg .total fuel on board is 63000 kg ?

Question 80-30 : 79000 kg 78000 kg 93000 kg 65200 kg

'standard mass' as used in the computation of passenger load establish the mass ?

Question 80-31 : 35 kg irrespective of age provided they occupy a seat 35 kg only if they are over 2 years old and occupy a seat 35 kg for children over 2 years occupying a seat and 10 kg for infants less than 2 years not occupying a seat 35 kg for children over 2 years occupying a seat and 10 kg for infants less than 2 years occupying a seat

The maximum certificated take off mass is ?

Question 80-32 : A structural limit which may not be exceeded for any take off a take off limiting mass which is affected by the aerodrome altitude and temperature a take off limiting mass which is governed by the gradient of climb after reaching v2 limited by the runway take off distance available it is tabulated in the flight manual

For a particular aeroplane the structural maximum mass without any fuel on ?

Question 80-33 : A fixed value which is stated in the aeroplane operating manual a variable value which is governed by the pcn and acn a variable value which is governed by the traffic load carried a fixed value which will limit the amount of fuel carried

On an aeroplane with a seating capacity of more than 30 it is decided to use ?

Question 80-34 : 84 kg 88 kg 76 kg 83 kg

The standard mass for a child is ?

Question 80-35 : 35 kg for all flights 35 kg for holiday charters and 38 kg for all other flights 38 kg for all flights 30 kg for holiday charters and 35 kg for all other flights

On an aeroplane with 20 or more seats engaged on an inter continental flight ?

Question 80-36 : 15 kg per passenger 13 kg per passenger 14 kg per passenger 11 kg per passenger

The following data applies to a planned flight .dry operating mass 34900 kg ?

Question 80-37 : 12700 kg 13230 kg 15200 kg 10730 kg

In determining the dry operating mass of an aeroplane it is common practice to ?

Question 80-38 : Flight crew 85 kg cabin crew 75 kg each these are inclusive of a hand baggage allowance flight crew 85 kg cabin crew 75 kg each these do not include a hand baggage allowance flight crew male 88 kg female 75 kg cabin crew 75 kg each these include an allowance for hand baggage flight crew male 88 kg female 75 kg cabin crew 75 kg each these do not include an allowance for hand baggage

The medium range jet transport aeroplane is to operate a flight carrying the ?

Question 80-39 : 14470 kg 13655 kg 16080 kg 15815 kg

An aircraft is to depart from an airfield at a take off mass of 302550 kg .fuel ?

Question 80-40 : 141100 kg 19650 kg 121450 kg 39105 kg