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The loading for a flight is shown in the loadsheet with the following data ? [ Mandatory landing ]

Question 67-1 : 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

Img143.946000/93000 = 10 17 m exemple 167 Landing cg is out of limits at 10.17 m aft of datum.Landing cg is out of limits at 10.17 m aft of datum.

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

Question 67-2 : 75000 kg and 17200 kg 75000 kg and 20000 kg 77200 kg and 19400 kg 77200 kg and 22200 kg

Img144.traffic load is 17200 kg .maximum take off mass = dry operating mass + fuel at take off + traffic load.maximum take off mass = 48000 + 9800 + 17200 = 75000 kg exemple 171 75000 kg and 17200 kg.75000 kg and 17200 kg.

Dry operating mass is the mass of the aircraft less ?

Question 67-3 : Usable fuel and traffic load usable fuel traffic load potable water and lavatory chemicals usable fuel potable water and lavatory chemicals

Please download the following document used as a reference at the exam .pdf/031 mass definitions pdf exemple 175 Usable fuel and traffic load.Usable fuel and traffic load.

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

Question 67-4 : Dry operating mass zero fuel mass landing mass maximum zero fuel mass

exemple 179 Dry operating mass.Dry operating mass.

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

Question 67-5 : The operator the commander the authority of the state of registration the person compiling the weighing schedule

exemple 183 The operator.The operator.

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

Question 67-6 : Usable fuel and traffic load the traffic load useful fuel crew and crew baggage

Please download the following document used as a reference at the exam ./pdf/031 mass definitions pdf exemple 187 Usable fuel and traffic load.Usable fuel and traffic load.

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

Question 67-7 : 42000 kg 56200 kg 41455 kg 42545 kg

Dry operating mass = take off mass traffic load usable fuel .dry operating mass = 66700 kg 14200 kg 10500 kg = 42000 kg..dry operating mass = the total mass of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load .this mass includes items such as .+ crew and crew baggage .+ catering and removable passenger service equipment food beverages potable water lavatory chemicals etc .+ special operational equipment e g stretchers rescue hoist cargo sling exemple 191 42000 kg.42000 kg.

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

Question 67-8 : 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

exemple 195 A fixed value which is listed in the flight manual.A fixed value which is listed in the flight manual.

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

Question 67-9 : Maximum certificated taxi ramp mass maximum regulated taxi ramp mass maximum certificated take off mass maximum regulated take off mass

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf.this is takeoff mass plus taxi fuel i e weight of loaded aircraft before starting the engines exemple 199 Maximum certificated taxi (ramp) mass.Maximum certificated taxi (ramp) mass.

The zero fuel mass and the dry operating mass ?

Question 67-10 : 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

Please download the following document used as a reference at the exam ./pdf/031 mass definitions pdf exemple 203 Differ by the value of the traffic load mass.Differ by the value of the traffic load mass.

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

Question 67-11 : 4530 kg 5400 kg 6350 kg 3185 kg

Performance limited landing mass 55000 kg.dry operating mass 34930 kg.fuel at landing = 1200+1600 = 2800 kg.traffic load minus the cargo load = 130x84 + 130x14 = 12740 kg.so the amount of cargo you can still carry is = 55000 34930+2800+12740 = 55000 50470 = 4530 kg exemple 207 4530 kg.4530 kg.

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

Question 67-12 : 18400 kg 20700 kg 23000 kg 19460 kg

Maximum traffic load = maximum zero fuel mass empty mass operational items.maximum traffic load = 65500 44800 2300 = 18400 kg exemple 211 18400 kg.18400 kg.

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

Question 67-13 : Traffic load traffic load unuseable fuel and crew standard mass unuseable and crew standard mass traffic load and crew standard mass

Zero fuel mass the dry operating mass plus traffic load but excluding fuel exemple 215 Traffic load.Traffic load.

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

Question 67-14 : 79000 kg 78000 kg 93000 kg 65200 kg

The zero fuel mass includes unusable fuel .usable fuel on board = 63000 kg 1000 kg = 62000 kg .take off mass usable fuel = 141000 kg 62000 kg = 79000 kg exemple 219 79000 kg.79000 kg.

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

Question 67-15 : 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

Eu ops . 153 exemple 223 35 kg irrespective of age provided they occupy a seat.35 kg irrespective of age provided they occupy a seat.

The maximum certificated take off mass is ?

Question 67-16 : 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

The certificated take off mass is a structural limit whereas all other answers refer to a performance climb respectively field limited take off mass the structural limit is a fixed value which shall never be exceeded to avoid any damage to the aircraft structure the other limitations can vary depending on the performance and environment .maximum certified mass = structural limitation.maximum regulated mass = structural and performance limitation exemple 227 A structural limit which may not be exceeded for any take-off.A structural limit which may not be exceeded for any take-off.

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

Question 67-17 : 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

exemple 231 A fixed value which is stated in the aeroplane operating manual.A fixed value which is stated in the aeroplane operating manual.

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

Question 67-18 : 84 kg 88 kg 76 kg 83 kg

Eu ops . 153 exemple 235 84 kg.84 kg.

The standard mass for a child is ?

Question 67-19 : 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

Eu ops . 153 exemple 239 35 kg for all flights.35 kg for all flights.

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

Question 67-20 : 15 kg per passenger 13 kg per passenger 14 kg per passenger 11 kg per passenger

Eu ops 1 620 mass values for passengers and baggage. . f mass values for baggage.1 where the total number of passenger seats available on the aeroplane is 20 or more the standard mass values given in table 3 are applicable for each piece of checked baggage .for aeroplanes with 19 passenger seats or less the actual mass of checked baggage determined by weighing must be used . 155

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

Question 67-21 : 12700 kg 13230 kg 15200 kg 10730 kg

Create a limitation table . 154.3700 kg + trip fuel 8600 kg + taxy fuel 400 kg = 12700 kg may be safely loaded exemple 247 12700 kg.12700 kg.

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

Question 67-22 : 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

Eu ops 1 615 mass values for crew. a an operator shall use the following mass values to determine the dry operating mass .1 actual masses including any crew baggage or.2 standard masses including hand baggage of 85 kg for flight crew members and 75 kg for cabin crew members or.3 other standard masses acceptable to the authority .b an operator must correct the dry operating mass to account for any additional baggage the position of this additional baggage must be accounted for when establishing the centre of gravity of the aeroplane exemple 251 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 are inclusive of a hand baggage allowance.

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

Question 67-23 : 14470 kg 13655 kg 16080 kg 15815 kg

Performance limited take off mass 60 400 kg and landing airfield is not performance limited .mass of fuel at take off = performance limited take off mass dry operating mass + traffic load .mass of fuel at take off = 60400 kg 34930 kg + 11000 kg = 14470 kg .departure airfield performance limited take off mass is 60 400 kg this is the maximum allowing mass at take off and the question states ' aeroplane is to operate a flight carrying the maximum possible fuel load' .our ramp mass will be 60 400 kg + 715 kg = 61115 kg exemple 255 14470 kg.14470 kg.

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

Question 67-24 : 141100 kg 19650 kg 121450 kg 39105 kg

Useful load = take off mass dry operating mass.useful load = 302550 kg 161450 kg = 141100 kg exemple 259 141100 kg.141100 kg.

Conversion of fuel volume to mass ?

Question 67-25 : May be done by using standard fuel density values as specified in the operations manual if the actual fuel density is not known may be done by using standard fuel density values as specified in easa air ops must be done by using actual measured fuel density values must be done using fuel density values of 0 79 for jet a1 and 0 76 for jet a2 as specified in easa air ops

exemple 263 May be done by using standard fuel density values as specified in the operations manual, if the actual fuel density is not known.May be done by using standard fuel density values as specified in the operations manual, if the actual fuel density is not known.

Standard masses may be used for the computation of mass values for baggage if ?

Question 67-26 : Has 20 or more seats has 6 or more seats has 30 or more seats is carrying 30 or more passengers

Eu ops 1 620 mass values for passengers and baggage. . f mass values for baggage.1 where the total number of passenger seats available on the aeroplane is 20 or more the standard mass values given in table 3 are applicable for each piece of checked baggage for aeroplanes with 19 passenger seats or less the actual mass of checked baggage determined by weighing must be used . 155 exemple 267 Has 20 or more seats.Has 20 or more seats.

A jet transport has the following structural limits . maximum ramp mass 63 060 ?

Question 67-27 : 16 370 kg 17 070 kg 16 570 kg 16 430 kg

Create a limitation table . 156.anything above 16370 kg will therefore exceed zfm but will keep the other three within limits so that is your answer exemple 271 16 370 kg.16 370 kg.

A flight has been made from london to valencia carrying minimum fuel and ?

Question 67-28 : 14 331 kg 13 240 kg 16 770 kg 9 830 kg

Fuel at ramp 20100 litres x 0 79 kg/l = 15879 kg .fuel at take off 15879 kg 250 kg of taxi fuel = 15629 kg.fuel at landing 15629 kg 5990 kg = 9639 kg .maximum traffic load = maximum landing mass dry operating mass remaining fuel at landing in london .maximum traffic load = 58900 kg 34930 kg 9639 kg = 14331 kg exemple 275 14 331 kg.14 331 kg.

The term 'useful load' as applied to a aircraft includes ?

Question 67-29 : Traffic load plus useable fuel the revenue earning portion of traffic load only traffic load only the revenue earning portion of traffic load plus useable fuel

exemple 279 Traffic load plus useable fuel.Traffic load plus useable fuel.

An aeroplane is performance limited to a landing mass of 54230 kg .the dry ?

Question 67-30 : 29280 kg 17080 kg 12200 kg 10080 kg

Take off mass = dry operating mass + useful load.64280 = 35000 + useful load.useful load = 64280 35000.useful load = 29280 kg exemple 283 29280 kg.29280 kg.

For the medium range transport aeroplane from the loading manual determine the ?

Question 67-31 : 11348 litres 8850 litres 11646 litres 5674 litres

The question states 'determine the maximum total volume of fuel which can be loaded into the main wing tanks' .if you use mass you will get 11646 litres 9084 kg / 0 78 = 11646 litres and it will not fit in the tanks because main tanks volume in litres is 2998 us gallons 1499 + 1499 .2998 usg x 3 7854 l/usg = 11348 litres for a mass of 11348 litres x 0 78 = 8851 kg exemple 287 11348 litres.11348 litres.

The flight preparation of a turbojet aeroplane provides the following data ?

Question 67-32 : 54 000 kg 55 000 kg 55 500 kg 61 500 kg

Img157 exemple 291 54 000 kg.54 000 kg.

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

Question 67-33 : 32 100 kg 40 400 kg 32 900 kg 18 900 kg

Img158 exemple 295 32 100 kg.32 100 kg.

The dry operating mass of an aircraft is 2000 kg .the maximum take off mass ?

Question 67-34 : 1000 kg 950 kg 1500 kg 1450 kg

Traffic load is the total mass of passengers baggage and cargo including any non revenue load .it means usable fuel is not a part of the 'traffic load' .traffic load = maximum take off mass dry operating mass + fuel on board at take off .traffic load = 3500 2000 + 500 = 1000 kg exemple 299 1000 kg.1000 kg.

The basic empty mass of an aircraft is 30000 kg the masses of the following ?

Question 67-35 : 30 665 kg 30 300 kg 38 300 kg 30 785 kg

The dry operating mass is = basic empty mass + standard items.the basic empty mass includes unuseable fuel .dry operating mass = 30000 + 300 + 365 = 30665 kg .the dom includes unusable fuel since unusable fuel is a part of basic empty mass .dry operating mass = the total mass of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load .this mass includes items such as .+ crew and crew baggage .+ catering and removable passenger service equipment food beverages potable water lavatory chemicals etc .+ special operational equipment e g stretchers rescue hoist cargo sling exemple 303 30 665 kg.30 665 kg.

By adding to the basic empty mass the following fixed necessary equipment for a ?

Question 67-36 : Dry operating mass take off mass zero fuel mass landing mass

Please download the following document used as a reference at the exam ./pdf/031 mass definitions pdf exemple 307 Dry operating mass.Dry operating mass.

An aircraft dry operating mass is 3000 kg the maximum take off landing and zero ?

Question 67-37 : 1600 kg 1550 kg 2200 kg 2150 kg

Maximum traffic load = 5200 kg 600 kg at take off 3000 kg = 1600 kg exemple 311 1600 kg.1600 kg.

Given .maximum structural take off mass 8350 kg.maximum structural landing mass ?

Question 67-38 : 7000 kg 7780 kg 7790 kg 8350 kg

Fuel on board at landing 90 + 300 + 400 = 790 kg .expected landing mass at destination = zero fuel mass + fuel on board at landing.expected landing mass at destination = 6210 + 790 = 7000 kg exemple 315 7000 kg.7000 kg.

Given .zero fuel mass 6660 kg.trip fuel 990 kg.block fuel 1540 kg.taxi fuel 25 ?

Question 67-39 : 8175 kg 8200 kg 7210 kg 8110 kg

Actual take off mass = zero fuel mass + block fuel taxi fuel.actual take off mass = 6660 + 1540 25 = 8175 kg exemple 319 8175 kg.8175 kg.

Given .zero fuel mass 4920 kg.trip fuel 880 kg.block fuel 1330 kg.taxi fuel 25 ?

Question 67-40 : 6225 kg 6250 kg 6810 kg 6360 kg

Actual take off mass = zero fuel mass + block fuel taxi fuel.actual take off mass = 4920 + 1330 25 = 6225 kg exemple 323 6225 kg.6225 kg.


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