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The term 'maximum zero fuel mass' consist of ? [ Exam pilot ]

Question 70-1 : The maximum permissible mass of an aeroplane with no usable fuel the maximum mass authorized for a certain aeroplane not including traffic load and fuel load the maximum mass authorized for a certain aeroplane not including the fuel load and operational items the maximum mass for some aeroplanes including the fuel load and the traffic load

exemple 170 The maximum permissible mass of an aeroplane with no usable fuel.The maximum permissible mass of an aeroplane with no usable fuel.

The actual 'zero fuel mass' is equal to the ?

Question 70-2 : Dry operating mass plus the traffic load operating mass plus all the traffic load basic empty mass plus the fuel loaded actual landing mass plus trip fuel

exemple 174 Dry operating mass plus the traffic load.Dry operating mass plus the traffic load.

The actual 'take off mass' is equivalent to ?

Question 70-3 : Dry operating mass plus take off fuel and the traffic load actual zero fuel mass plus the traffic load dry operating mass plus the take off fuel actual landing mass plus the take off fuel

exemple 178 Dry operating mass plus take-off fuel and the traffic load.Dry operating mass plus take-off fuel and the traffic load.

With respect to aeroplane loading in the planning phase which of the following ?

Question 70-4 : Lm = tom trip fuel mtom = zfm + full tank fuel mass mzfm = traffic load + dom reserve fuel = tom trip fuel

Landing mass = take off mass trip fuel .'mzfm = traffic load + dom' is not correct to be correct it would have to say 'mzfm = dom + maximum traffic load'

Given an aeroplane with .maximum structural landing mass 125000 kg.maximum zero ?

Question 70-5 : 130500 kg and 26500 kg 130500 kg and 31500 kg 125500 kg and 21500 kg 125500 kg and 26500 kg

Img135.the lowest value is our maximum traffic load 26500 kg .now our maximum permitted take off mass is .maximum zero fuel mass + fuel at take off = 108500 + 22000 = 130500 kg exemple 186 130500 kg and 26500 kg.130500 kg and 26500 kg.

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

Question 70-6 : Less the operating mass plus the operating mass plus the trip fuel mass less the trip fuel mass

Take off mass = operating mass + traffic load. operating mass is 'dom + fuel at take off' .therefore you can say that the traffic load = tom operating mass

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

Question 70-7 : Take off fuel mass ramp fuel mass trip fuel mass ramp fuel mass less the fuel for apu and run up

/pdf/031 mass definitions pdf exemple 194 Take-off fuel mass.Take-off fuel mass.

When establishing the mass breakdown of an aeroplane the empty mass is defined ?

Question 70-8 : 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

Basic empty mass is the mass of an aeroplane plus standard items such as . unusable fuel and other unusable fluids. lubricating oil in engine and auxiliary units. fire extinguishers. pyrotechnics. emergency oxygen equipment. supplementary electronic equipment exemple 198 Standard empty mass plus specific equipment mass plus trapped fluids plus unusable fuel mass.Standard empty mass plus specific equipment mass plus trapped fluids plus unusable fuel mass.

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

Question 70-9 : 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

Please download the following document used as a reference at the exam ./pdf/031 mass definitions pdf exemple 202 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 and traffic load.

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

Question 70-10 : 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

Operational items are the difference between dry operating mass and empty mass .60120 57320 = 2800 kg .the traffic load is the difference between mzfm and dom .72100 60120 = 11980 kg exemple 206 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 11980 kg.

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

Question 70-11 : 21080 kg 21500 kg 21220 kg 20870 kg

Img137.lowest limitation is 21080 kg exemple 210 21080 kg.21080 kg.

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

Question 70-12 : 68400 kg 29600 kg 70700 kg 26900 kg

Useful load = the mass of the aircraft including everything and everyone contained within it at the commencement of take off the total mass of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load ..useful load = take off mass dry operating mass = 132000 kg 63600 kg = 68400kg.for information the dry operating 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 214 68400 kg.68400 kg.

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

Question 70-13 : 78900 kg 78150 kg 18200 kg 17450 kg

Useful load = the mass of the aircraft including everything and everyone contained within it at the commencement of take off the total mass of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load .useful load = take off mass dry operating mass = 137300 kg 58400 kg = 78900 kg .for information the dry operating 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 218 78900 kg.78900 kg.

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

Question 70-14 : 17 840 kg 25 800 kg 18 170 kg 13 950 kg

Create a limitation table . 138.the maximum traffic load that can be carried is 17 840 kg exemple 222 17 840 kg.17 840 kg.

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

Question 70-15 : 17 810 kg 21 170 kg 21 070 kg 20 420 kg

69300 kg t/o mass dom all the fuel you have on board you only used the taxi fuel = 20070 kg avaiable for traffic load..58900 kg landing mass dom the fuel you will have on board you used taxi and trip fuel = 21170 kg avaiable for traffic load..52740 kg zfm dom you don't have fuel = 17810 kg avaiable for traffic load..anything above 17810 kg will therefore exceed zfm but will keep the other two within limits so that is your answer exemple 226 17 810 kg.17 810 kg.

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

Question 70-16 : 17 840 kg 19 500 kg 19 100 kg 19 200 kg

Img138.the maximum traffic load that can be carried is 17 840 kg exemple 230 17 840 kg.17 840 kg.

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

Question 70-17 : 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

Fuel on board fuel remaining at landing = 16500 kg 10300 kg = 6200 kg .we only have one mass given for take off the performance limited take off mass thus the landing mass will be .93500 kg 6200 kg = 87300 kg and structural stress could result maximum certificated landing mass is 86300 kg exemple 234 Is 87300 kg and excess structural stress could result.Is 87300 kg and excess structural stress could result.

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

Question 70-18 : 4720 lbs 4120 lbs 4390 lbs 4372 lbs

You simply have to add .basic empty mass 3210 lbs.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 lbs.baggage in zone 4 50 lbs.block fuel 100 us gal x 6 lbs = 600 lbs. .ramp mass 4720 lbs exemple 238 4720 lbs.4720 lbs.

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

Question 70-19 : 25 800 kg 55 800 kg 25 000 kg 55 000 kg

Traffic load = take off mass dry operating mass fuel .traffic load = 145000 kg 90000 kg 29200 kg .traffic load = 25800 kg .block fuel includes taxi fuel .lined up for take off the 800 kg of fuel for taxi is assumed to have been used

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

Question 70-20 : 2449 lbs 2589 lbs 2659 lbs 2414 lbs

Zero fuel mass = the dry operating mass plus traffic load but excluding fuel .zero fuel mass = basic empty mass + pilot + front seat passenger + cargo mass.zero fuel mass = 1799 + 300 + 350 = 2449 lbs exemple 246 2449 lbs.2449 lbs.

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

Question 70-21 : 2589 lbs 2599 lbs 2472 lbs 2557 lbs

Take off mass = 1764 + 35 + 300 + 350 + 6x 60 1 7 = 2799 lbs.expected landing mass = 2799 6 x 35 = 2589 lbs exemple 250 2589 lbs.2589 lbs.

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

Question 70-22 : 44000 kg 54200 kg 56500 kg 43465 kg

Dry operating mass = take off mass traffic load usable fuel .dry operating mass = 66700 kg 12500 kg + 10200 kg = 44000 kg exemple 254 44000 kg.44000 kg.

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

Question 70-23 : 5480 kg 5290 kg 8410 kg 6710 kg

Dry operating mass = take off mass traffic load usable fuel .dry operating mass = 8600 kg 1890 kg 1230 kg = 5480 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 258 5480 kg.5480 kg.

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

Question 70-24 : 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 262 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 70-25 : 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 266 75000 kg and 17200 kg.75000 kg and 17200 kg.

Dry operating mass is the mass of the aircraft less ?

Question 70-26 : 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 270 Usable fuel and traffic load.Usable fuel and traffic load.

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

Question 70-27 : Dry operating mass zero fuel mass landing mass maximum zero fuel mass

exemple 274 Dry operating mass.Dry operating mass.

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

Question 70-28 : The operator the commander the authority of the state of registration the person compiling the weighing schedule

exemple 278 The operator.The operator.

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

Question 70-29 : 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 282 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 70-30 : 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 286 42000 kg.42000 kg.

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

Question 70-31 : 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 290 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 70-32 : 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 294 Maximum certificated taxi (ramp) mass.Maximum certificated taxi (ramp) mass.

The zero fuel mass and the dry operating mass ?

Question 70-33 : 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 298 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 70-34 : 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 302 4530 kg.4530 kg.

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

Question 70-35 : 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 306 18400 kg.18400 kg.

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

Question 70-36 : 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 310 Traffic load.Traffic load.

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

Question 70-37 : 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 314 79000 kg.79000 kg.

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

Question 70-38 : 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 318 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 70-39 : 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 322 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 70-40 : 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 326 A fixed value which is stated in the aeroplane operating manual.A fixed value which is stated in the aeroplane operating manual.


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