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

Question 67-1 : 1600 kg 1550 kg 2200 kg 2150 kg

Maximum traffic load = 5200 kg 600 kg at take off 3000 kg = 1600 kg exemple 167 1600 kg.1600 kg.

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

Question 67-2 : 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 171 7000 kg.7000 kg.

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

Question 67-3 : 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 175 8175 kg.8175 kg.

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

Question 67-4 : 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 179 6225 kg.6225 kg.

Given.maximum structural take off mass 8600 kg.maximum structural landing mass ?

Question 67-5 : 7340 kg 8310 kg 8325 kg 8600 kg

Fuel on board at landing 110 + 600 + 130 = 840 kg.expected landing mass at destination = zero fuel mass + fuel on board at landing..expected landing mass at destination = 6500 + 840 = 7340 kg exemple 183 7340 kg.7340 kg.

Given.maximum structural take off mass 7400 kg.maximum structural landing mass ?

Question 67-6 : 6625 kg 7385 kg 7400 kg 7135 kg

Fuel on board at landing 110 + 275 + 250 = 635 kg.expected landing mass at destination = zero fuel mass + fuel on board at landing...expected landing mass at destination = 5990 + 635 = 6625 kg exemple 187 6625 kg.6625 kg.

Given.dry operating mass 4920 kg.zero fuel mass 5740 kg.trip fuel 670 kg.take ?

Question 67-7 : 820 kg 2160 kg 1340 kg 2480 kg

Dry operating mass is the total mass of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load.traffic load is the total mass of passengers baggage and cargo including any non revenue load.5740 4920 = 820 kg exemple 191 820 kg.820 kg.

Given.dry operating mass 5320 kg.zero fuel mass 6790 kg.trip fuel 770 kg.take ?

Question 67-8 : 1470 kg 3080 kg 1610 kg 2940 kg

Dry operating mass is the total mass of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load.traffic load is the total mass of passengers baggage and cargo including any non revenue load.6790 5320 = 1470 kg exemple 195 1470 kg.1470 kg.

Given.dry operating mass 5210 kg.zero fuel mass 6230 kg.trip fuel 990 kg.take ?

Question 67-9 : 1020 kg 3390 kg 2370 kg 2980 kg

Dry operating mass is the total mass of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load.traffic load is the total mass of passengers baggage and cargo including any non revenue load.6230 5210 = 1020 kg exemple 199 1020 kg.1020 kg.

Given.zero fuel mass 4770 kg.trip fuel 1040 kg.block fuel 1960 kg.taxi fuel 20 ?

Question 67-10 : 6710 kg 6730 kg 5890 kg 4970 kg

Actual take off mass = zero fuel mass + block fuel taxi fuel..actual take off mass = 4770 + 1960 20 = 6710 kg exemple 203 6710 kg.6710 kg.

Considering only structural limitations on very short legs with minimum take ?

Question 67-11 : Maximum zero fuel mass maximum landing mass maximum take off mass actual landing mass

Maximum zero fuel mass exists to prevent wing bending if too much weight is concentrated in the fuselage then the wings will flex dramatically in flight by placing fuel into the wings the weight is distributed more evenly there is not a concentration of mass in one area .on very short legs with minimum take off fuel it means very low fuel in the wings and no fuel in center tank the traffic load will be limited due to this bending moment at the wing roots exemple 207 maximum zero fuel mass.maximum zero fuel mass.

Basic empty mass is ?

Question 67-12 : A component of dry operating mass the actual take off mass minus traffic load dry operating mass minus fuel load dry operating mass minus traffic load

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf exemple 211 a component of dry operating mass.a component of dry operating mass.

Allowed traffic load is the difference between ?

Question 67-13 : Allowed take off mass and operating mass allowed take off mass and basic empty mass plus trip fuel allowed take off mass and basic empty mass operating mass and basic empty mass

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf exemple 215 allowed take off mass and operating mass.allowed take off mass and operating mass.

The operating mass of an aeroplane is ?

Question 67-14 : The dry operating mass plus the take off fuel mass the empty mass plus the take off fuel mass the empty mass plus crew crew baggage and catering the empty mass plus the trip fuel mass

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf exemple 219 the dry operating mass plus the take-off fuel mass.the dry operating mass plus the take-off fuel mass.

The maximum zero fuel mass is ?

Question 67-15 : A structural limit listed in the flight manual as a fixed value governed by the cg limits governed by the traffic load to be carried tabulated in the flight manual against arguments of airfield elevation and temperature

exemple 223 a structural limit listed in the flight manual as a fixed value.a structural limit listed in the flight manual as a fixed value.

The maximum structural take off mass is ?

Question 67-16 : A 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 vy limited by the take off distance available it is tabulated in the flight manual

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf exemple 227 a limit which may not be exceeded for any take-off.a limit which may not be exceeded for any take-off.

To calculate the allowable take off mass the factors to be taken into account ?

Question 67-17 : Maximum landing mass augmented by the fuel burn maximum landing mass and the fuel on board at take off maximum zero fuel mass and the trip fuel maximum take off mass minus the trip fuel

Maximum landing mass and the trip fuel .correct because you can take off at the mlm plus trip fuel because you would land at mlm in the mlm would be the reserve contingency and diversion fuel.maximum take off mass minus the trip fuel .this is nonsense the mtom minus trip fuel will not give the allowable tom.maximum landing mass and the fuel on board at take off .it can't be the mlm plus take off fuel because this would mean you would land above the mlm as you would only plan to burn the trip fuel thus you would be landing at mlm plus reserve contingency and diversion fuel.maximum zero fuel mass and the trip fuel .this cannot be right because the allowable tom is not the mzfm plus trip fuel but the mzfm plus take off fuel assuming it doesn't exceed the mtom exemple 231 maximum landing mass augmented by the fuel burnmaximum landing mass augmented by the fuel burn

The traffic load is defined as the total mass of ?

Question 67-18 : Passengers baggage and cargo including any non revenue load passengers baggage cargo and usable fuel flight crew passengers baggage cargo and usable fuel crew and passengers excluding any baggage or cargo

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf exemple 235 passengers, baggage and cargo, including any non revenue load.passengers, baggage and cargo, including any non revenue load.

Given.dry operating mass = 38 000 kg.maximum structural take off mass = 72 000 ?

Question 67-19 : 71 300 kg and 23 000 kg 71 300 kg and 25 300 kg 73 000 kg and 24 700 kg 73 000 kg and 27 000 kg

Zfm is the mass of the aeroplane minus all useable fuel .payload is the load we are carrying that earns revenue.payload = maximum zero fuel mass dom..61000 38000 = 23000 kg..maximum allowed take off mass = payload + dom + fuel.23000 + 38000 + 10300 = 71300 kg..we are below the maximum structural take off mass .we will be below the maximum landing mass 71300 8000 = 63300 kg exemple 239 71 300 kg and 23 000 kg.71 300 kg and 23 000 kg.

In relation to an aeroplane the term 'basic empty mass' includes the mass of ?

Question 67-20 : Found in the latest version of the weighing schedule as corrected to allow for modifications found in the flight manual and is inclusive of unusable fuel plus fluids contained in closed systems printed in the loading manual and includes unusable fuel inclusive of an allowance for crew crew baggage and other operating items it is entered in the loading manifest

The 'basic empty mass' is recorded in the weighing schedule not in the flight manual

Prior to departure the medium range twin jet aeroplane is loaded with maximum ?

Question 67-21 : 13090 kg 16470 kg 18040 kg 12840 kg

Question states 'prior to departure the jet is loaded with maximum fuel'.20100 litres = 15680 kg..traffic load possible at take off .67200 kg 34930 kg + 15680 kg = 16590 kg..at landing taxi and trip fuel have been burnt .15680 250 + 9250 = 6180 kg of fuel remains in our aeroplane.traffic load possible at landing .54200 34930 kg + 6180 kg = 13090 kg exemple 247 13090 kg.13090 kg.

The operator of an aircraft equipped with 50 seats uses standard masses for ?

Question 67-22 : The operator should use the individual masses of the passengers or alter the standard masss the operator may use the standard masses for the balance but must correct these for the load calculation the operator is obliged to use the actual masses of each passenger the operator may use the standard masses for the load and balance calculation without correction

Easa air ops.mass values for passengers and baggage . . g on any flight identified as carrying a significant number of passengers whose masses including hand baggage are expected to exceed the standard passenger mass an operator must determine the actual mass of such passengers by weighing or by adding an adequate mass increment exemple 251 the operator should use the individual masses of the passengers or alter the standard masss.the operator should use the individual masses of the passengers or alter the standard masss.

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

Question 67-23 : Is 87300 kg and excess structural stress could result is 87300 kg which is acceptable in this case because this is a diversion and not a normal scheduled landing 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

Fuel on board fuel remaining at landing = 16500 kg 10300 kg = 6200 kg.we only have one mass givent 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 255 is 87300 kg and excess structural stress could result.is 87300 kg and excess structural stress could result.

The following data relates to a planned flight of an aeroplane .dry operational ?

Question 67-24 : 7010 kg 7730 kg 11730 kg 15730 kg

168 exemple 259 7010 kg.7010 kg.

Maximum allowed take off mass limit 37 200kg.dry operating mass 21 600 kg.take ?

Question 67-25 : 585 kg 340 kg 1105 kg 965 kg

Adults = 33 males + 32 females x 84 kg = 5460 kg.children = 5 x 35 kg = 175 kg.passenger load is 5460 kg + 175 kg = 5635 kg.mtom dom + fuel + passenger + baggage .37200 kg 21600 + 8500 + 5635 + 880 = 585 kg exemple 263 585 kg.585 kg.

The take off mass of an aircraft is 8470 kg .total fuel on board is 1600 kg ?

Question 67-26 : 6899 kg 6129 kg 6870 kg 6420 kg

Total fuel on board including unusable fuel = 1600 kg..take off mass minus total fuel on board = 8470 1600 = 6870 kg..unusable fuel is included within the zero fuel mass = 6870 + 29 = 6899 kg exemple 267 6899 kg.6899 kg.

Traffic load is the difference between ?

Question 67-27 : The take off mass and the operating mass the take off mass and the basic empty mass the operating mass and the basic empty mass the take off mass and the basic empty mass plus trip fuel

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf exemple 271 the take-off mass and the operating mass.the take-off mass and the operating mass.

The basic empty mass of an aircraft is 30000 kg .given the following data ?

Question 67-28 : 30900 kg 30930 kg 34630 kg 29100 kg

Dry operating mass = basic empty mass + variable load..dry operating mass = 30000 kg + 300 kg + 600 kg = 30900 kg . unusable fuel is already included in the basic empty mass exemple 275 30900 kg.30900 kg.

Which is true of the aircraft basic empty mass ?

Question 67-29 : It is a component of dry operating mass it is the actual take off mass less traffic load it is dry operating mass minus fuel load it is dry operating mass minus traffic load

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf exemple 279 it is a component of dry operating mass.it is a component of dry operating mass.

The maximum quantity of fuel that can be loaded into an aircraft's tanks is ?

Question 67-30 : 11364 kg 18206 kg 14383 kg 13647 kg

1 us gallon = 3 78 litres 3 785411784 litres.3800 x 3 785411784 x 0 79 = 11363 8 kg exemple 283 11364 kg.11364 kg.

Determine the landing mass for the following single engine aeroplane .given . ?

Question 67-31 : 2599 lbs 2799 lbs 2659 lbs 2449 lbs

Take off mass = 1764 + 35 + 300 + 350 + 6 x 60 = 2809 lbs..expected landing mass = 2809 6 x 35 = 2599 lbs exemple 287 2599 lbs.2599 lbs.

Given.maximum allowable take off mass 64400 kg.maximum landing mass 56200 ?

Question 67-32 : 3000 kg 7000 kg 4000 kg 5600 kg

Take off mass will be 35500 + 14500 + 7400 = 57400 kg.landing mass will be 57400 4900 = 52500 kg..maximum landing mass is 56200 kg so we can add 56200 52500 kg = 3700 kg.last check the maximum zero fuel mass of 53000 kg .35500 + 14500 + 3700 = 53700 kg we are exceeding this limit we need to reduce the additional load by 700 kg.3700 700 = 3000 kg exemple 291 3000 kg.3000 kg.

The traffic load is a part of the ?

Question 67-33 : Zero fuel mass basic empty mass operating mass dry operating mass

Please download the following document used as a reference at the exam./pdf/031 mass definitions pdf exemple 295 zero fuel mass.zero fuel mass.

The si units of running or linear load are ?

Question 67-34 : N/m kg/m kg/m³ n kg/m² kg n/m² lb/ft

exemple 299 n/m, kg/m.n/m, kg/m.

Given .fuel density of 0 78 kg/l dry operating mass = 33500 kg traffic load = ?

Question 67-35 : 17350 kg 21900 kg 17550 kg 22100 kg

Maximum fuel at take off = maximum take off mass dry operating mass + traffic load .maximum fuel at take off = 66200 33500 + 10600 = 22100 kg.this is more than what the fuel tanks can contains.therefore we can fill them full and we will have to remove 200 kg for taxi to know our maximum possible fuel at take off .2500 x 0 78 = 17550 kg .17550 200 = 17350 kg exemple 303 17350 kg.17350 kg.

An aircraft is to depart at an take off mass of 8220 kg .take off fuel ?

Question 67-36 : 1130 kg 1550 kg 1040 kg 2590 kg

8220 1750 4920 420 = 1130 kg exemple 307 1130 kg.1130 kg.

The take off mass of an aircraft is 6700 kg .total fuel on board is 800 kg ?

Question 67-37 : 5919 kg 5900 kg 5681 kg 5000 kg

The total fuel includes 19 kg of unuseable fuel.this unuseable fuel is part of the basic empty mass and therefore part of the dom..tom useable fuel = zfm..6700 800 19 = 5919 kg exemple 311 5919 kg.5919 kg.

The maximum quantity of fuel that can be loaded into an aircraft's tanks is ?

Question 67-38 : 885 kg 1418 kg 858 kg 1011 kg

1120 x 0 79 = 885 kg exemple 315 885 kg.885 kg.

Given . dry operating mass 2800 kg. trip fuel 300 kg. traffic load 400 kg. ?

Question 67-39 : 800 kg 1000 kg 500 kg 700 kg

Zero fuel mass= 2800 + 400 = 3200 kg.useful limitation = the lowest value from the following two values. maximum take off mass 4200 kg. maximum landing mass + trip fuel = 3700 + 300 = 4000 kg this is our 'useful limitation'. maximum fuel load = 4000 3200 = 800 kg exemple 319 800 kg.800 kg.

The dry operating mass of an aircraft is the sum of the basic empty mass + crew ?

Question 67-40 : Operating items traffic load taxi fuel traffic load + usable fuel

exemple 323 operating items.operating items.

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