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 ?
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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 ?
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 kgMaximum Landing Mass 58 900 kgMaximum ?
The following data extracted from an aeroplane's loading manifest performance limited take off mass 93500 kgexpected landing mass at destination 81700 kgmaximum certificated landing mass 86300 kgfuel on board 16500 kgduring flight a diversion made to an en route alternate which not 'performance limite landing fuel remaining at landing 10300 kg the landing mass Is 873 kg excess structural stress could result. Fuel on board fuel remaining at landing = 16500 kg 10300 kg = 6200 kg we only have one mass given take off performance limited take off mass thus landing mass will be 93500 kg 6200 kg = 87300 kg structural stress could result (maximum certificated landing mass 86300 kg). 
With respect to multi engine piston powered aeroplane determine ramp mass lbs in following conditions basic empty mass 3210 lbsbasic arm 88 5 inchesone pilot 160 lbsfront seat passenger 200 lbscentre seat passengers 290 lbsone passenger rear seat 110 lbsbaggage in zone 1 100 lbsbaggage in zone 4 50 lbsblock fuel 100 us gal trip fuel 55 us gal fuel start up and taxi included in block fuel 3 us gal fuel density 6 lbs/us gal 200 Is 873 kg excess structural stress could result. 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. 
The crew of a transport aeroplane prepares a flight using following data dry operating mass 90 000 kg block fuel 30 000 kg taxi fuel 800 kg maximum take off mass 145 000 kgthe traffic load available this flight Is 873 kg excess structural stress could result. 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 take off 800 kg of fuel taxi assumed to have been used. 
Determine zero fuel mass the following single engine aeroplane given standard empty mass 1799 lbspilot + front seat passenger 300 lbscargo mass 350 lbsblock fuel 60 gal trip fuel 35 gal fuel density 6 lbs/gal Is 873 kg excess structural stress could result. 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. Question 64-8
Given standard empty mass 1764 lbsoptional equipment 35 lbspilot + front seat passenger 300 lbscargo mass 350 lbsblock fuel 60 gal trip fuel 35 gal taxi fuel 1 7 gal fuel density 6 lbs/galdetermine expected landing mass Is 873 kg excess structural stress could result. Take off mass = 1764 + 35 + 300 + 350 + (6x(60 1 7)= 2799 lbs expected landing mass = 2799 (6 x 35) = 2589 lbs. Question 64-9
The take off mass of an aeroplane 66700 kg which includes a traffic load of 12500 kg and a usable fuel load of 10200 kg if standard mass the crew 545 kg dry operating mass Is 873 kg excess structural stress could result. Dry operating mass = take off mass (traffic load usable fuel) dry operating mass = 66700 kg (12500 kg + 10200 kg) = 44000 kg. Question 64-10
The take off mass of an aeroplane 8600 kg which includes a traffic load of 1890 kg and a usable fuel load of 1230 kg if standard mass the crew 190 kg dry operating mass Is 873 kg excess structural stress could result. 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 a specific type of operation excluding all usable fuel traffic load this mass includes items such as + crew crew baggage + catering removable passenger service equipment (food beverages potable water lavatory chemicals etc ) + special operational equipment (e g stretchers rescue hoist cargo sling). Question 64-11
The loading a flight shown in loadsheet with following data applying to aeroplane maximum take off mass 150 000 kgmaximum landing mass 140 000 kgcentre of gravity cg limit forward 10 5 m aft of datumaft 13 0 m aft of datumestimated trip fuel 55 000 kg 205 Landing cg out of limits at 7 m aft of datum. 946000/93000 = 10 17 m. Question 64-12
Given an aeroplane with maximum structural landing mass 68000 kgmaximum zero fuel mass 70200 kgmaximum structural take off mass 78200 kgdry operating mass 48000 kgscheduled trip fuel 7000 kg and reserve fuel 2800 kgassuming performance limitations are not restricting maximum permitted take off mass and maximum traffic load are respectively Landing cg out of limits at 7 m aft of datum. traffic load 17200 kg maximum take off mass = dry operating mass + fuel at take off + traffic load maximum take off mass = 48000 + 9800 + 17200 = 75000 kg. Question 64-13
Dry operating mass the mass of aircraft less Usable fuel traffic load. Please download following document used as a reference at exam pdf/031_mass_definitions pdf. Question 64-14
The total mass of aircraft including crew crew baggage plus catering and removable passenger equipment plus potable water and lavatory chemicals but excluding usable fuel and traffic load referred to as Usable fuel traffic load. Please download following document used as a reference at exam pdf/031_mass_definitions pdf. Question 64-15
The responsibility determination of mass of 'operating item and 'crew member included within dry operating mass lies with Usable fuel traffic load. Please download following document used as a reference at exam pdf/031_mass_definitions pdf. Question 64-16
The dry operating mass the total mass of aircraft ready a specific type of operation but excluding Usable fuel traffic load. Please download following document used as a reference at exam /pdf/031_mass_definitions pdf. Question 64-17
The take off mass of an aeroplane 66700 kg which includes a traffic load of 14200 kg and a usable fuel load of 10500 kg if standard mass the crew 545 kg dry operating mass Usable fuel traffic load. 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 a specific type of operation excluding all usable fuel traffic load this mass includes items such as + crew crew baggage + catering removable passenger service equipment (food beverages potable water lavatory chemicals etc ) + special operational equipment (e g stretchers rescue hoist cargo sling). Question 64-18
The maximum certificated taxi or ramp mass that mass to which an aircraft may be loaded prior to engine start it A fixed value which listed in flight manual. 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 a specific type of operation excluding all usable fuel traffic load this mass includes items such as + crew crew baggage + catering removable passenger service equipment (food beverages potable water lavatory chemicals etc ) + special operational equipment (e g stretchers rescue hoist cargo sling). Question 64-19
The maximum mass to which an aeroplane may be loaded prior to engine start Maximum certificated taxi (ramp) mass. Please download following document used as a reference at exam /pdf/031_mass_definitions pdf this takeoff mass plus taxi fuel i e weight of loaded aircraft before starting engines. Question 64-20
The zero fuel mass and dry operating mass Differ the value of traffic load mass. Please download following document used as a reference at exam /pdf/031_mass_definitions pdf. Question 64-21
A revenue flight planned the transport aeroplane take off mass not airfield limited the following data applies dry operating mass 34930 kgperformance limited landing mass 55000 kgfuel on board at ramp taxi fuel 350 kg trip fuel 9730 kg contingency and final reserve fuel 1200 kg alternate fuel 1600 kgpassengers on board 130standard mass each passenger 84 kgbaggage per passenger 14 kgtraffic load maximum possible use loading manual provided and above data determine maximum cargo load that may be carried without exceeding limiting aeroplane landing mass 216 Differ the value of traffic load mass. Performance limited landing mass 55000 kg dry operating mass 34930 kg fuel (at landing) = 1200+1600 = 2800 kg traffic load (minus cargo load) = 130x84 + 130x14 = 12740 kg so amount of cargo you can still carry = 55000 (34930+2800+12740) = 55000 50470 = 4530 kg. Question 64-22
The empty mass of an aeroplane given as 44800 kg operational items including crew standard mass of 1060 kg are 2300 kg if maximum zero fuel mass given as 65500 kg maximum traffic load which could be carried Differ the value of traffic load mass. Maximum traffic load = maximum zero fuel mass empty mass operational items maximum traffic load = 65500 44800 2300 = 18400 kg. Question 64-23
The maximum zero fuel mass a structural limiting mass it made up of aeroplane dry operational mass plus Differ the value of traffic load mass. Zero fuel mass the dry operating mass plus traffic load but excluding fuel. Question 64-24
The take off mass of an aeroplane 141000 kg total fuel on board 63000 kg including 14000 kg reserve fuel and 1000 kg of unusable fuel the traffic load 12800 kg the zero fuel mass Differ the value of traffic load mass. 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. Question 64-25
'standard mas as used in computation of passenger load establish mass of a child as 35 kg irrespective of age provided they occupy a seat. 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. Question 64-26
The maximum certificated take off mass A structural limit which may not be exceeded any take off. The certificated take off mass a structural limit whereas all other answers refer to a performance climb respectively field limited take off mass the structural limit a fixed value which shall never be exceeded to avoid any damage to aircraft structure the other limitations can vary depending on performance environment maximum certified mass = structural limitation maximum regulated mass = structural and performance limitation. Question 64-27
For a particular aeroplane structural maximum mass without any fuel on board other than unusable quantities A fixed value which stated in aeroplane operating manual. The certificated take off mass a structural limit whereas all other answers refer to a performance climb respectively field limited take off mass the structural limit a fixed value which shall never be exceeded to avoid any damage to aircraft structure the other limitations can vary depending on performance environment maximum certified mass = structural limitation maximum regulated mass = structural and performance limitation. Question 64-28
On an aeroplane with a seating capacity of more than 30 it decided to use standard mass values computing total mass of passengers if flight not a holiday charter mass value which may be used an adult A fixed value which stated in aeroplane operating manual. The certificated take off mass a structural limit whereas all other answers refer to a performance climb respectively field limited take off mass the structural limit a fixed value which shall never be exceeded to avoid any damage to aircraft structure the other limitations can vary depending on performance environment maximum certified mass = structural limitation maximum regulated mass = structural and performance limitation. Question 64-29
The standard mass a child A fixed value which stated in aeroplane operating manual. The certificated take off mass a structural limit whereas all other answers refer to a performance climb respectively field limited take off mass the structural limit a fixed value which shall never be exceeded to avoid any damage to aircraft structure the other limitations can vary depending on performance environment maximum certified mass = structural limitation maximum regulated mass = structural and performance limitation. Question 64-30
On an aeroplane with 20 or more seats engaged on an inter continental flight 'standard mas which may be used passenger baggage A fixed value which stated in aeroplane operating manual. Eu ops 1 620 mass values passengers baggage (f) mass values baggage 1 where total number of passenger seats available on aeroplane 20 or more standard mass values given in table 3 are applicable each piece of checked baggage for aeroplanes with 19 passenger seats or less actual mass of checked baggage determined weighing must be used . Question 64-31
The following data applies to a planned flight dry operating mass 34900 kg performance limited take off mass 66300 kg performance limited landing mass 55200 kg maximum zero fuel mass 53070 kg fuel required at ramp taxy fuel 400 kg trip fuel 8600 kg contingency fuel 430 kg alternate fuel 970 kg holding fuel 900 kgtraffic load 16600 kg fuel costs at departure airfield are such that it decided to load maximum fuel quantity possible the total fuel which may be safely loaded prior to departure A fixed value which stated in aeroplane operating manual. Create a limitation table 3700 kg + trip fuel 8600 kg + taxy fuel 400 kg = 12700 kg may be safely loaded. Question 64-32
In determining dry operating mass of an aeroplane it common practice to use 'standard mas values crew these values are Flight crew 85 kg cabin crew 75 kg each these are inclusive of a hand baggage allowance. Eu ops 1 615 mass values crew (a) an operator shall use following mass values to determine dry operating mass 1 actual masses including any crew baggage or 2 standard masses including hand baggage of 85 kg flight crew members 75 kg cabin crew members or 3 other standard masses acceptable to authority b) an operator must correct dry operating mass to account any additional baggage the position of this additional baggage must be accounted when establishing centre of gravity of aeroplane. Question 64-33
The medium range jet transport aeroplane to operate a flight carrying maximum possible fuel load departure airfield performance limited take off mass 60 400 kg landing airfield not performance limiteddry operating mass 34930 kgfuel required flight taxi fuel 715 kgtrip fuel 8600 kgcontingency and final reserve fuel 1700 kgalternate fuel 1500 kgadditional reserve 400 kgtraffic load flight 11000 kgusing following data as appropriate determine mass of fuel on board at start of take off 217 Flight crew 85 kg cabin crew 75 kg each these are inclusive of a hand baggage allowance. Performance limited take off mass 60 400 kg landing airfield 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 60 400 kg this the maximum allowing mass at take off the question states ' aeroplane to operate a flight carrying maximum possible fuel loa our ramp mass will be 60 400 kg + 715 kg = 61115 kg. Question 64-34
An aircraft to depart from an airfield at a take off mass of 302550 kg fuel on board at take off including contingency and alternate of 19450 kg 121450 kg the dry operating mass 161450 kg the useful load will be Flight crew 85 kg cabin crew 75 kg each these are inclusive of a hand baggage allowance. Useful load = take off mass dry operating mass useful load = 302550 kg 161450 kg = 141100 kg. Question 64-35
Conversion of fuel volume to mass May be done using standard fuel density values as specified in operations manual if actual fuel density not known. Useful load = take off mass dry operating mass useful load = 302550 kg 161450 kg = 141100 kg. Question 64-36
Standard masses may be used the computation of mass values baggage if aircraft Has 2 or more seats. Eu ops 1 620 mass values passengers baggage (f) mass values baggage 1 where total number of passenger seats available on aeroplane 20 or more standard mass values given in table 3 are applicable each piece of checked baggage aeroplanes with 19 passenger seats or less actual mass of checked baggage determined weighing must be used . Question 64-37
A jet transport has following structural limits maximum ramp mass 63 060 kg maximum take off mass 62 800 kg maximum landing mass 54 900 kg maximum zero fuel mass 51 300 kgthe aeroplane's fuel loaded accordance with following requirements taxi fuel 400 kg trip fuel 8400 kg contingency and final reserve fuel 1800 kg alternate fuel 1100 kgif dry operating mass 34930 kg determine maximum traffic load that can be carried on flight if departure and landing airfields are not performance limited Has 2 or more seats. Create a limitation table anything above 16370 kg will therefore exceed zfm but will keep other three within limits so that your answer. Question 64-38
A flight has been made from london to valencia carrying minimum fuel and maximum traffic load on return flight fuel tanks in aeroplane are to be filled to capacity with a total fuel load of 20100 litres at a fuel density of 0 79 kg/l the following are 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 kgthe performance limited take off mass at valencia 67 330 kg the landing mass at london not performance limited dry operating mass 34 930 kgtrip fuel valencia to london 5 990 kgtaxi fuel 250 kgthe maximum traffic load that can be carried from valencia will be Has 2 or more seats. 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. Question 64-39
The term 'useful loa as applied to a aircraft includes Traffic load plus useable fuel. 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. Question 64-40
An aeroplane performance limited to a landing mass of 54230 kg the dry operating mass 35000 kg and zero fuel mass 52080 kg if take off mass 64280 kg useful load Traffic load plus useable fuel. Take off mass = dry operating mass + useful load 64280 = 35000 + useful load useful load = 64280 35000 useful load = 29280 kg.
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