The JAA
IR Flight Planning and Monitoring
test bank contains questions pertaining to
033-06-01 Extraction of data
. The following list contains only a relatively small percentage of the pertinent
questions. Our software, which you are free to download now at no cost, will
generally contain a much more complete set of questions associated with this
test bank. This list is intended only to familiarize you in a general way with
the questions of the
Flight Planning and Monitoring
test bank.
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That said, while the following questions are intended
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We do not update this website as often as we update our software, which will
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if you need to actually study for your test, instead of using the list below,
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| Sample Questions
from the JAA IR
Flight Planning and Monitoring
Test Bank |
- When calculating the fuel required to carry out a given flight, one must take into account: 1. the wind2. foreseeable airborne delays3. other weather forecasts4. any foreseeable conditions which may delay landingThe combination of correct statements is:
- Given: Brake release mass= 40000kg, Temperature= ISA+20°C, Trip distance= 150 Nautical Air Miles (NAM)Find the SHORT DISTANCE CRUISE ALTITUDE for the twin jet aeroplane.
- Given: Twin jet aeroplane, zero fuel mass 50000kg, landing mass at alternate 52000kg, final reserve fuel 2000kg, alternate fuel 1000kg, Flight to destination: Distance 720NM, True course 030°, W/V 340°/30kt, Long range cruise, FL330, OAT -30°CFind: Estimated trip fuel and time with simplified flight planning
- The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg distance: 3500NMFlight level FL310, true airspeed: 450ktHeadwind component at this level: 55ktInitially planned take-off mass (without extra fuel on board): 180000kgFuel price: 0.27$/l at destinationThe commander may carry a fuel quantity of 8000kg in addition to that which is necessary.For this fuel transport operation to be cost effective, the maximum fuel price at departure must be:
- Given:Maximum allowable take-off mass: 64400kgMaximum landing mass: 56200kgMaximum zero fuel mass: 53000kgDry operating mass: 35500kgTraffic load: 14500kgMinimum Take-off fuel: 7400kgFind: Maximum allowable take-off fuel
- The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg distance: 2700NMFlight level FL310, true airspeed: 470ktTailwind component at this level: 35ktInitially planned take-off mass (without extra fuel on board): 180000kgFuel price: 0.28 Euro/l at departure; 0.26 Euro/l at destinationTo maximise savings, the commander chooses to carry extra fuel in addition to that which is necessaryUsing the annex, the optimum quantity of fuel which should be carried in addition to the prescribed quantity is:
- For flight planning purposes the landing mass at alternate is taken as:
- Given: brake release mass 57500kgtemperature ISA-10°C; headwind component 16ktinitial FL280Find: still air distance (NAM) and ground distance (NM) for the climb
- Given: estimated take-off mass 57000kg; still air distance 150NAM; outside air temperature (OAT) ISA-10K; cruise at 0.74 Mach.Find: cruise altitude and expected true airspeed
- Planning a flight from Paris-CDG to London-LHR for a twin-jet aeroplane. Preplanning:Powersetting: Mach 0.74FL280, W/V 280°/40ktThe landing mass in the fuel graph is 50000kgThe trip distance used for calculation is 200NMFind the estimated trip fuel.
- Given: long range cruise; OAT -45°C in FL350; mass at the beginning of the leg 40000kg; mass at end of the leg 39000kg. Find: true airspeed (TAS) at the end of the leg and the leg distance (NAM).
- On an ATC flightplan, the letter "Y" is used to indicate that the flight is carried out under the following flight rules:
- Given flight details:Distance: 1825 NMAll engines TAS: 300 ktOne engine inoperative TAS: 250 ktW/C outbound: 10 kt headW/C Inbound: 20 kt headWhat is the time and distance to all engines operating PET?
- If CAS is 190 kts, Altitude 9000 ft. Temp. ISA - 10° C, True Course (TC) 350° , W/V 320/40, distance from departure to destination is 350 NM, endurance 3 hours, and actual time of departure is 1105 UTC. The Point of Equal Time (PET) is reached at:
- Given flight details:Distance: 1825 NMAll engines TAS: 300 ktOne engine inoperative TAS: 250 ktW/C outbound: 10 kt headW/C Inbound: 20 kt headWhat is the time and distance to the one engine inoperative PET?
- INTEGRATED RANGE curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is:
- Find the distance to the POINT OF SAFE RETURN (PSR), given:Maximum useable fuel: 15000 kgMinimum reserve fuel: 3500 kgOUTBOUND: TAS 425 kt, head wind component 30 kt, fuel flow 2150 kg/hRETURN: TAS 430 kt, tailwind component 20 kt, fuel flow 2150 kg/h
- A twin engine aircraft is to fly from A to B:Track 245° (T)Distance 830 NMW/V 310/402 engine TAS 280 Kts1 engine TAS 220 KtsIf the ETD is 0800 Z the ETA at the 1 ENG INOP PET (CP) is:
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Flight Planning and Monitoring
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