The JAA
CPL 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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| Sample Questions
from the JAA CPL
Flight Planning and Monitoring
Test Bank |
- Given: Twin jet aeroplane, Ground distance to destination aerodrome is 1600NM,Headwind component 50kt, FL330, Cruise .78Mach, ISA Deviation +20°C and Landing mass 55000kgFind: Fuel required and trip time with simplified flight planning
- "Integrated Range" curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is
- 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: 5ktInitially planned take-off mass (without extra fuel on board): 180000kgFuel price: 0.35$/l at departure; 0.315$/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:
- 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 Euro/l at departure; 0.30 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:
- Planning an IFR-flight from Paris-CDG to London-LHR for the twin jet aeroplane.Given: Estimated take-off mass (TOM) 52000kg, Airport elevation 387ft, FL280,W/V280°/40kt, ISA Deviation -10°C, Average True Course 340°Find: Time to the top of climb (TOC)
- The flight crew of a turbojet aeroplane prepares a flight using the following data: Take-off mass: 210500kgFlight leg ground distance: 2500NMFL330; "Long Range" flight regimeTailwind component at this level: 70ktTotal anti-ice set "ON"Fixed taxi fuel: 500kg; final reserve: 2400kgIgnore alternate fuelThe effects of climb and descent are not corrected for consumption.The quantity of fuel that must be loaded at the parking area is
- Given: flight time from top of climb to the enroute point in FL280 is 48min. Cruise procedure is long rang range cruise (LRC).ISA-5°CTake-off mass 56000kgClimb fuel 1100kgFind: distance in nautical air miles (NAM) for this leg and fuel consumption:
- Given:FL330long range cruiseOAT-63°Cgross mass 50500kgFind: true airspeed (TAS)
- Planning a flight from Paris-CDG to London-LHR for a twin-jet aeroplane. The alternate airport is Manchester. Preplanning:W/V 250°/30ktdistance 160NMAssume the estimated landing mass at alternate is about 50000kg.Find the alternate fuel and the according time.
- Finish the ENDURANCE/FUEL CALCULATION and determine ATC ENDURANCE for a twin jet aeroplane, with the help of the table provided. Contingency fuel is 5% of the planned trip fuel and fuel flow for the extra fuel is 2400kg/h.
- On an ATC flightplan, an aircraft indicated as "H" for "Heavy"
- On an ATC flightplan, to indicate that you will overfly the way-point ROMEO at 120kt at FL085, you write:
- Given:Distance A to B: 3060 NMMean groundspeed OUT: 440 ktMean groundspeed BACK: 540 ktSafe Endurance: 10 hoursThe time to the Point of Safe Return (PSR) is:
- Given:Course A to B 088° (T)Distance 1250 NMMean TAS 330 ktMean W/V 340° /60 ktThe time from A to the PET between A and B is:
- The Wind Component from A to the PET is 45 Kts Headwind and the Wind Component from the PET to B is 60 Kts Headwind. The distance A to B is 750 NM and TAS 300 Kts.The Distance of the PET from A is:
- Given:X = Distance A to point of equal time (PET) between A and BE = EnduranceD = Distance A to BO = Groundspeed ONH = Groundspeed BACKThe formula for calculating the distance X to point of equal time (PET) is:
- Given flight details:Distance: 2140 NMAll engines TAS: 500 ktOne engine inoperative TAS: 460 ktW/C outbound: 40kt headW/C inbound: 30kt tailWhat is the time and distance to the one engine inoperative PET?
- Given flight details:Usable Endurance: 6 hrsTAS: 250 ktsW/C outbound: -55 ktsW/C homebound: +35 ktsCalculate the distance to the Point of Safe Return:
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Flight Planning and Monitoring
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