The JAA
ATPL 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 ATPL
Flight Planning and Monitoring
Test Bank |
- (Refer to CAP 697 - figure 3.1)Calculate the fuel used in lbs, time in minutes and the distance travelled in the climb given:Aerodrome Pressure Altitude: 6000 ftAmbient Temperature: +8° CTOC: 16 000 ft Pressure AltitudeAmbient Temperature: -15° CWind Component: 30 kt headwind
- A twin engine aircraft is to fly from C to D:Track 035° (T)Distance 884 NMW/V 135/452 engine TAS 220 Kts1 engine TAS 185 KtsIf the ETD is 1100 Z the ETA at the 1 ENG INOP PET (CP) is:
- (Refer to figures 4.3.1.B & 4.5.3.1)Given for the twin jet aeroplane:Zero fuel mass: 50 000 kgLanding mass at alternate: 52 000 kgFinal reserve fuel: 2 000 kgAlternate fuel: 1 000 kgFlight to destination: Distance 720 NM, TC 030° , W/V 340° /30 ktCruise: LRC, FL 330, OAT -30° CFind: Estimated trip fuel and time with simplified flight planning.
- Refer to Jeppesen Manual, any SID or approach chart for London Heathrow (or figure AP-12).Which of the following is the correct Minimum Safe Altitude (MSA) for the airport?
- (Refer to figure 4.7.3)Given:Distance to alternate: 950 NMHead wind component: 20 ktMass at point of diversion: 50 000 kgDiversion fuel available: 5 800 kgThe minimum pressure altitude at which the above conditions may be met is:
- (Refer to the Jeppesen Student Pilot Route Manual or figure AP-27)Using the 10-2 STAR charts for Amsterdam (REKKEN A to Runway 06). The IAF is:
- (Refer to CAP 697 - figure 3.6)Calculate the fuel used in lbs, time taken and distance travelled with an 8 kt headwind for the descent, given:Cruise Pressure Altitude: 18 000 ftAmbient Temperature: -22° CAerodrome Pressure Altitude: 7 000 ftAmbient Temperature: -2° C
- (Refer to CAP 697 - figure 3.1)Calculate the fuel used in lbs, time taken in minutes and the distance travelled in the climb, given:Aerodrome Pressure Altitude: 5 000 ftAmbient Temperature: +6° CTOC: 13 000 ft Pressure AltitudeAmbient Temperature: -10° CWind Component: +28 kts
- 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:
- (Refer to CAP 697 - figures 3.3 & 3.4)Calculate the fuel used in lbs, the Manifold Pressure and the time taken in the cruise, given:55% power set at 2500 rpmCruise Pressure Altitude: 15 000 ftAmbient Temperature: -17° CLeg Distance: 373 NMWind Component: 19 kt tailwind
- (Refer to figure 4.5.1)Given:Estimated take-off mass: 57 500 kgInitial cruise: FL 280Average temperature during climb: ISA -10° CAverage head wind component: 18 ktFind the climb time.
- (Refer to Jeppesen Manual Paris Charles-de-Gaulle (21-7) ILS rwy 10 or figure AP-16)What is the ILS course?
- (Refer to figure 3-6)A flight is to be made to an airport, pressure altitude 3000 ft, in a multi engine piston aeroplane (MEP1). The forecast OAT for the airport is -1° C. The cruising level will be FL 110, where OAT is -10° C. Calculate the still air descent distance for:145 KIASRate of descent 1000 ft/minGear and flaps up
- (Refer to CAP 697 - figure 3.5)What is the endurance with 45 minute reserve for the aircraft using 65% power at 15 000 ft?
- (Refer to figure 3-1)Given:Take-off mass 3500 lbsDeparture aerodrome pressure altitude 2500 ft, OAT +10° CFirst cruising level: FL 140, OAT -5° CFind the time, fuel and still air distance to climb:
- (Refer to CAP 697 figure 4.4)Given for the twin jet aeroplane:Estimated mass on arrival at the alternate: 50 000 kgEstimated mass on arrival at the destination: 52 525 kgAlternate elevation: MSLDestination elevation: 1500 ftFind: Final reserve fuel and corresponding time.
- (Refer to Jeppesen Manual SID chart for AMSTERDAM SCHIPOL (10-3) or figure AP-06)Which statement is correct for ANDIK departures from runway 19L?
- (Refer to Route Manual chart E(HI)4 or figure HI-09)An aeroplane has to fly from Abbeville (50° 08.1N 001° 51.3E) to Biggin (51° 19.8N 00° 00.2E).At Biggin you can find: 141° . This is:
- Given:Distance A to B: 2050 NMMean groundspeed on 440 ktMean groundspeed back 540 ktThe distance to the point of equal time (PET) between A and B is:
- (Refer to CAP697 figure 4.5.3.1)Long Range Cruise at FL350OAT: -45° CGross mass at the beginning of the leg: 40 000 kgGross mass at the end of the leg: 39 000 kgFind: True airspeed (TAS) and cruise distance (NAM) for a twin jet aeroplane.
- (Refer to figure 4.4)HOLDING PLANNINGThe fuel required for 45 minutes holding, in a racetrack pattern, at PA 5000 ft, mean gross mass 47 000 kg, is:
- INTEGRATED RANGE curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is:
- (Refer to CAP 697 figure 4.2.2)Given:Brake release mass: 45 000 kgTemperature: ISA + 20° CTrip distance: 50 Nautical Air Miles (NAM)Find the SHORT DISTANCE CRUISE ALTITUDE for the twin - jet aeroplane.
- Given:15,000 kg total fuelReserve 1,500 kgTAS 440 ktWind component 45 head outboundAverage fuel flow 2150 kg/hrWhat is the distance to the point of safe return?
- (Refer to CAP 697 figure 4.5.1)Planning an IFR-flight from Paris (Charles de Gaulle) to London (Heathrow) for the twin jet aeroplane. Given:Estimated Take-off Mass (TOM): 52 000 kgAirport elevation: 387 ftFL 280W/V 280° /40 ktISA Deviation: -10° CAverage True Course: 340° Find: Time to the top of climb (TOC).
- On a flight from A to B aircraft performance outbound is 0.423 GNM/KG and aircraft performance returning to B is 0.527 GNM/KG. Total Fuel on board is 9000 KG which includes a 1500 KG reserve.The distance to the PNR keeping the reserve fuel intact is :
- On a flight from A to B, the wind component outbound is 50kt H/W. The all engines operating TAS is 500 kt and the aircraft’ s safe endurance is 4 hrs. If the PSR to A is 330 NM beyond the PET between A and B, the distance between A and B is:
- Total fuel available overhead X (excluding reserves): 24,000 kgDistance X to Y: 850 NMMean TAS (4 engines): 310 ktMean TAS (3 engines): 275 ktMean F/F (4 engines): 6500 kg/hrMean F/F (3 engines): 6350 kg/hrMean wind component out: -45 ktMean wind component home: +35 ktAssuming the ETA at the all engines operating PNR is 1419, the ETA at Y on 4 engines is:
- (Refer to the Jeppesen Student Pilot Route Manual or figure AP-27)Using the 10-2 STAR charts for Amsterdam (REKKEN A to Runway 06). At DME 30 from SPL the maximum altitude should be:
- (Refer to CAP 697 – SEP 1 - figure 2.2.2)What is the fuel flow (gal/hr) and KTAS for an aircraft at FL70, ISA +10° C deviation?
- Given flight details:Usable Endurance: 4 hrsTAS: 390 ktsW/C outbound: +32 ktsW/C homebound: -38 ktsCalculate the distance to the Point of Safe Return:
- 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:
- 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:
- (Refer to Route Manual chart STAR LONDON Heathrow (10-2) or figure AP-08)Planning a IFR flight from Paris (Charles de Gaulle) to London (Heathrow). Find the elevation of the destination aerodrome.
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