The EASA
ATPL Flight Planning and Monitoring
test bank contains questions pertaining to
033-01-02 Fuel plan
. 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
as a general familiarization tool, this list may not be up-to-date nor accurate.
We do not update this website as often as we update our software, which will
contain at any moment all questions that we have for a given test / topic. Therefore,
if you need to actually study for your test, instead of using the list below,
we strongly, strongly encourage you to download our GroundSchool
EASA ATPL
Written Test Prep Software and Apps. Not only is it more complete and up-to-date, but is also considerably faster and more efficient as a study tool.
| Sample Questions
from the EASA ATPL
Flight Planning and Monitoring
Test Bank |
- (Refer to CAP 697 - figure 2.5)Find the pressure height to achieve the endurance under the following conditions:Power setting: Full throttle / 2300 rpmEndurance: 348 min
- (Refer to CAP 697 - figure 2.2.1)Give the fuel flow (GPH) and TAS for 25 in. HG @ 2500 RPM at FL 65, ISA -17° C:
- (Refer to CAP 697 figure 2.4)Take-off Mass: 3663 lbsFuel Load: 74 US GallonsTake-off Altitude: Sea LevelWind component: +40 ktsCruise Altitude: 9000 ftPower Setting: Full Throttle, 2500 rpmWhat is the range of the aircraft?
- (Refer to CAP 697 - figure 2.5)What is the endurance and approximate TAS for a flight at 11,500 feet pressure altitude, 23 in HG (or full throttle) @ 2300 RPM?
- (Refer to CAP 697 figure 2.2.2)What is the fuel flow (lb/hr) and KIAS for an aircraft at FL70, ISA +10° C deviation?
- A multi engine piston aeroplane is on an IFR flight. The fuel plan gives a trip fuel of 65 US gallons. The alternate fuel, final reserve included, is 17 US gallons. Contingency fuel is 5% of the trip fuel. The usable fuel at departure is 93 US gallons. At a certain moment the fuel consumed according to the fuel gauges is 40 US gallons and the distance flown is half of the total distance. Assume that fuel consumption does not change. Which statement is right?
- (Refer to CAP 697 - figure 2.2.3)Given the following calculate the fuel flow, IAS and TAS for a power setting of 23 inches / 2300 rpm:Cruise: 7000 ftTemperature: 3° C
- (Refer to CAP 697 - figure 2.5)What is the percentage increase in endurance for 23 inches / 2300 rpm opposed to 25 inches / 2500 rpm at 4000ft?
- (Refer to CAP 697 - figure 2.3)Given the following find the fuel remaining at the end of the leg:Temp deviation: -10° CCruise level: FL100Forecast W/V: 240/48Track: 315° TSector distance: 275 NMFuel on board at start of leg: 360 lb
- (Refer to CAP 697 - figure 2.4)Take-off Mass: 3663 lbsFuel Load: 74 US GallonsTake-off Altitude: Sea LevelWind component: -50 ktsCruise Altitude: 11 000 feetPower Setting: Full Throttle, 2500 rpmWhat is the range of the aircraft?
- For a planned flight the calculated fuel is as follows:Flight time: 3h06minTaxi fuel: 8 kgBlock fuel: 118 kgThe reserve fuel, at any time, should not be less than 30% of the remaining trip fuelHow much fuel should remain after 2 hours flight time?
The
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Flight Planning and Monitoring
test bank, click here.
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