The EASA
ATPL Flight Planning and Monitoring
test bank contains questions pertaining to
033-04-03 General flight planning tasks
. 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.
 |
GroundSchool:
Flight Planning and Monitoring
EASA ATPL Theory Test Prep Software
for MS-Windows |
 | Sorry, file temporarily unavailable. Please check back soon. | |
|
|
|
|
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 |
- If the pressure altitude is 5,000 feet and the ambient outside air temperature is ISA +20° C what is the density altitude?
- (Refer to CAP 697 - figure 3.2)The aircraft is using 65% power, flying at 17 500 ft. What range is lost if the 45 minute reserve figures are used rather than the no reserve figures?
- Details of a flight are as follows:MTOM: 142,500 kgDry Operating Mass: 68,000 kgMaximum Zero Fuel Mass: 85,500 kgMean TAS: 410 ktsDistance P to Q: 3600 NMMean Fuel consumption: 6500 kg/hrReserve Fuel (assume unused): 7500 kgMaximum Landing Mass: 96,000 kgFind the maximum Traffic Load in still air:
- The still air distance in the climb is 189 Nautical Air Miles (NAM) and time 30 minutes. What ground distance would be covered in a 30 kt head wind?
- Given:Ground speed: 292 ktsDistance NAM: 93Time: 17 minutesCalculate TAS, Wind component and NGM:
- From which of the following would you expect to find facilitation information (FAL) regarding customs and health formalities?
- An aircraft is in cruising flight at FL 095, IAS 155kt. The pilot intends to descend at 500 ft/min to arrive overhead the MAN VOR at 2 000 FT (QNH 1 030hPa). The TAS remains constant in the descent, wind is negligible, temperature standard. At which distance from MAN should the pilot commence the descent?
- Given:Dry Operating Mass: 48,500 kgMaximum take-off Mass: 76,500 kgMaximum landing Mass: 59,740 kgRoute fuel excluding reserve: 14,220 kgFuel reserve: 2,200 kgAssuming that the fuel reserve will be unused, determine the take-off weight when maximum payload is carried:
- Calculate the distance covered in a descent form the information below:Cruise Altitude: 20 000 ftCleared Altitude: 1000 ftRate of Descent: 500 fpmGroundspeed: 300 knots
- (Refer to Route Manual chart NAP or figure HI-23)The average true course from C (62° N 020° W) to B (58° N 004° E) is:
- An aircraft is to fly from A to B and then to C without refuelling at B.Given:MTOM at A: 41,800 kgMTOM at B: 37,000 kgDOM: 23,500 kgMaximum Zero Fuel Mass: 31,300 kgMean TAS: 418 ktsDistance A to B: 521 NMDistance B to C: 703 NMWind component A to B: 35 kts tailWind Component B to C: 30 kts headMean fuel consumption A to B: 3100 kg/hrMean fuel consumption B to C: 2950 kg/hrReserve fuel (assume unused): 2,000 kgMaximum Landing Mass at B: 38,000 kgMaximum Landing Mass at C: 36,500 kgCargo weighing 1250 kg loaded at A must be carried to C.Determine the maximum Traffic Load that could be loaded at A:
- Details of a flight are as follows:MTOM: 142,500 kgDry Operating Mass: 68,000 kgMaximum Zero Fuel Mass: 85,500 kgMean TAS: 410 ktsDistance P to Q: 3600 NMMean Fuel consumption: 6500 kg/hrReserve Fuel (assume unused): 7500 kgMaximum Landing Mass: 96,000 kgFind the maximum Traffic Load with a 100 kt tail wind:
- (Refer to Route Manual chart NAP or figure HI-23)The average true course from A (64° N 006° E) to C (62° N 020° W) is:
- Given:TAS: 245 ktsDistance NAM: 785Distance NGM: 745Calculate GS and Wind component:
- An aircraft is to fly from A to B and then to C without refuelling at B.Given:MTOM at A: 41,800 kgMTOM at B: 37,000 kgDOM: 23,500 kgMaximum Zero Fuel Mass: 31,300 kgMean TAS: 418 ktsDistance A to B: 521 NMDistance B to C: 703 NMWind component A to B: 35 kts tailWind Component B to C: 30 kts headMean fuel consumption A to B: 3100 kg/hrMean fuel consumption B to C: 2950 kg/hrReserve fuel (assume unused): 2,000 kgMaximum Landing Mass at B: 38,000 kgMaximum Landing Mass at C: 36,500 kgCargo weighing 1250 kg loaded at A must be carried to C.Determine the maximum Traffic Load that could be loaded at B:
- Given:Wind Component: -55 ktsDistance NAM: 377Time: 57 minutesCalculate NGM:
- The fuel burn - off is 200 kg/hr with a relative fuel density of 0.8. If the relative fuel density is 0.75, the fuel burn will be:
- Given:Dry Operating Mass: 48,500 kgMaximum take-off Mass: 76,500 kgMaximum landing Mass: 59,740 kgRoute fuel excluding reserve: 14,220 kgFuel reserve: 2,200 kgAssuming that the fuel reserve will be unused, determine the maximum Traffic Load:
The
list above contains 1/4 or less of the actual number of questions
and may not be up to date! Download the software today to get
access to all available questions. |
For
more information about the EASA ATPL
Flight Planning and Monitoring
test bank, click here.
Copyright,
Content, and Accuracy Notice: . Dauntless Software grants visitors
permission to use the contents of this page for personal use - commercial or
public use, including collecting (or harvesting) of any data or material on
this page is strictly prohibited. This material is presented for informational
purposes only and may be in error. Dauntless Software works hard to maintain
our EASA ATPL question banks. If you see an error on this web page, it
is likely NOT an error that is repeated in our software, as our software (unlike
this web page) is connected to our editorial mechanism whose mission is to quickly
identify and correct errors. If you see what you believe to be an error, please
download and try our software to see if the error is repeated there. If you
believe it is, you can use the issue-reporting mechanisms within the software
to contact our editors about any concern you may have and we will be happy to
look into it promptly.
<
|
