The JAA
CPL 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.
 |
GroundSchool:
Flight Planning and Monitoring
JAA CPL Theory Test Prep Software
for MS-Windows |
|
|
|
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
JAA CPL
written test prep software. 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 JAA CPL
Flight Planning and Monitoring
Test Bank |
- The fuel burn off is 200kg/h with a relative fuel density of 0.8. If the relative density is 0.75, the fuel burn will be:
- The following apply:-Temperature ISA+15°C-Brake release mass 62000kg-Trip time 5hr 20minWhat is the trip fuel?
- Given: Distance B-C: 1200NMCruise Mach 0.78 at FL300Temperature: ISA-14°CTailwind component: 40ktGross mass at B: 50200kgThe fuel required from B-C is:
- For a flight of 2400 ground nautical miles the following apply:Head wind component: 25ktTemperature: ISA-10°CCruise altitude: 31000ftLanding mass: 52000kgThe (a) trip fuel and (b) trip time respectively are:
- For a flight of 2400 ground nautical miles the following apply:Tail wind: 25ktTemperature: ISA-10°CBrake release mass: 66000kgThe (a) trip fuel and (b) trip time respectively are:
- Given: FL75, OAT: +5°CDuring climb: average head wind component 20ktTake-off from MSL with the initial mass of 3650lbsFind: Still air distance (NAM) and ground distance (NM) using the graph "time, fuel, distance to climb".
- Given: FL75; OAT: +5°CDuring climb: average head wind component 20ktTake-off from MSL with the initial mass of 3650lbsFind: Time and fuel to climb
- An aircraft is in cruising flight at FL095, IAS 155kt. The pilot intends to descend at 500ft/min to arrive overhead the MAN VOR at 2000ft (QNH 1030). TAS will remain constant during descent, wind is neglegible, temperature is standard. The pilot must start the descent at a distance from MAN of:
- Given: FL75; OAT +10°C; Lean mixture 2300RPMFind: Fuel flow in gallons per hour (GPH) and TAS.
- Given:Dry operating mass (DOM)= 33510kgLoad= 7600kgFinal reserve fuel= 983kgAlternate fuel= 1100kgContingency fuel= 102kgThe estimated landing mass at alternate should be:
- A public transport aeroplane with reciprocating engines, is flying from PARIS to LYON. The final reserve corresponds to:
- The Trip Fuel for a jet aeroplane to fly from the departure aerodrome to the destination aerodrome is 5350kg. Fuel consumption in holding mode is 6000kg/h. The quantity of fuel which is needed to carry out one go-around and land on the alternate airfield is 4380kg. The destination aerodrome has a single runway.What is the minimum quantity of fuel which should be on board at take-off?
- Given: maximum allowable take-off mass 64400kgmaximum landing mass 56200kgmaximum zero fuel mass 53000kgdry operating mass 35500kgestimated load 14500kgestimated trip fuel 4900kgminimum take-off fuel 7400kgFind the maximum allowable take-off fuel:
- During an IFR flight in a Beech Bonanza the fuel indicators show that the remaining amount of fuel is 100 lbs after 38 minutes. The total amount of fuel at departure was 160 lbs. For the alternate fuel, 30 lbs is necessary.The planned fuel for taxi was 13 lbs. Final reserve fuel is estimated at 50 lbs. If the fuel flow remains the same, how many minutes can be flown to the destination with the remaining fuel?
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 JAA CPL
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 JAA CPL 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.
<
|
