The JAA
IR 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 IR 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 IR
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 IR
Flight Planning and Monitoring
Test Bank |
- You are to determine the maximum fuel load which can be carried in the following conditions:-dry operating mass: 2800kg-trip fuel: 300kg-payload: 400kg-maximum take-off mass: 4200kg-maximum landing mass: 3700kg
- The following apply:-Tail wind component 10kt-Temperature ISA+10°C-Brake release mass 63000kg-Trip fuel available 20000kgWhat is the maximum possible trip distance?
- Within the limits of the data given, a mean temperature increase of 30°C will affect the trip time by approximately:
- For a flight of 2800 ground nautical miles the following apply:Head wind component: 15ktTemperature: ISA+15°CCruise altitude: 35000ftLanding mass: 50000kgThe (a) trip fuel and (b) trip time respectively are:
- For a flight of 2000 ground nautical miles, cruising at 30000ft, within the limits of the data given, a headwind component of 25kt will affect the trip time by approximately:
- For a flight of 1900 ground nautical miles the following apply:Head wind component: 10ktTemperature: ISA-5°CTrip fuel available: 15000kgLanding mass: 50000kgWhat is the minimum cruise level (pressure altitude) which may be planned?
- True Air Speed: 170kt; Wind in the area: 270°/40ktAccording to the attached navigation log, an aircraft performs a turn overhead BULEN to re-route to ARD via TGJ.The given wind conditions remaining constant.The fuel consumption during the turn is 20 litres.The total fuel consumption at position overhead ARD will be:
- In the cruise at FL155 at 260TAS, the pilot plans for a 500feet/min descent in order to fly overhead MAN VOR at 2000feet (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: Break release mass: 58000kgTemperature: ISA+15The fuel required to climb from an aerodrome at elevation 4000ft to FL300 is:
- Given: Distance to Alternate: 450NM; Landing mass at Alternate: 45000kg; Tailwind component: 50kt; The alternate fuel required is:
- HOLDING PLANNING: The fuel required for 30 minutes holding, in a racetrack pattern, at PA 1500ft, mean gross mass 45000kg, is:
- The flight crew of a turbojet aeroplane prepares a flight using the following data:-Take-off mass: 168500kg-Flight leg ground distance: 2000NM-FL370; "Long Range" flight regime-Tailwind component at this level: 30kt-Total anti-ice set on "ON"-Fixed taxi fuel: 500kg; final reserve: 2000kg-Ignore alternate fuelThe effects of climb and descent are not corrected for consumption.The prescribed quantity of trip fuel for the flight leg is:
- A flight has to be made with a multi engine piston aeroplane (MEP1). For the fuel calculations take 5Us gallons for the taxi, and additional 13 minutes at cruise condition to account for climb and descent. Calculated time overhead to overhead is 2h37min.Powersetting is 65%, 2500RPM. Calculated reserve fuel is 30% of the trip fuel. FL120. Temperature 1°C. Find the minimum block fuel.
- 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?
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 IR
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 IR 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.
<
|
