The JAA
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.
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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
JAA ATPL
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 ATPL
Flight Planning and Monitoring
Test Bank |
- (Refer to Route Manual chart NAP or figure HI-23)The average magnetic course from A (64° N 006° E) to C (62° N 020° W) is:
- (Refer to Route Manual chart NAP or figure HI-23)The distance (NM) from A (64° N 006° E) to C (62° N 020° W) is:
- Given:Maximum authorised Take-off Mass: 45,000 kgDOM: 24,500 kgMaximum authorised Zero Fuel Mass: 36,500 kgMean TAS: 425 ktsMaximum fuel capacity: 13,300 kgMean fuel consumption: 2400 kg/hReserve fuel (assume unused): 1300 kgMaximum Landing Mass: 39,500 kgAssuming still air conditions determine the greatest Traffic Load which can be carried over the maximum range:
- Given:Wind component: +83 ktsGround speed: 539 ktsDistance NGM: 280Distance NAM: 237Calculate TAS and Time:
- A sector distance is 450 NM long. The TAS is 460 kt. The wind component is 50 kt tailwind. What is the still air distance?
- Convert 4500 ft to metres:
- Given:Maximum Take-off Mass: 62,800 kgMaximum Zero Fuel Mass: 51,300 kgMaximum Landing Mass: 54,900 kgDry Operating Mass: 35,000 kgTraffic Load: 12,000 kgTotal trip fuel required (including all reserves and diversion fuel): 13,200 kgEstimated reserve on landing: 3,100 kgCalculate the extra fuel uplift available:
- A turbine-engine aircraft burns fuel at 200 gals per hour (gph) with a Fuel Density of 0.8. What is the fuel flow if Fuel Density is 0.75?
- From which of the following would you expect to find information regarding known short un-serviceability of VOR, TACAN, and NDB?
- (Refer to CAP 697 figure 2-1)Aerodrome elevation 2500 ft, OAT +10° CInitial weight: 3 500 lbsClimb to FL140, OAT -5° CWhat is the climb time, fuel, and NAM?
- Given:Maximum authorised Take-off Mass: 45,000 kgDOM: 24,500 kgMaximum authorised Zero Fuel Mass: 36,500 kgMean TAS: 425 ktsMaximum fuel capacity: 13,300 kgMean fuel consumption: 2400 kg/hReserve fuel (assume unused): 1300 kgMaximum Landing Mass: 39,500 kgAssuming still air conditions determine the greatest distance over which the maximum traffic load in can be carried. (Assume reserve fuel unused).
- Given the following:True Course: 150° Wind velocity: 300/30TAS: 400 knotsWhat is the wind correction angle (WCA) and the groundspeed?
- Given:TAS: 312 ktsWind component: -27 ktsDistance NGM: 119Time: 25 minutesCalculate Ground speed and NAM:
- Assume for a flight from A to B:Maximum Take-off Mass: 53,500 kgDry Operating Mass: 32,000 kgMean TAS: 220 ktsDistance A to B: 1320 NMMean consumption: 1340 kg/hrReserve fuel to be carried (assume unused): 2400 kgMaximum Landing Mass: 44,500 kgCalculate the maximum Traffic Load which can be carried with a headwind of 40 kts:
- The still air distance for a climb is 210 NAM. The climb takes 30 minutes with a headwind component of 50 knots the NGM covered are:
- Given:Maximum Take Off Mass: 114,000 lbDOM: 61,000 lbMaximum Zero Fuel Mass: 95,000 lbAverage groundspeed: 500 ktsMean fuel consumption: 6250 lb/hReserve fuel to be carried (assume unused): 5000 lbMaximum Landing Mass: 102,000 lbCalculate the maximum traffic load that could be carried over the distance of 800 NM:
- (Refer to Route Manual chart NAP or figure HI-23)The initial true course from C (62° N 020° W) to B (58° N 004° E) is:
- (Refer to CAP 697 figure 4.5.4)Planning an IFR-flight from Paris to London for the twin jet aeroplane.Given:Estimated Landing Mass: 49 700 kgFL 280W/V 280° /40 ktAverage True Course: 320° Procedure for descent: .74 M/250 KIASDetermine the time from the top of descent to London (elevation 80 ft) .
- Given:Maximum authorised Take-off Mass: 45,000 kgDOM: 24,500 kgMaximum authorised Zero Fuel Mass: 36,500 kgMean TAS: 425 ktsMaximum fuel capacity: 13,300 kgMean fuel consumption: 2400 kg/hReserve fuel (assume unused): 1300 kgMaximum Landing Mass: 39,500 kgAssuming still air conditions determine the absolute maximum Traffic Load this aircraft can carry.
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. |
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more information about the JAA ATPL
Flight Planning and Monitoring
test bank, click here.
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