Exam quiz Flight Performance and Planning - PPL(H) - Private Pilot License

Question 1

The upper limit of LO R 4 equals... See annex (PFP-030) Siehe Anlage 8

Accepted Answer

4.500 ft MSL.

Answer

1.500 ft AGL.

Answer

1.500 ft MSL.

Answer

4.500 ft AGL.

Question 2

What are the variable physical properties of the atmosphere that affect the helicopter performance?

Accepted Answer

Temperature, pressure, and humidity

Answer

Temperature, pressure, and carbon content

Answer

Pressure, humidity, and specific gravity

Answer

Pressure, humidity, and nitrogen content

Question 3

The position of the center of gravity (including fuel) equals... See figure(PFP-053e) Siehe Anlage 2

Accepted Answer

37.1 cm.

Answer

0.403 m.

Answer

37.3 cm.

Answer

0.401 m.

Question 4

What is the maximum helicopter mass to conduct a departure at 8000 feet pressure altitude and an outside air temperature of +20° C? Max. gross mass: 2500 lbs. Min. gross mass: 1600 lbs. See annex (PFP-045) Siehe Anlage 13

Accepted Answer

2460 lbs

Answer

1950 lbs

Answer

2500 lbs

Answer

1550 lbs

Question 5

What document contains information about the fuel consumption?

Accepted Answer

Flight manual (POH)

Answer

Mass and balance report

Answer

Log book

Answer

Airworthiness certificate

Question 6

The term "center of gravity" is defined as...

Accepted Answer

The point at which the total mass of the aeroplane is considered to act.

Answer

The heaviest point on an aeroplane.

Answer

Another designation for the neutral point.

Answer

Half the distance between the neutral point and the datum line.

Question 7

Exceeding the maximum allowed aircraft mass is...

Accepted Answer

Not permissible and essentially dangerous.

Answer

Only relevant if the excess is more than 10 %.

Answer

Exceptionally permissible to avoid delays.

Answer

Exceptionally permissible to avoid delays.

Question 8

What must be considered for cross-border flights?

Accepted Answer

Requires flight plans

Answer

Regular location messages

Answer

Approved exceptions

Answer

Transmission of hazard reports

Question 9

The basic empty mass of an aircraft includes...

Accepted Answer

The mass of the aeroplane plus standard items such as unusable fuel and other unusable liquids, lubricating oil in engine and auxiliary units, fire extinguishers, pyrotechnics, emergency oxygen equipment, supplementary electronic equipment.

Answer

The total mass of the aeroplane ready for a specific type of operation including crew, navigation instruments and engine cowling.

Answer

The total mass of an aeroplane ready for a specific type of operation including the required fuel and crew, but excluding traffic load.

Answer

The total mass of the aeroplane ready for a specific type of operation excluding unusable fuel and traffic load. The mass includes items such as crew and crew baggage.

Question 10

The density of AVGAS 100LL at 15° C is...

Accepted Answer

0.72 kg/l.

Answer

1.0 kg/l

Answer

0.82 kg/l.

Answer

0.68 kg/l.

Question 11

Why does the VNE decrease with increasing pressure altitude?

Accepted Answer

The true airspeed (TAS) increases

Answer

The groundspeed (GS) decreases

Answer

The rotor thrust exceeds the permissible structure limitations

Answer

The tail rotor effectiveness does not provide directional stability

Question 12

The power output of a piston engine is limited by...

Accepted Answer

Main rotor gearbox.

Answer

Exhaust system.

Answer

Crankcase.

Answer

Centrifugal clutch.

Question 13

For the purpose of a flight preparation, the pilot calculates a total take-off mass of 750 kg and a total moment of 625 mmkg. Which cross marks the center of gravity (CG)? See annex (PFP-003) Siehe Anlage 3

Accepted Answer

1

Answer

3

Answer

4

Answer

2

Question 14

Considering the following fuel data, how much trip fuel is required? Fuel for start-up and taxi: 5 L Fuel for take-off and climb: 12 L Fuel for cruise flight: 25 L Fuel for descent, approach and landing: 7 L Fuel for taxi and parking: 3 L Fuel to alternate: 13 L Final reserve fuel: 10 L

Accepted Answer

44 L

Answer

75 L

Answer

49 L

Answer

52 L

Question 15

The empty weight and the corresponding center of gravity (CG) of an aircraft are initially determined...

Accepted Answer

By weighing.

Answer

Through data provided by the aircraft manufacturer.

Answer

For one aircraft of a type only, since all aircraft of the same type have the same mass and CG position.

Answer

By calculation.

Question 16

The total weight of an aeroplane is acting vertically through the...

Accepted Answer

Center of gravity.

Answer

Center of pressure.

Answer

Neutral point.

Answer

Stagnation point.

Question 17

(For this question, please use annex PFP-061) According ICAO, what symbol indicates a group of unlighted obstacles? (2,00 P.) Siehe Anlage 16

Accepted Answer

C

Answer

D

Answer

A

Answer

B

Question 18

The maximum endurance with a helicopter is achieved by flying at...

Accepted Answer

A lower speed than for maximum range and at the lowest altitude that is safely possible.

Answer

The same speed as for maximum range and at optimum height.

Answer

A lower speed than for maximum range and at the service ceiling.

Answer

A higher speed than for maximum range and at the lowest altitude that is safely possible.

Question 19

(For this question, please use annex PFP-062) According ICAO, what symbol indicates a civil airport (not international airport) with paved runway? (2,00 P.) Siehe Anlage 17

Accepted Answer

A

Answer

B

Answer

C

Answer

D

Question 20

During a flight with a flight plan submitted, landing is conducted at an airfield other than the destination stated in the filed flight plan. Who has to be contacted by the pilot immediately?

Accepted Answer

Aeronatical Information Service (AIS).

Answer

The police department

Answer

The flight manager on duty.

Answer

Local office for aereal supervision.

Question 21

The center of gravity has to be located...

Accepted Answer

Between the front and the rear C.G. limit.

Answer

Behind the rear C.G. limit.

Answer

Right of the lateral C. G. limit.

Answer

In front of the front C.G. limit.

Question 22

The position of the center of gravity equals... See figure (PFP-052e) Siehe Anlage 1

Accepted Answer

142 in.

Answer

137.5 in.

Answer

147.5 in.

Answer

145.7 in.

Question 23

The result of a front C.G. position is: 1. Increase in stability. 2. Increase in fuel consumption. 3. Increase in stall speed. 4. Increase in range.

Accepted Answer

.1, 2, 3

Answer

.2, 3, 4

Answer

.1, 2

Answer

.2, 4

Question 24

What needs to be observed in conjunction with a flight on a hot day?

Accepted Answer

Outside air temperature and pressure altitude should be considered in particular

Answer

Thermal updraft should be used over uninhabited areas

Answer

Low density of the provided fuel should be observed during refueling

Answer

Air-fuel mixture in the climb and cruise should be fully enriched

Question 25

Which factor has a positive effect on the power required?

Accepted Answer

Clean blades

Answer

Unleaded fuel

Answer

Icy helicopter airframe

Answer

High density altitude

Question 26

During an unaccelerated flight...

Accepted Answer

The vertical component of thrust equals gravity and the horizontal component of thrust equals drag.

Answer

The vertical component of thrust equals the horizontal component of thrust and drag equals gravity.

Answer

The vertical component of thrust equals drag and the horizontal component of thrust equals gravity.

Answer

The horizontal component of thrust equals the sum of drag and gravity.

Question 27

The term "moment" with regard to a mass and balance calculation is referred to as...

Accepted Answer

Product of a mass and a balance arm.

Answer

Quotient of a mass and a balance arm.

Answer

Difference of a mass and a balance arm.

Answer

Sum of a mass and a balance arm.

Question 28

What is the purpose of "interception lines" in visual navigation?

Accepted Answer

They are used as easily recognizable guidance upon a possible loss of orientation

Answer

To mark the next available en-route airport during the flight

Answer

They help to continue the flight when flight visibility drops below VFR minima

Answer

To visualize the range limitation from the departure aerodrome

Question 29

What factor is affected by headwind during a departure?

Accepted Answer

Climb path angle

Answer

Rate of climb

Answer

Vx

Answer

Vy.

Question 30

A flight plan has been files for a flight departing at an uncontrolled aerodrome. When has the actual take-off time been transmitted to ATC?

Accepted Answer

Immediately after take-off.

Answer

At deviation from expected off-block time by more than 15 min.

Answer

When landing is assured.

Answer

Upon request from ATC.

Question 31

Which point indicates the speed for maximum endurance? See figure (PFP-044) Siehe Anlage 15

Accepted Answer

3

Answer

1

Answer

4

Answer

2

Question 32

Which section of the flight manual describes the centre of gravity limitations of a helicopter?

Accepted Answer

Limitations

Answer

Normal procedures

Answer

Performance

Answer

Supplements

Question 33

Given values: Calculated take-off mass = 746 kg calculated CG = 37.1 cm fuel burn = 30.5 l on station 45 cm. Where is the CG situated after the landing?

Accepted Answer

36.9 cm

Answer

37.5 cm

Answer

36.3 cm

Answer

37.2 cm

Question 34

Baggage and cargo must be properly stowed and fastened, otherwise a shift of the cargo may cause...

Accepted Answer

Uncontrollable attitudes, structural damage, risk of injuries.

Answer

Structural damage, angle of attack stability, velocity stability.

Answer

Calculable instability if the C.G. is shifting by less than 10 %.

Answer

Continuous attitudes which can be corrected by the pilot using the flight controls.

Question 35

Calculated take-off mass = 1082 kg, calculated CG = 0.254 m, fuel burn = 55 l on station 0.40 m. Where is the CG situated after the landing?

Accepted Answer

24.8 cm

Answer

25.2 cm

Answer

24.6 cm

Answer

25.4 cm

Question 36

Which is the most recently determined empty mass and the associated center of gravity (CG) arm from the aircraft documentation? See annex (PFP-006) Siehe Anlage 6

Accepted Answer

498 kg; 280.59 m

Answer

512 kg; 285.39 m

Answer

4 kg; 1.1 m

Answer

5 kg; 1.3 m

Question 37

The EOBT (estimated off-block time) is specified in the ATS flight plan as...

Accepted Answer

Coordinated Universal Time (UTC).

Answer

Local Mean Time (LMT).

Answer

Standard Time (ST).

Answer

Central European Time (CET).

Question 38

Loads must be adequately secured in order to...

Accepted Answer

Avoid any centre of gravity (C.G.) movements.

Answer

Allow steep turns.

Answer

Prevent excessive 'g'-loading during the landing flare.

Answer

Carry extra fuel.

Question 39

What needs to observed regarding ice formation during the flight?

Accepted Answer

An increase in mass and drag and a significant lift reduction

Answer

An increase in both drag and lift coefficient due to a mass increase

Answer

An increase in mass and a decrease in drag

Answer

An increase in mass and a reduced rate of descent

Question 40

When landing, if the TAS is significantly less than the ground speed, you will have...

Accepted Answer

Tailwind.

Answer

Headwind.

Answer

Crosswind.

Answer

An inversion.

Question 41

A helicopter approach is conducted into the wind because...

Accepted Answer

This provides more control at low groundspeeds.

Answer

It reduces groundspeed and increases the landing distance.

Answer

It increases the true airspeed and decreases the landing distance.

Answer

This avoids wake turbulence near the touchdown zone.

Question 42

During a flight, a flight plan can be filed at the...

Accepted Answer

Flight Information Service (FIS).

Answer

Search and Rescue Service (SAR).

Answer

Aeronautical Information Service (AIS).

Answer

Next airport operator en-route.

Question 43

What needs to be done to compensate a tail-heavy centre of gravity in a helicopter?

Accepted Answer

Add additional load in the front of the helicopter cabin

Answer

Remove all unnecessary attachment parts and covers

Answer

Remove unneeded equipment from the cockpit

Answer

Add additional fuel to the fuel tank behind the main rotor mast

Question 44

The term "balance arm" in the context of a mass and balance calculation defines the...

Accepted Answer

Distance from the datum to the center of gravity of a mass.

Answer

Point through which the force of gravity is said to act on a mass.

Answer

Point on the longitudinal axis of an aeroplane or its extension from which the centers of gravity of all masses are referenced.

Answer

Distance of a mass from the center of gravity.

Question 45

The term "maximum elevation figure" (MEF) is defined as...

Accepted Answer

The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude plus a safety margin, rounded to the next higher 100 ft.

Answer

The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude.

Answer

The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude plus a safety margin of 1000 ft (305 m), rounded to the next higher 100 ft.

Answer

The highest elevation within an area covering 1 degree of latitude and 1 degree of longitude plus a safety margin, rounded to the next lower 100 ft.

Question 46

The center of gravity (CG) defines...

Accepted Answer

The point through which the force of gravity is said to act on a mass.

Answer

The point on the longitudinal axis or its extension from which the centers of gravity of all masses are referenced.

Answer

The distance from the datum to the position of a mass.

Answer

The product of mass and balance arm.

Question 47

Up to which altitude is an overflight prohibited according to the NOTAM? See figure (PFP-024) Siehe Anlage 10

Accepted Answer

Altitude 9500 ft MSL

Answer

Height 9500 ft

Answer

Flight Level 95

Answer

Altitude 9500 m MSL

Question 48

Which actions should be taken if the orientation is lost during helicopter flight operations?

Accepted Answer

Continue with planned heading to the next interception line and reorientate from there

Answer

Return to the departure aerodrome and reorientate from there

Answer

Continue the flight in any direction until the navigation can be resumed

Answer

According the Warsaw convention orientation triangles must be flown

Question 49

An aircraft must be loaded and operated in such a way that the center of gravity (CG) stays within the approved limits during all phases of flight. This is done to ensure...

Accepted Answer

Both stability and controllability of the aircraft.

Answer

That the aircraft does not exceed the maximum permissible airspeed during a descent.

Answer

That the aircraft does not stall.

Answer

That the aircraft does not tip over on its tail while it is being loaded.

Question 50

The upper limit of LO R 16 equals... See annex (PFP-056) Siehe Anlage 7

Accepted Answer

1 500 ft MSL.

Answer

1 500 m MSL.

Answer

1.500 ft GND.

Answer

FL150.

Question 51

The specified speed in the ATS flight plan equals: See annex (PFP-051) Siehe Anlage 12

Accepted Answer

100 kt.

Answer

100 m/h.

Answer

100 km/h.

Answer

1000 kt.

Question 52

The term "datum" with regard to a mass and balance calculation defines...

Accepted Answer

The point on the longitudinal axis of an aeroplane or its extension from which the centers of gravity of all masses are referenced.

Answer

The distance from the reference plane to the center of gravity of an aircraft.

Answer

The point on the vertical axis of an aeroplane or its extension from which the centers of gravity of all masses are referenced.

Answer

The point on the lateral axis of an aeroplane or its extension from which the centers of gravity of all masses are referenced.

Question 53

What is the lowest possible VFR flight level if a true course of 181° is selected and a variation of 3° east exists?

Accepted Answer

FL 055

Answer

FL 065

Answer

FL 060

Answer

FL 050

Question 54

Which section of the flight manual describes the power required of a helicopter in a hover?

Accepted Answer

Performance

Answer

Limitations

Answer

Normal procedures

Answer

Supplements

Question 55

The power output of a turbine engine is limited by...

Accepted Answer

Compressor RPM, turbine inlet temperature, and main rotor gearbox.

Answer

Auxiliary equipment rack and exhaust system in multi-shaft turbine engines.

Answer

Fuel type, burn rate, and exhaust system.

Answer

Freewheel unit and main rotor gearbox in single-shaft turbine engines.

Question 56

How do manufacturers reduce the power output of their engines for use in helicopters?

Accepted Answer

Decrease the shaft RPM

Answer

Adjust the ignition timing

Answer

Reduce the combustion chamber

Answer

Limit the fuel flow

Question 57

What mass equals 102 litres of Avgas 100LL?

Accepted Answer

74 kg

Answer

74 lbs

Answer

142 lbs

Answer

142 kg

Question 58

What is the nature of the flight shown in the given ATC flight plan? See annex (PFP-051a) Siehe Anlage 11

Accepted Answer

Night flight under visual flight rules.

Answer

Flight under instrument flight rules.

Answer

Border crossing flight.

Answer

Traffic pattern under visual flight rules.

Question 59

For a given fuel load, if the helicopter mass is increased...

Accepted Answer

The maximum range will be decreased.

Answer

The normal fuel burn will be increased.

Answer

The power required will be unchanged.

Answer

The parasite drag will be unchanged.

Question 60

The conversion factor from kilogram [kg] into pounds [lb] is...

Accepted Answer

Kg x 2.205 = lb.

Answer

Kg / 2.205 = lb.

Answer

Kg x 0.454 = lb.

Answer

Kg x 2 = lb.

Question 61

How much taxi fuel must be consumed before take-off to reduce the aircraft mass to the maximum take-off mass? Maximum ramp mass (MRM): 1150 kg Actual ramp mass: 1148 kg Maximum take-off mass (MTOM): 1145 kg

Accepted Answer

4 L

Answer

3 L

Answer

2 L

Answer

5 L

Question 62

What is the never-exceed speed at 4000 feet pressure altitude, +10° C outside air temperature and a helicopter mass of 2300 lbs? See annex (PFP-046) Siehe Anlage 14

Accepted Answer

116 KIAS

Answer

126 KIAS

Answer

96 KIAS

Answer

130 KIAS

Question 63

What is the message of the NOTAM shown below? B7938/11 NOTAMN Q) LECB/QMRLC/IV/NBO/A /000/999/3933N00244E005 A) LEPA B) 1111212200 C) 1111220500 E) RWY 24L/06R CLOSED

Accepted Answer

Runway 24L/06R at Palma de Mallorca (LEPA) airport will be closed from November 21st 2011 2200 UTC until November 22nd 2011 0500 UTC

Answer

Runway 24L/06R at Palma de Mallorca (LEPA) airport will be closed from November 21st 2011 2200 local time until November 22nd 2011 0500 local time

Answer

Runway 24L/06R at Palma de Mallorca (LEPA) airport will be closed from present time (000) indefinitely (999)

Answer

Runway 24L/06R at Cataluña/Barcelona (LECB) airport will be closed from November 21st 2011 2200 UTC until November 22nd 2011 0500 UTC

Question 64

What is the maximum pressure altitude to conduct a hover in ground effect if the helicopter mass equals 2400 lbs and the outside air temperature is +20° C? See annex (PFP-045) Siehe Anlage 13

Accepted Answer

8600 ft

Answer

9000 ft

Answer

11000 ft

Answer

9500 ft

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