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Online Test 2
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Preguntas del test (30)
1The consideration which determines whether an aircraft is in the normal, utility or aerobatic category is -
- Athe Vne of the aircraft
- Bthe maximum positive and negative load factor limitations
- Cthe power/weight ratio
- Dthe manoeuvring speed
2A centre of gravity range is imposed on an aircraft to ensure that -
- Athe aircraft will be controllable during flight
- Bthe climb performance after take-off will allow a gradient of at least 6 percent
- Cthe aircraft will be controllable in strong cross winds
- Dthe maximum structural limits on the tailplane are not exceeded
3The height registered on a sensitive altimeter when the sub scale is set to 1013.2 hPa is known as -
- AISA height
- Bpressure height
- Cdensity height
- Dstandard height
4An atmospheric density expressed in terms of a height which corresponds to that density in the standard atmosphere is called -
- Adensity height
- BISA height
- Cpressure height
- Dstandard height
5All of the speed limitations such as Vne, Va and Vno are imposed because -
- Ano performance data is available for operation beyond these speeds
- Bno control will exist above these speeds
- Cthe aircraft may become unstable above these speeds
- Dthe aircraft structure may suffer damage if operated above these speeds under the conditions described
6A structural take-off weight limit is imposed on an aircraft to ensure that -
- Athe aircraft is capable of achieving a 5 percent climb gradient after take-off
- Bthe maximum tyre pressure limitations are not exceeded
- Cthe aircraft is capable of becoming airborne in the distance available
- Dno damage is caused during the take-off run
7A climb weight limit line on a performance chart determines a weight which ensures a climb gradient of not less than -
- A6 percent in the take-off configuration
- B6 percent in the landing configuration
- C3.2 percent in the take-off configuration
- D5.0 percent in the landing configuration
8When using an asphalt runway, the landing distance will increase if -
- Athere is a crosswind on the runway
- Bfull flap is lowered
- CThere is a decrease in stalling speed
- Dthere is water on the runway
9If the pressure height of a certain airfield is 4500 ft and the ambient temperature is +12 deg C, the ISA deviation is -
- A+12 deg C
- B+6 deg C
- C-6 deg C
- D0 deg C
10An aircraft is cruising at 13000 ft. If the ISA deviation is +11, the outside air temperature is closest to -
- A0 deg C
- B+11 deg C
- C-22 deg C
- D-11 deg C
11The positive and negative load factor limits for a particular aeroplane are considered when determining the aircraft's -
- AVNE [never exceed speed]
- Bpermitted category of registration
- Ctake-off and landing performance
- Dstability
12The flight situation during which the limit load factors are most likely to be exceeded is -
- Ahigh IAS in severe turbulence
- Blow IAS in severe turbulence
- CIAS above VNE in smooth air
- Da steep level turn at low IAS
13A windmill is situated on the extended centreline of the strip at an aeroplane landing area [ALA] and 180 metres from the upwind end of the strip.
To comply with the recommendations of the Civil Aviation Advisory Publication 92.1 for day operation, the windmill should be no higher than -- A15 metres
- B9 metres
- C20 metres
- D18 metres
14The following data relates to a day VFR charter flight.
TAS in cruise....................170 kt
Fuel flow during cruise..........60 litres/hour
Wind component during cruise....20 knot headwind
Fixed reserve...................45 minutes at cruise rate
Taxi allowance..................5 litres
Holding requirement at departure aerodrome......30 minutes
Holding requirement at destination aerodrome....60 minutes
Holding to be calculated at cruise rate
Fuel on board at start up 150 litres
The distance to the PNR for the flight described above is -- A61 nm
- B27 nm
- C85 nm
- D34 nm
15Refer to page 18 of the work booklet.
An Echo aeroplane has an empty weight and moment index of 1967 kg and 480 index units respectively. In preparation for loading, all seats except the pilots seat are removed.
The moment index after the removal of the seats is closest to -- A463.56
- B481.25
- C471.26
- D475.30
16An Echo has 300 litres of fuel on board at start up.
The flight fuel required is 120 litres.
The fixed reserve is 15 gallons.
The start up allowance is 3 gallons.
Fuel flow for holding is 17.2 gph.
The maximum time the aircraft could plan to hold at the destination aerodrome is -- A86 min
- B75 min
- C95 min
- D105 min
17Refer to page 22 of the work booklet.
The take-off data for an Echo aeroplane at a given strip are as follows:
QNH.............1030 hPa
Elevation.......500 ft
Temperature.....+ 20 degrees C
TODA............800 m
Surface.........short wet grass
Slope...........1.5 percent down to the South
Wind............120 degrees M at 20 kt
Runway..........18/36
The maximum weight permitted for this take-off is closest to -- A2725 kg
- B2950 kg
- C2600 kg
- D2550 kg
18Your aircraft is fuelled with 45 US gallons of fuel. You allow 2 US gallons for start-up, taxi and take-off. Your average fuel consumption rate in flight is 13.0 US gallons per hour.
The amount of fuel, in litres, that should remain after 76 minutes of flight is closest to -- A100 litres
- B205 litres
- C130 litres
- D220 litres
19Refer to loading system Echo on pages 18 to 21 of the work booklet.
A box of cargo is presented for loading on an Echo aeroplane, its dimensions are 400mm x 300 mm x 200 mm.
The MAXIMUM weight permitted for this box if it is carried in the FORWARD compartment is closest to -- A27 kg
- B54 kg
- C36 kg
- D55 kg
20Given:
Distance A to B..........410 nm
POB........................Pilot only is on board and his weight is 77 kg
Basic empty weight......1990 kg
No limitations imposed by runway lengths at A or B.
No seats to be removed.
Cruise TAS is 185 knots and cruise fuel flow is 28 gph. [Ignore climbs and descents]
Fixed reserve is 15 gallons and start-up/taxi allowance is 3 gallons.
Assume a 20 knot tail wind.
Ignore balance considerations.
The maximum cargo permitted for an Echo aeroplane on the charter flight described above is closest to -- A505 kg
- B603 kg
- C570 kg
- D563 kg
21Given:
Useable fuel [excluding reserves].......115 litres
Fuel flow...............................28 litres/hour
Ground speed............................95 kt
The maximum distance that can be covered on this flight is -- AGiven:
Useable fuel [excluding reserves].......115 litres
Fuel flow...............................28 litres/hour
Ground speed............................95 kt
The maximum distance that can be covered on this flight is - - B350 nm
- C390 nm
- D205 nm
- AGiven:
22Given:
Flight fuel required to the destination ..... 190 litres
Fixed reserve required ...................... 60 litres
Variable reserve ............................ 15% of flight fuel
Start-up and taxi allowance ................. 12 litres
Fuel flow for holding if required ........... 45 litres per hour
The aircraft whose flight planning details are given above has 350 litres of fuel at start-up.
The maximum time this aircraft could plan to hold at the destination aerodrome is closest to -- A90 min
- B133 min
- C80 min
- D60 min
23Given:
Fuel on board at start-up ........... 200 litres
Fixed reserve required .............. 55 litres
Variable reserve .................... 15% of flight fuel
Start-up and taxi allowance ......... 15 litres
Fuel flow for holding if required ... 45 litres per hour
The maximum flight fuel available for the aircraft whose flight planning details are given above is closest to -- A135 litres
- B126 litres
- C130 litres
- D113 litres
24Given:
Fuel on board at start-up ............ 180 litres
Fixed reserve required ............... 30 litres
Variable reserve ..................... 15% of flight fuel
Start-up and taxi allowance .......... 10 litres
Fuel flow during cruise .............. 40 litres per hour
Charter flight
The maximum flight time from departure to destination aerodrome that could be planned by the aircraft whose flight planning details are given above is closest to -- A196 min
- B210 min
- C183 min
- D270 min
25Given:
Estimated time interval for the flight ........ 155 min
Fixed reserve required ........................ 15 US gal
Variable reserve .............................. 15% of flight fuel
Start-up and taxi allowance ................... 3 US gal
Fuel flow during cruise ....................... 28 US gal per hour
Holding required at destination ............... 30 min @ 20 US gal per hour
The minimum fuel required at start-up for the flight described above is closest to -- A111 US gal
- B105 US gal
- C82 US gal
- D100 US gal
26Given:
Estimated time interval for the flight ......... 155 min
Time interval to nearest suitable alternate .... 40 min
Fixed reserve required ......................... 15 US gal
Variable reserve ............................... 15% of flight fuel
Start-up and taxi allowance .................... 3 US gal
Fuel flow during cruise......................... 28 US gal per hour
The minimum fuel required at start-up for the flight described above, including fuel to the nearest suitable alternate, is closest to -- A123 US gal
- B120 US gal
- C111 US gal
- D109 US gal
27Refer to the Echo loading data on page 18 to 21 of the supplement.
An Echo aeroplane has an empty weight and moment of 1970 kg and 480.00 index units respectively. It is loaded as follows:
Forward baggage compartment.........50 kg
Row 1...............................Pilot + passenger
Row 2................................2 passengers
(Assume each person on board weighs 77 kg)
If the loading is not changed and no fuel is added to the auxiliary tanks, determine the maximum weight of fuel that can be added to the main tanks without exceeding the forward limit of the centre of gravity- A159 kg
- B93 kg
- C261 kg
- D76 kg
28Given:
Distance for the proposed flight .............. 220 nm
Fuel flow expected during cruise .............. 75 litres per hour
True Air Speed expected at cruise ............. 150 kt
Fixed reserve required ........................ 55 litres
Variable reserve required ..................... 15% of flight fuel
Start-up and taxi allowance ................... 8 litres
Fuel on board at start-up ..................... 200 litres
Charter flight
The maximum headwind component that could be tolerated to allow the flight described above to proceed without refuelling is -- A15 kt
- B12 kt
- C5 kt
- Dnil
29An Echo aircraft has a basic empty weight and moment of 1963 kg and 490.75 index units respectively. It is loaded as follows:
Row 1 ....................... pilot and one passenger [77 kg each]
Row 2 ....................... two passengers [77 kg each]
Row 3 ....................... two passengers [77 kg each]
Nose compartment ............ 45 kg
Wing compartments ........... 40 kg
Rear compartment ............ 80 kg
Hard ballast is available in the form of 5 kg sand bags.
The minimum amount of ballast fuel that must be carried in the main tanks to keep the aircraft in balance throughout the flight, if no change is made in the existing load, is closest to -- A21 US gal
- B13 US gal
- C35 US gal
- Dnil
30An Echo aircraft has a basic empty weight and moment of 1971 kg and 484.5 index units respectively. It is loaded as follows:
Row 1 ...................... pilot and one passenger [77 kg each]
Row 2 ...................... 140 kg
Row 3 ...................... 140 kg
Wing compartments .......... 60 kg
Rear compartment ........... 125 kg
Hard ballast is available in the form of 5 kg sand bags.
The minimum amount of ballast fuel that must be carried in the main tanks to keep the aircraft in balance throughout the flight, if no change is made in the existing load, is closest to -- A29 US gal
- B44 US gal
- Cnil
- D79 US gal
Información
- Descripción
- CPL Performance Test sobre Online Test 2, creado por Arone Atu el 06/03/2017.
- Autor
- Arone Atu
- Idioma
- English
- Visitas
- 4
- Etiquetas
- Valoración
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