PROVA - P9 COP

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	P9 - COP
	
	
	
	
	
	
	
	
	SELEÇÃO PARA PILOTOS - AZUL LINHAS AÉREAS
	Nome:
	 
	 
	 
	 
	Assinatura:
	 
	 
	 
	
	Data:
	 
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	1)
	
	
	
	
	
	
	
	
	
	Following a heavy weight landing on a short runway, you should pay attention to the:
	( )
	A
	pressure of the hydraulic fluid
	( X )
	B
	temperature of the brakes
	( )
	C
	temperature of the hydraulic fluid
	( )
	D
	pressure of the pneumatic system
	
	
	
	
	
	
	
	
	
	
	2)
	
	
	
	
	
	
	
	
	
	From which of the following would you expect to find the dates and times when temporary danger areas are active
	( )
	A
	SIGMET
	( X )
	B
	NOTAM and AIP
	( )
	C
	RAD/NAV charts
	( )
	D
	Only AIP
	
	
	
	
	
	
	
	
	
	
	3)
	
	
	
	
	
	
	
	
	
	In the ATS flight plan Item 15, for a flight along a designated route, where the departure aerodrome is not on or connected to that route :
	( X )
	A
	the letters "DCT" should be entered, followed by the point of joining the ATS route
	( )
	B
	it is not necessary to indicate the point of joining that route as it will be obvious to the ATS unit
	( )
	C
	the words "as cleared" should be entered
	( )
	D
	it is necessary only to give the first reporting point on that route
	
	
	
	
	
	
	
	
	
	
	4)
	
	
	
	
	
	
	
	
	
	An aeroplane suffers an explosive decompression at an altitude of 31000 ft . What is the initial action by the operating crew ?
	( X )
	A
	to put on oxygen masks
	( )
	B
	transmit a MAYDAY message
	( )
	C
	place the seat belts sign to ON
	( )
	D
	disconnect the autopilot
	
	
	
	
	
	
	
	
	
	
	5)
	
	
	
	
	
	
	
	
	
	Declared Distances "ASDA" (Acceleration Stop Distance Available) is:
	( )
	A
	The length of the runway plus the length of stop way available (if stop way provided)
	( X )
	B
	The length of the take-off run available plus the length of stop way (if stop way provided)
	( )
	C
	The length of the take-off run available plus the length of clearway
	( )
	D
	The length of the take-off run available plus the length of stop way and clearway (if provided)
	6)
	
	
	
	
	
	
	
	
	
	What is the name of an area beyond the end of a rwy which does not contain obstructions and can be considered when calculating takeoff performance of turbin-powered aircraft?
	( )
	A
	stopway
	( X )
	B
	clearway
	( )
	C
	obstruction clearance plane
	( )
	D
	safety area
	
	
	
	
	
	
	
	
	
	
	7)
	
	
	
	
	
	
	
	
	
	The Density Altitude
	( )
	A
	is equal to the pressure altitude
	( )
	B
	is used to calculate the FL above the transition altitude
	( )
	C
	is used to establish minimum clearance of 2000 feet over mountains
	( X )
	D
	is used to determine the aeroplane performance
	
	
	
	
	
	
	
	
	
	
	8)
	
	
	
	
	
	
	
	
	
	Which is true of the aircraft basic empty weight?
	( )
	A
	it is dry operating weight minus traffic load
	( )
	B
	it is dry operating weight minus fuel load
	( X )
	C
	it is a component of dry operating weight
	( )
	D
	it is the actual take-off weight, less traffic load
	
	
	
	
	
	
	
	
	
	
	9)
	
	
	
	
	
	
	
	
	
	The fuel plan gives a trip fuel of 65.000 KG. The alternate fuel, final reserve included, is 17.000 KG. Contingency fuel is 5% of the trip fuel. The usable fuel at departure is 93.000 KG. At a certain moment the fuel consumed according to the fuel gauges is 40.000 KG and the distance flown is half of the total distance. Assume that fuel consumption doesn't change. Which statement is right ?
	( X )
	A
	the remaining fuel is not sufficient to reach the destination with reserves intact
	( )
	B
	at departure the reserve fuel was 28.000 KG
	( )
	C
	at the destination there will still be 30.000 KG in the tanks
	( )
	D
	at destination the required reserves remain intact
	
	
	
	
	
	
	
	
	
	
	10)
	
	
	
	
	
	
	
	
	
	The speed used to determine the "maximum tyre-speed limit" is the:
	( )
	A
	groundspeed
	( )
	B
	TAS
	( X )
	C
	IAS
	( )
	D
	EAS
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	11)
	
	
	
	
	
	
	
	
	
	An aeroplane has the following weights; ESTLWT= 50 000 kg, Trip fuel= 4 300 kg, Contingency fuel= 215 kg, Alternate fuel (final reserve included)= 2 100kg, Taxi= 500 kg, Block fuel= 7 115 kg. Before departure the captain orders to make the block fuel 9 000 kg. The trip fuel in the operational flight plan should read:
	( )
	A
	9000 kg
	( X )
	B
	4300 kg
	( )
	C
	6185 kg
	( )
	D
	6400 kg
	
	
	
	
	
	
	
	
	
	
	12)
	
	
	
	
	
	
	
	
	
	What will be the influence on the aeroplane performance if aerodrome pressure altitude is increased?
	( )
	A
	it will decrease the take-off run
	( X )
	B
	it will increase the take-off distance
	( )
	C
	it will increase the take-off distance available
	( )
	D
	it will decrease the take-off distance
	
	
	
	
	
	
	
	
	
	
	13)
	
	
	
	
	
	
	
	
	
	The optimum altitude
	( )
	A
	decreases as weight decreases
	( )
	B
	is the altitude at which the specific range reaches its minimum
	( )
	C
	is the altitude up to which cabin pressure of 8.000 ft can be maintained
	( X )
	D
	increases as weight decreases and is the altitude at which the specific range reaches its maximum
	
	
	
	
	
	
	
	
	
	
	14)
	
	
	
	
	
	
	
	
	
	The role of the FMS is to:; 1 - aid the crew with navigation; 2 - shut down the engine in case of a malfunction ; 3 - automatically avoid conflicting traffic when autopilot engaged ; 4 - reduce crew workload; 5 - aid fuel efficiency; The combination that regroups all of the correct statements is:
	( )
	A
	1, 2, 3
	( )
	B
	2, 3, 4, 5
	( )
	C
	1, 3, 4
	( X )
	D
	1, 4, 5
	
	
	
	
	
	
	
	
	
	
	15)
	
	
	
	
	
	
	
	
	
	A METAR reads : SA1430 35002KT 7000 SKC 21/03 QI024 =; Which of the following information is contained in this METAR ?
	( X )
	A
	temperature/dewpoint
	( )
	B
	day/month
	( )
	C
	period of validity
	( )
	D
	runway in use
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	16)
	
	
	
	
	
	
	
	
	
	Given: Maximum structural take-off weight: 8350 kg Maximum structural landing weight: 8350 kg Zero Fuel weight: 6210 kg Taxi Fuel: 10 kg Contingency Fuel:90 kg. Alternate Fuel: 300 kg. Final Reserve Fuel: 400 kg. Trip Fuel: 780 kg; The expected Landing weight at destination will be:
	
	( )
	A
	7790
	( )
	B
	7780
	( )
	C
	7000
	( )
	D
	8350
	
	
	
	
	
	
	
	
	
	
	17)
	
	
	
	
	
	
	
	
	
	When completing an ATC flight plan for a European destination, clock times are to be expressed in:
	( )
	A
	local standart time
	( )
	B
	local mean time
	( )
	C
	central european time
	( X )
	D
	UTC
	
	
	
	
	
	
	
	
	
	
	18)
	
	
	
	
	
	
	
	
	
	Due to standing water on the runway the field length limited take-off weight will be
	( )
	A
	higher
	( )
	B
	unaffected
	( )
	C
	only higher for three and four engine aeroplanes
	( X )
	D
	lower
	
	
	
	
	
	
	
	
	
	
	19)
	
	
	
	
	
	
	
	
	
	Traffic load is the difference between:; 
	( )
	A
	the take-off weight and the basic empty weight
	( )
	B
	the take-off weight and the basic empty weight plus trip fuel
	( X )
	C
	the take-off weight and the operating weight
	( )
	D
	the operating weight and the basic empty weight
	
	
	
	
	
	
	
	
	
	
	20)
	
	
	
	
	
	
	
	
	
	The second segment begins
	( )
	A
	when flap retraction begins
	( )
	B
	when flap are selected up
	( )
	C
	when acceleration starts from V2 to the speed for flap retraction
	( X )
	D
	when landing gear is fully retracted
	
	
	
	
	
	
	
	
	
	
	21)
	
	
	
	
	
	
	
	
	
	During a night flight, an observer located in the cockpit, seeing an aircraft coming from front left on approximate opposite parallel track, will first see the:
	( )
	A
	white steady light
	( X )
	B
	red steady light
	( )
	C
	green steady light
	( )
	D
	green and white flashing light
	
	
	
	
	
	
	
	
	
	
	22)
	
	
	
	
	
	
	
	
	
	The actual 'Take-off Weight' is equivalent to:
	( )
	A
	actual zerofuel weight plus the traffic load
	( )
	B
	dry operating weight plus take-off fuel and the traffic load
	( )
	C
	dry operating weight plus the take-off fuel
	( )
	D
	actual landing weight plus the take-off fuel
	
	
	
	
	
	
	
	
	
	
	23)
	
	
	
	
	
	
	
	
	
	In establishing the aerodrome operating minima which will apply to any particular operation, an operator must take full account of:; 1. equipment available on the aircraft; 2. dimensions and characteristics of the runways; 3. composition of the flight crew; 4. obstacles in the vicinity of approach and missed approach areas; 5. facilities for determining and communicating the weather conditions; The combination regrouping all the correct statements is :
	( )
	A
	2, 3, 5
	( )
	B
	1, 2, 4, 5
	( )
	C
	1, 2, 3, 4, 5
	( )
	D
	2, 4, 5
	
	
	
	
	
	
	
	
	
	
	24)
	
	
	
	
	
	
	
	
	
	On an ATC flight plan you are required to indicate in the box marked "speed" the planned speed for the first part of the cruise or for the entire cruise. This speed is:
	( )
	A
	the equivalent airspeed
	( )
	B
	the estimated ground speed
	( )
	C
	the true airspeed
	( )
	D
	the indicated airspeed
	
	
	
	
	
	
	
	
	
	
	25)
	
	
	
	
	
	
	
	
	
	What effect has a centre of gravity close to the most forward limit?
	( )
	A
	a decreased induced drag
	( )
	B
	a better rate of climb capability
	( X )
	C
	a reduced rate of climb capability
	( )
	D
	a reduction in the specific fuel consumption
	
	
	
	
	
	
	
	
	
	
	26)
	
	
	
	
	
	
	
	
	
	The result of a higher flap setting up to the optimum at take-off is
	( )
	A
	a shorter ground roll
	( )
	B
	a longer take-off run
	( )
	C
	a higher V1
	( )
	D
	an increased acceleration
	
	
	
	
	
	
	
	
	
	
	27)
	
	
	
	
	
	
	
	
	
	For an ATC flight plan filed before the flight, the indicated time of departure is:
	( )
	A
	the time at which the flight plan is filed
	( )
	B
	the time overhead the first reporting point after take-off
	( )
	C
	the time of take-off
	( X )
	D
	the estimated off-block time
	
	
	
	
	
	
	
	
	
	
	28)
	
	
	
	
	
	
	
	
	
	If severe turbulence is encountered, which procedure is recommended?
	( )
	A
	Maintain a constant altitude
	( )
	B
	Maintain constant airspeed and altitude
	( X )
	C
	Maintain a constant attitude
	
	
	
	
	
	
	
	
	
	
	
	
	
	29)
	
	
	
	
	
	
	
	
	
	How should reverse thrust propellers be used during landing for maximum effectiveness in stopping?
	( )
	A
	Gradually increase reverse power to maximum as rollout speed decreases.
	( )
	B
	A, C and D
	( )
	C
	Select reverse-pitch after landing and use idle power setting of the engines.
	( X )
	D
	Use maximum reverse power as soon as possible after touchdown.
	
	
	
	
	
	
	
	
	
	
	30)
	
	
	
	
	
	
	
	
	
	Which of the following statements is true ?
	( )
	A
	QNH is always equal to QFE
	( X )
	B
	QNH can be equal to QFE
	( )
	C
	QNH is always lower than QFE
	( )
	D
	QNH is always higher than QFE
	
	
	
	
	
	
	
	
	
	
	31)
	
	
	
	
	
	
	
	
	
	For the purpose of completing the Weight and Balance documentation, the Traffic Load is considered to be equal to the Take-off weight
	( )
	A
	less the trip fuel weight
	( X )
	B
	less the operating weight
	( )
	C
	plus the trip fuel weight
	( )
	D
	plus the operating weight
	
	
	
	
	
	
	
	
	
	
	32)
	
	
	
	
	
	
	
	
	
	An additional baggage container is loaded into the aft cargo compartment but is not entered into the load and trim sheet. The aeroplane will be heavier than expected and calculated take-off safety speeds
	( )
	A
	will be greater than required
	( )
	B
	will give reduced safety margins
	( )
	C
	will not be achieved
	( )
	D
	are unaffected but V1 will be increased
	
	
	
	
	
	
	
	
	
	
	33)
	
	
	
	
	
	
	
	
	
	Which procedure produces the minimum fuel consumption for a given leg of the cruise flight?
	( X )
	A
	Increase speed for a headwind
	( )
	B
	Increase speed for a tailwind
	( )
	C
	Increase altitude for a headwind, decrease altitude for a tailwind
	( )
	D
	B and C
	34)
	
	
	
	
	
	
	
	
	
	An aircraft has two certified landing flaps positions, 25° and 35°. If a pilot chooses 25° instead of 35°, the aircraft will have:
	( )
	A
	an increased landing distance and degraded go-around performance
	( )
	B
	an increased landing distance and better go-around performance
	( )
	C
	a reduced landing distance and better go-around performance
	( )
	D
	a reduced landing distance and degraded go-around performance
	
	
	
	
	
	
	
	
	
	
	35)
	
	
	
	
	
	
	
	
	
	The take-off distance required increases
	( X )
	A
	due to slush on the runway
	( )
	B
	due to lower gross weight at take-off
	( )
	C
	due to head wind because of the drag augmentation
	( )
	D
	due to downhill slope because of the smaller angle of attack
	
	
	
	
	
	
	
	
	
	
	36)
	
	
	
	
	
	
	
	
	
	Considering only structural limitations, on very short legs with minimum take-off fuel, the traffic load is normally limited by:
	( )
	A
	MTOW
	( )
	B
	MZFW
	( )
	C
	MLW
	( )
	D
	ALW
	37)
	
	
	
	
	
	
	
	
	
	The maximum speed during takeoff that the pilot may abort the takeoff and stop the airplane within the accelerate-stop distance is:
	( )
	A
	V2
	( )
	B
	Vef
	( X )
	C
	V1
	( )
	D
	Vr
	
	
	
	
	
	
	
	
	
	
	38)
	
	
	
	
	
	
	
	
	
	What effect does an uphill runway slope have upon takeoff performance?
	( )
	A
	Increases takeoff distance
	( )
	B
	Decreases takeoff speed
	( )
	C
	Decreases takeoff distance
	
	
	
	39)
	
	
	
	
	
	
	
	
	
	Which condition reduces the required runway for takeoff?
	( X )
	A
	Increased headwind component
	( )
	B
	Lower-than-standard air density
	( )
	C
	Higher-than-recommended airspeed before rotation
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	40)
	
	
	
	
	
	
	
	
	
	What should a pilot do to maintain "best range" airplane performance when a tailwind is encountered?
	( )
	A
	Decrease speed
	( )
	B
	Maintain speed
	( )
	C
	Increase speed
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