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PROVA:
	P7 - COP
	
	
	
	
	
	
	
	
	SELEÇÃO PARA PILOTOS - AZUL LINHAS AÉREAS
	Nome:
	 
	 
	 
	 
	Assinatura:
	 
	 
	 
	
	Data:
	 
	/
	/
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	1)
	
	
	
	
	
	
	
	
	
	For a non pressurised aircraft, the supplemental oxygen is:
	( )
	A
	used for protection against smoke and carbon dioxide
	( )
	B
	available for supply to passengers for physiological reasons
	( X )
	C
	required to operate at pressure altitudes above 10 000ft
	( )
	D
	therapeutical oxygen specially carried for certain passengers
	
	
	
	
	
	
	
	
	
	
	2)
	
	
	
	
	
	
	
	
	
	The Alerting Service is provided by:
	( )
	A
	Only by ATC units
	( X )
	B
	The ATS unit responsible for the aircraft at that moment
	( )
	C
	The ATC unit responsible for the aircraft at that moment, when it is provided with 121.5 MHz
	( )
	D
	The Area Control Centers
	
	
	
	
	
	
	
	
	
	
	3)
	
	
	
	
	
	
	
	
	
	The Zero Fuel Weight and the Dry Operating Weight
	( X )
	A
	differ by the value of the traffic load weight
	( )
	B
	differ by the sum of the weight of usable fuel plus traffic load weight
	( )
	C
	are the same value
	( )
	D
	differ by the weight of usable fuel
	
	
	
	
	
	
	
	
	
	
	4)
	
	
	
	
	
	
	
	
	
	The STOPWAY is a defined rectangular area on the ground at the end of take-off run available prepared as a suitable area where:
	( x )
	A
	An aircraft can be stopped in the case of an abandoned take-off
	( )
	B
	A landing aircraft can be stopped if overcoming the end of runway
	( )
	C
	A landing aircraft can be stopped only in emergency
	( )
	D
	An aircraft taking-off or landing can be stopped
	
	
	
	
	
	
	
	
	
	
	5)
	
	
	
	
	
	
	
	
	
	An aircraft in distress shall send the following signal by radiotelephony:
	( )
	A
	PAN PAN, PAN PAN, PAN PAN
	( x )
	B
	MAYDAY, MAYDAY, MAYDAY
	( )
	C
	URGENCY, URGENCY, URGENCY
	( )
	D
	DETRESFA, DETRESFA, DETRESFA
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	6)
	
	
	
	
	
	
	
	
	
	Definitions - Aerodrome. A defined rectangular area, selected or prepared as a suitable area over which an aeroplane may make a portion of its initial climb to a specified height is called:
	( )
	A
	Runway end safety area (RESA)
	( x )
	B
	Clearway
	( )
	C
	Take-off run available (TORA)
	( )
	D
	Stopway
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	7)
	
	
	
	
	
	
	
	
	
	In a 5 kt right crosswind component behind a taking off aircraft:
	( )
	A
	the right and left wake turbulence stays approximately on the runway
	( )
	B
	the left wake turbulence stays approximately on the runway
	( )
	C
	the runway will be clear of any hazard turbulence
	( X )
	D
	the right wake turbulence stays approximately on the runway
	
	
	
	
	
	
	
	
	
	
	8)
	
	
	
	
	
	
	
	
	
	A message preceded by the phrase "Transmitting blind due receiver failure" shall be transmitted:
	( )
	A
	On the company frequency
	( )
	B
	On the international emergency frequency
	( X )
	C
	On the frequency presently in use
	( )
	D
	On all available aeronautical stations
	
	
	
	
	
	
	
	
	
	
	9)
	
	
	
	
	
	
	
	
	
	When an aircraft is no longer in distress, it shall transmit a message cancelling the distress condition. Which words shall this message include ?
	( X )
	A
	... Cancel distress
	( )
	B
	... MAYDAY cancelled
	( )
	C
	... Distress condition terminated
	( )
	D
	... MAYDAY, resuming normal operations
	
	
	
	
	
	
	
	
	
	
	10)
	
	
	
	
	
	
	
	
	
	The most common sensors interfacing a FMS to compute the aircraft position along the flight plan are: 1- GPS 2- NDB 3- DME 4- LOCALIZER The combination which regroups all of the correct statements is:
	( X )
	A
	1, 3
	( )
	B
	1, 4
	( )
	C
	1, 2, 3
	( )
	D
	2, 3
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	11)
	
	
	
	
	
	
	
	
	
	On a pressurised aeroplane, supplemental oxygen is used to:
	( )
	A
	assist a passenger with breathing disorders
	( X )
	B
	provide passengers on board with oxygen following a cabin depressurisation
	( )
	C
	provide selected passengers with oxygen
	( )
	D
	protect the aircrew fighting fires
	
	
	
	
	
	
	
	
	
	
	12)
	
	
	
	
	
	
	
	
	
	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, 3, 4, 5
	( )
	C
	1, 2, 4, 5
	( )
	D
	2, 4, 5
	
	
	
	
	
	
	
	
	
	
	13)
	
	
	
	
	
	
	
	
	
	If warning, caution, or advisory lights are installed in the cockpit, they must, unless otherwise approved by the Authority, be red for:
	( )
	A
	caution lights
	( )
	B
	advisory lights
	( )
	C
	other distress messages
	( )
	D
	warning lights
	
	
	
	
	
	
	
	
	
	
	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
	( )
	D
	1, 4, 5
	
	
	
	
	
	
	
	
	
	
	15)
	
	
	
	
	
	
	
	
	
	Fuel loaded onto an aeroplane is 15400 kg but is erroneously entered into the load and trim sheet as 14500 kg. This error is not detected by the flight crew but they will notice that
	( )
	A
	speed at un-stick will be higher than expected
	( )
	B
	the aeroplane will rotate much earlier than expected
	( )
	C
	V1 will be increased
	( )
	D
	V1 will be reached sooner than expected
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	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
	( X )
	C
	7000
	( )
	D
	8350
	
	
	
	
	
	
	
	
	
	
	17)
	
	
	
	
	
	
	
	
	
	When completing an ATC flight plan, 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)
	
	
	
	
	
	
	
	
	
	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 ?
	( )
	A
	at the destination there will still be 30.000 KG in the tanks
	( )
	B
	at departure the reserve fuel was 28.000 KG
	( )
	C
	the remaining fuel is not sufficient to reach the destination with reserves intact
	( )
	D
	at destination the required reserves remain intact
	
	
	
	
	
	
	
	
	
	
	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 retracted21)
	
	
	
	
	
	
	
	
	
	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
	
	
	
	
	
	
	
	
	
	
	22)
	
	
	
	
	
	
	
	
	
	Given: Planned and actual data as shown in the Flight Log excerpt. Arriving overhead GAMMA you are cleared for direct routeing to MIKE. The flight time for direct flight GAMMA to MIKE will be 57 minutes, assuming other flight data remains constant, what fuel will be expected on arrival overhead MIKE?
	Waypoint
	ETA (h:min)
	ATA (h:min)
	Planned Remaining Fuel (kg)
	Actual Remaining Fuel (kg)
	
	
	ALPHA
	1:07
	1:07
	3400
	3400
	
	
	BETA
	1:37
	1:37
	3010
	2950
	
	
	GAMMA
	2:02
	2:02
	2685
	2575
	
	
	DELTA
	2:37
	 
	2230
	 
	
	
	SIERRA
	3:22
	 
	1645
	 
	
	
	MIKE
	3:37
	 
	1450
	 
	
	
	( )
	A
	790 kg
	( )
	B
	1720 kg
	( )
	C
	2305 kg
	( )
	D
	1450 kg
	
	
	
	
	
	
	
	
	
	
	23)
	
	
	
	
	
	
	
	
	
	The purpose of Auto Throttle is:
	( )
	A
	to deactivate manual throttles and transfer engine control to Auto Pilot
	( )
	B
	to synchronize engines to avoid "yawing"
	( )
	C
	to maintain constant engine power or aeroplane speed
	( )
	D
	to automatically shut down an engine if it is at too high temperature.
	
	
	
	
	
	
	
	
	
	
	24)
	
	
	
	
	
	
	
	
	
	In a precision approach category I lighting system, the center line and crossbar lights shall be:
	( )
	A
	flashing lights showing variable white
	( )
	B
	flashing lights showing variable green
	( )
	C
	fixed lights showing variable white
	( )
	D
	fixed lights showing variable green
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	25)
	
	
	
	
	
	
	
	
	
	The term drift refers to the wander of the axis of a gyro in:
	( )
	A
	any plane
	( )
	B
	the vertical plane
	( X )
	C
	the horizontal plane
	( )
	D
	the vertical and horizontal plane
	
	
	
	
	
	
	
	
	
	
	26)
	
	
	
	
	
	
	
	
	
	When severe mountain waves are present, where would the area of most severe turbulence be located?
	( )
	A
	In the rotor zone
	( )
	B
	Just above the cap cloud
	( )
	C
	On the windward side of the mountain range
	( )
	D
	Just below the tropopause
	
	
	
	
	
	
	
	
	
	
	27)
	
	
	
	
	
	
	
	
	
	An increase in atmospheric pressure has, among other things, the following consequences on landing performance:
	( )
	A
	an increased landing distance and improved go-around performance
	( )
	B
	an increased landing distance and degraded go-around performance
	( )
	C
	a reduced landing distance and degraded go around performance
	( X )
	D
	a reduced landing distance and improved go-around performance
	
	
	
	
	
	
	
	
	
	
	28)
	
	
	
	
	
	
	
	
	
	An aft CG shift:
	( )
	A
	has no influence on static longitudinal stability
	( )
	B
	decreases longitudinal manoeuvrability
	( )
	C
	increases longitudinal manoeuvrability
	( )
	D
	increases static longitudinal stability
	
	
	
	
	
	
	
	
	
	
	29)
	
	
	
	
	
	
	
	
	
	Which elements of instructions or information shall always be read back ?
	( )
	A
	Surface wind, visibility, ground temperature, runway-in-use, altimeter settings, heading and speed instructions
	( )
	B
	Runway-in-use, visibility, surface wind, heading instructions, altimeter settings
	( )
	C
	Time check, runway-in-use, altimeter settings, level instructions, SSR codes
	( X )
	D
	Runway-in-use, altimeter settings, SSR codes, level instructions, heading and speed instructions
	
	
	
	
	
	
	
	
	
	
	30)
	
	
	
	
	
	
	
	
	
	What does the word "disregard" mean ?
	( )
	A
	Annul the previously transmitted clearance
	( X )
	B
	Consider that transmission as not sent
	( )
	C
	An error has been made in this transmission
	( )
	D
	Wait and I will call you
	31)
	
	
	
	
	
	
	
	
	
	The primary duty provided by a radar unit is:
	( )
	A
	to assist aircraft on the location storms
	( )
	B
	to provide radar separation
	( )
	C
	to assist aircraft due to failure of airborne equipment
	( )
	D
	to assist aircraft where navigation appears unsatisfactory
	
	
	
	
	
	
	
	
	
	
	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)
	
	
	
	
	
	
	
	
	
	The center of gravity of an aircraft is that point through which the total weight of the aircraft is said to act. The weight acts in a direction
	( )
	A
	parallel to the gravity vector
	( )
	B
	at right angles to the flight path
	( )
	C
	always parallel to the aircraft's vertical axis
	( )
	D
	governed by the distribution of the weight within the aircraft
	
	
	
	
	
	
	
	
	
	
	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
	( X )
	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 weight of an item multiplied by it's distance from the datum is it's
	( X )
	A
	Moment
	( )
	B
	Moment arm
	( )
	C
	Force
	( )
	D
	Center of gravity
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	36)
	
	
	
	
	
	
	
	
	
	VFR flights shall not be flown over the congested areas of cities at a height less than
	( )
	A
	2000 ft above the highest obstacle within a radius of 600 ft from the aircraft
	( )
	B
	1000 ft above the highest obstacle within a radius of 600 m from the aircraft
	( )
	C
	500 ft above the highest obstacle
	( )
	D
	the highest obstacle
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	
	37)
	
	
	
	
	
	
	
	
	
	Which of the following weather reports could be, in accordance with the regulations, abbreviated to "CAVOK"?
	( )
	A
	34004KT 7000 MIFG SCT260 09/08 Q1029 BECMG 1600 =
	( )
	B
	26012KT 8000 SHRA BKN025 16/12 Q1018 NOSIG=
	( X )
	C
	27019G37KT 9999 BKN050 18/14 Q1016 NOSIG=
	( )
	D
	00000KT 0100 FG VV001 11/11 Q1025 BECMG 0500=
	
	
	
	
	
	
	
	
	
	
	38)
	
	
	
	
	
	
	
	
	
	Given: Maximum structural take-off weight= 146 900 kg, Maximum structural landing weight= 93 800 kg, Maximum zero fuel weight= 86 400 kg, Trip fuel= 27 500 kg, Block fuel= 35 500 kg; Engine starting and taxi fuel = 1 000 kg. The maximum take-off weight is equal to:
	( X )
	A
	120.900 KG
	( )
	B
	121.300 KG
	( )
	C
	120.300 KG
	( )
	D
	113.900 KG
	
	
	
	39)
	
	
	
	
	
	
	
	
	
	Which does ATC Term "Radar contact" signify?
	( )
	A
	Your aircraft has been identified on the radar display and radar flight instructions will be provided until radar identification is terminated
	( )
	B
	You will be given traffic advisories until advised that the service has been terminated or that radar contact has been lost
	( )
	C
	ATC is receiving your transponder and will furnish vectors and traffic advisories until you are advised that contact has been lost
	( )
	D
	Your aircraft has been identified and you will receive separation from all aircraft while in contact with this radar facility
	
	
	
	
	
	
	
	
	
	
	40)
	
	
	
	
	
	
	
	
	
	Clearance on Final Approach. A pilot may expect toreceive the clearance to land or any alternative clearance before the aircraft reaches a distance of:
	( X )
	A
	2 NM from touchdown
	( )
	B
	3 NM from touchdown
	( )
	C
	4 NM from touchdown
	( )
	D
	5 NM from touchdown
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