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757 typerating - 2023 > Ice próf > Flashcards

Ice próf Flashcards

1
Q

What is the maximum Takeoff and landing
altitude for the B757? (without high altitude
landing switch)
A. 8400 ft
B. 10.000 ft
C. 14.000 ft
D. No limit

A

A. 8400 ft

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2
Q

What indications can you expect when
equipment smoke is present?
A. one or both air conditioning packs switch to high flow
B. one or both recirculation fans turn off
C. the overboard exhaust valve opens
D. All correct

A

D. All correct

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3
Q

Leaving the aircraft in Burkina Faso for crew rest, 42°C OAT, electrical power on. Which procedure is required?
A. No procedure required
B. Two cabin doors open
C. One pack operating or equivalent ground cooling
D. Two packs operating is minimum required

A

C. One pack operating or equivalent ground cooling

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4
Q

The Engine anti ice operation is dependent upon engine bleed switch position
A. True
B. False

A

B. False

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5
Q

The EICAS msg „ENG HIGH STAGE“ displays when…
A. Engine bleed air temperature is excessive
B. Engine bleed air pressure is excessive
C. The engine is in high stage mode
D. The engine bleed air valve is closed.

A

B. Engine bleed air pressure is excessive

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6
Q

The EICAS msg „ENG BLEED VALVE“ displays
when…
A. Engine bleed air temperature is excessive
B. Engine bleed air pressure is excessive
C. The engine is in high stage mode
D. The engine bleed air valve is closed.

A

A. Engine bleed air temperature is excessive

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7
Q
  1. The EICAS msg „PACK TEMP“ displays when…
    A. Pack outlet temperature is excessive
    B. Pack internal temperature is excessive
    C. Pack controller fault
    D. All correct
A

D. All correct

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8
Q
  1. The EICAS msg „PACK OFF“ displays when…
    A. Pack switched off
    B. Pack internal temperature is excessive
    C. Pack controller fault
    D. A and B correct
A

D. A and B correct

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9
Q
  1. “The _____ recirculation fan should NOT be
    turned off as this causes the overboard
    exhaust valve to open.”
    A. Left
    B. Right
A

A. Left

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10
Q
  1. Equipment Cooling System. What below
    describes the forward system?
    A. One supply fan and Left recirc fan operate
    in normal operation
    B. Two supply fans and Left recirc fan
    operate in normal operation
    C. Only the L recirc fan operates in normal
    operation
    D. L and R recirc fan operate in normal
    operation
A

A. One supply fan and Left recirc fan operate
in normal operation

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10
Q
  1. The Zone Temperature controllers are set as
    follows: 22°C, 24°C, 25°C. What temperature
    will the packs output?
    A. 22°
    B. 24°
    C. 25°
    D. No way to tell
A

A. 22°

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11
Q
  1. What is accomplished by pushing the Equip Cooling switch to ALTN?
    A. Activates the alternate supply fan
    B. Activates the Right recirc fan
    C. Activates the Left recirc fan
    D. Opens the overboard exhaust valve
A

A. Activates the alternate supply fan

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12
Q
  1. At what cabin altitude does the CABIN
    ALTITUDE light illuminate?
    a) 8500
    b) 10000
    c) 14000
A

b) 10000

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13
Q
  1. What can cause a PACK OFF light to
    illuminate when the selector is in AUTO?
    a) Lack of air to the pack
    b) Excessive air flow
    c) Trim air switch off
A

a) Lack of air to the pack

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14
Q
  1. What does the pack INOP light indicate?
    a) Excessive pack temperature or
    controller fault.
    b) Loss of zone temperature controller
    c) Excessive trim air temp or pack valve
    closed.
A

a) Excessive pack temperature or
controller fault.

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15
Q
  1. What does it Indicate when the Isolation
    VALVE Light comes on?
    a) Valve and switch positions are not in
    agreement.
    b) The valve is open.
    c) The valve is closed.
A

a) Valve and switch positions are not in
agreement.

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16
Q
  1. The Trim Air Switch is off. What cabin
    temperature do the packs attempt to
    maintain?
    a) 50°F ( 10°C)
    b) 75°F ( 24°C)
    c) Variable, depending upon zone
    requirement
A

b) 75°F ( 24°C)

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17
Q
  1. What altitude setting should be set on the
    LDG ALT selector during Cockpit
    preparation?
    a) 200 ft. below takeoff airport elevation.
    b) Destination airport elevation.
    c) Cabin altitude as determined from
    placard.
A

b) Destination airport elevation.

18
Q
  1. During automatic temperature control,
    which temperature zone controls the output
    of the air conditioning packs?
    a) The zone requiring the coolest air.
    b) The zone requiring the warmest air.
    c) The zone with the warmest selection.
A

a) The zone requiring the coolest air.

19
Q
  1. One forward equipment cooling supply fan operates at a time. What causes the
    alternate fan to operate?
    a) High temperature in the forward E/E
    compartment
    b) Pushing the Alternate equipment
    Cooling switch.
    c) Low cooling air pressure.
A

b) Pushing the Alternate equipment
Cooling switch.

20
Q
  1. What limits are set by the AUTO RATE
    Control?
    a) Cruise altitude.
    b) Differential pressure.
    c) Cabin rates of climb and descent.
A

c) Cabin rates of climb and descent.

21
Q
  1. What type of power is used for outflow
    valve actuation during auto control?
    a) DC
    b) DC and AC
    c) AC
A

c) AC

22
Q
  1. When a pack selector is positioned to STBY N, what is the outlet temperature of the
    pack?
    a) Constant moderate temperature
    b) Variable, dependent upon zone
    requirements.
    c) Full cold.
A

a) Constant moderate temperature

23
Q

Flightcrew oxygen system; What is the normal setting?
A. 100%
B. N
Hvernig myndirðu eiga við unitið ef það væri smoke in the cockpit?

A

A. 100%
Myndirðu snúa takkanum til hægri, í átt að “emegerncy” möo Rotated in the direction of the arrow

24
Q

The passenger oxygen system is deployed
automatically when the cabin altitude reaches:
A. 12000 ft.
B. 14000 ft.
C. 15000 ft.

A

B. 14000 ft.

25
Q

The crew can escape from the cockpit using
the cockpit window Emergency pneumatic
slide.
A. True.
B. False.

A

B. False.

26
Q

With the EICAS computer selector in AUTO,
what happens if the left EICAS computer fails?
A. Left engine indications are blanked.
B. The right computer controls both CRTs.
C. The upper CRT is blanked.

A

B. The right computer controls both CRTs.

27
Q

The lower EICAS display (STATUS display)
shows what oxygen pressure?
a) Passenger oxygen pressure.
b) Cockpit crew oxygen pressure.
c) Flight attendant oxygen pressure

A

b) Cockpit crew oxygen pressure.

28
Q

The passenger oxygen system uses the same
source as the cockpit crew?
a) True.
b) False

A

b) False

29
Q
  1. The Engine anti-ice operation is dependent upon engine bleed switch position.
    a) True
    b) False
A

b) False

30
Q
  1. The windows are protected from thermal shock when the switches are initially placed on.
    a) True
    b) False
A

a) True

31
Q
  1. The Wing anti-ice operation is dependent upon engine bleed switch position.
    a) True
    b) False
A

a) True

32
Q
  1. What is used to compute engine thrust limit corrections for engine anti-ice?
    a) Engine anti-ice valve position
    b) Engine bleed air switch position
    c) Engine anti-ice switch position
A

c) Engine anti-ice switch position

33
Q
  1. Wing Anti-ice is on, what will the Wing anti-ice valves do when the airplane lands?
    a) Close.
    b) Remain open until wing anti-ice is turned
    off.
    c) Close only if an overheat condition exists.
A

a) Close.

34
Q
  1. If the left engine anti-ice switch is blank
    and its VALVE light on, what is the condition of the Left Engine Anti-ice Valve?
    a) Signaled open, and not open
    b) Signaled closed, and not closed.
    c) Signaled open, and is in transit.
A

b) Signaled closed, and not closed.

35
Q
  1. You are flying over the south Atlantic through the intertropical convergence zone. SAT is -54°C. Is aircraft icing possible?
    a) Airframe Icing: yes, engine icing: yes
    b) Airframe Icing: no, engine icing: no
    c) Airframe Icing: no, engine icing: yes
    d) Airframe Icing: yes, engine icing: no
A

c) Airframe Icing: no, engine icing: yes

36
Q
  1. OAT is 4°C in Keflavík with light rain.
    a) Engine anti ice must be on and a run up of 10 sec 60% N1 before takeoff must be
    accomplished
    b) Engine anti ice must be on but a run up before takeoff is not required
    c) Engine anti ice off and no run up
A

b) Engine anti ice must be on but a run up before takeoff is not required. Hefði verið 3°C eða kaldara þá hefðirðu þurft að gera runup.

37
Q
  1. When will the Ram Air Turbine extend
    automatically?
    a) When both engines fail in-flight.
    b) When either engine fails
    c) When center hydraulic system pressure is
    low.
A

a) When both engines fail in-flight.

38
Q
  1. What is indicated when one hydraulic pump “PRESS” light comes on?
    a) Pump output pressure low
    b) System pressure low.
    c) Pump output pressure high
A

a) Pump output pressure low

39
Q
  1. The Ram Air Turbine can be retracted in flight.
    a) True.
    b) False.
A

b) False.

40
Q
  1. Left and Right hydraulic system pressures are low. Is normal flap extension possible?
    a) Yes
    b) No
A

b) No

41
Q
  1. The Ram Air Turbine provides adequate
    hydraulic power down to…
    a) 200 kts
    b) 160 kts
    c) 130 kts
    d) 80 kts
A

c) 130 kts

42
Q
  1. Right and Center Hydraulic system pressure low. Is stabilizer trim available?
    a) No
    b) Yes, at 50% of normal rate
    c) Yes, at 25% of normal rate
    d) Yes, at normal rate
A

a) No

43
Q
  1. Is pressurization of the hydraulic reservoirs monitored?
    a) Yes
    b) No
  2. Your colleague on the flight deck inadvertently
    operates the alternate trim switches during
    cruise with C autopilot selected. What
    happens?
    a) Nothing happens
    b) ‘UNSCHD STAB TRIM’ EICAS msg
    appears
    c) The autopilot disconnects
    d) The airplane enters an attitude stabilizing
    mode
  3. Following the loss of which hydraulic system
    in-flight, results in the longest landing
    distance used?
    a) L with the loss of all hydraulic fluid
    b) R with the loss of all hydraulic fluid
    c) C with the loss of all hydraulic fluid
  4. Compared to a normal dry runway landing.
    How much longer is your landing distance
    following a loss of R and L hydraulic systems?
    (approx.)
    a) The landing distance doubles
    b) The landing distance increases 50%
    c) The landing distance increases 25%
    d) Nearly same landing distance
A

757 typerating - 2023 (21 decks)

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