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Frontier Airbus > Systems - June 22 Update > Flashcards

Systems - June 22 Update Flashcards

1
Q

SYSTEMS -

If you have a DMC failure what is displayed on the screen?

A

“Invalid Data”

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2
Q

SYSTEMS -

When the RAT deploys and the EMER GEN is coupled which screens do you have?

A
  • CA PFD
  • ND
  • E/WD
  • MCDU 1
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3
Q

SYSTEMS -

What provides Predictive and Reactive Windshear Warnings? When are those systems active?

A
  • Predictive is a function of the weather radar and looks 5nm ahead of the aircraft.
    • Active on the ground up to 100kts.
    • Active again from 50ft until 1800
    • Active on landing from 1800 until 50ft.
  • Reactive is a function of the FACs and alerts the crew when windshear conditions have been entered. The FAC measures the difference between the current energy state and the minimum energy state for safe flight.
    • On takeoff: Active from 3 seconds after liftoff until 1300ft.
    • On landing: Active from 1300ft to 50ft.
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4
Q

SYSTEMS -

What functions do the SECs provide?

A

PARSS

  • Pitch
  • Abnormal attitudes
  • Roll
  • Speed brakes
  • Spoilers
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5
Q

SYSTEMS-

What indication is there for each of the three ECAM levels of warning/caution?

A
  1. Amber on EWD with no Master Caution
  2. Amber on EWD with a Master Caution
  3. Red on EWD with a Master Warning

Vol II 9.20 pg 1

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6
Q

SYSTEMS -

On battery power only which screens are displayed?

A
  • Capt PFD
  • E/WD
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7
Q

SYSTEMS -

When will fuel from the outer wing tanks transfer to the inner wing tanks?

A

1650lbs in either inner wing tank

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8
Q

SYSTEMS -

What functions do the FACs provide?

A

BeSWiFT RATTY

  • BEta target and normal side slip indications
    • Flaps 1,2,3
    • 1 engine above 80% N1
    • More than a 35% N1 split
  • Speed, speed, speed
    • Low energy warning
    • Flaps 2 to FULL, 2000’ to 100’
    • Forewarns of Alpha Floor
  • WIndshear
    • Reactive
    • 3 sec after liftoff to 1300’
    • 1300’ to 50’
  • Flight envelope protections
    • speed tape symbology
  • Tail
    • Rudder limiting
    • Alternate law yaw
    • Turn coordination
    • Trim
    • Yaw damping
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9
Q

SYSTEMS -

What is Alpha Lock?

A

Alpha lock inhibits slat retraction at high AoA and low speeds

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10
Q

SYSTEMS -

At what speed does the anti-skid deactivate?

A

Below 20kts

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11
Q

SYSTEMS -

Above what speed is landing gear extension inhibited?

A

260kts

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12
Q

SYSTEMS -

What are the maximum pitch, roll and airspeed that the aircraft can reach due to external factors and remain in Normal Law?

A
  • Roll: 125 degree
  • Pitch: 50 degrees NU, -30 degrees ND
  • Max Speed: 440 kias, .91 Mach
  • Min Speed: 70-90 knots
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13
Q

SYSTEMS -

When in the EMERGENCY ELECTICAL CONFIGURATION what happens at:

  • 140 knots
  • 125 knots
  • 100 knots
  • 50 knots
  • Stopped
A
  • 140
    • RAT may stall
  • 125
    • RAT may be useable down to this speed (2 screens)
  • 100
    • DC BATTERY BUS is powered by BATs (no change - 2 screens)
  • 50
    • AC ESS BUS shed (no screens)
  • Stopped
    • Outflow valve (manual DC motor control)
    • APU Fire Protection and Detection
    • VHF-1
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14
Q

SYSTEMS -

Alternate Law: BYPALS

A
  • Bank
    • No Protection
  • Yaw
    • Damping only
  • Pitch
    • No Protection
  • AoA
    • VLS, VSW
  • Load
    • 2.5 to -1 Clean
    • 2.0 to 0 Dirty
  • Speed
    • High and Low speed stabilities may be available depending on failures.
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15
Q

SYSTEMS -

If a display screen fails what is you indication?

A

A “F” will be displayed.

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16
Q

SYSTEMS -

What is the maximum pitch, roll and speed a pilot can command and remain in Normal Law?

A
  • Roll: 67 degrees
  • Pitch: 30 degrees NU, -15 degrees ND
  • Max speed: VMO +30
  • Min Speed: alpha Max
17
Q

SYSTEMS -

Normal Law: BYPALS

A
  • Bank
    • 67 degrees max input, 33 degrees without constant pilot input
    • FD/AP lost at 45 degrees
    • FD/AP regained at 40 degrees
  • Yaw
    • Damping and turn coordination
  • Pitch
    • Flaps 0-3: 25-30 degrees NU
    • Flaps FULL: 20-25 degrees NU
      • Lose AP and FD at 25 degrees and regain at 22 degrees.
    • All Config: -15 degrees ND
      • Lose FD and AP at -13 degrees and regain at -10
  • AoA
    • VMAX, VLS, a Prot, a Max
  • Load
    • 2.5 to -1 Clean
    • 2.0 to 0 Dirty
  • Speed
    • VMO +16 pitch nose down authority smoothly reduced to zero.
18
Q

SYSTEMS -

Which displays does each DMC run?

A
  • DMC1 - PFD1, ND1, EWD and SD
  • DMC2 - PFD2 and ND2

Failure of DMC1 will automatically cause DMC2 to power EWD and SD.

19
Q

SYSTEMS -

How many green arrows on the E/WD are needed to confirm each gear are down and locked?

A

1 per gear.

The two triangles represent a signal from LGCIU 1 and LGCIU 2. If either is green the gear is locked in the down position.

20
Q

SYSTEMS -

Which CRC events cannot be canceled by the Master Warning?

A
  • Stall
  • Overspeed
  • Landing Gear not down below 750’
21
Q

SYSTEMS -

When alpha Prot is activated what happens?

A

BASAP

  • Bank limited to 45 degrees
  • Autopilot is disconnected
  • Spoilers are retracted
  • AoA demand instead of load demand
  • Pitch up trim inhibited
22
Q

SYSTEMS -

Direct Law: BYPALS

A
  • Bank
    • No Protections
  • Yaw
    • Mechanical Rudder control
  • Pitch
    • No Protections
  • AoA
    • VLS, VSW
  • Load
    • No Protections
  • Speed
    • Aural overspeed warning only
23
Q

SYSTEMS

What warnings are NOT inhibited during takeoff?

A
  • FWC 1+2 FAULT
  • ENG 1(2) FIRE
  • L+R ELEV FAULT
  • L(R) SIDESTICK FAULT
  • DUAL INPUT
  • APU FIRE
  • DUAL ENG FAILURE

(FELLDAD)

Vol II 4.05 pg 11

24
Q

SYSTEMS -

Above what brake temperature whould we avoid applying the parking brake?

A

500 degrees

Vol 3.20 pg 3

25
Q

SYSTEMS-

Is there a limitation on how long the aircraft should be left powered up with no cooling?

A

The aircraft electrical system should not be powered for more than 2 hours without a cooling system when the outside air temperature is above 49°C.

Vol II 2.10 pg 1

26
Q

SYSTEMS -

When is Alpha Floor protection available?

A

Liftoff to 100’ on approach

27
Q

SYSTEMS -

What functions do the ELACs provide?

A
  • PARAAA
  • Pitch
  • Abnormal Altitudes
  • Roll
  • Aileron droop
  • Autopilot acquisition
  • Activates the protections
28
Q

SYSTEMS -

When High-speed protection is activated what happens?

A

BASN

  • Bank limited to 40 degrees
  • Autopilot disconnects
  • Seeks wings level
  • Nose up movement
29
Q

SYSTEMS -

When does TO INHIBIT appear on the EWD and how long does it stay displayed.

A

Appears at the application of takeoff power and stays until 1500ft or 2 minutes which ever occurs first.

30
Q

SYSTEMS -

When are WingTip brakes (WTB) activated?

A
  • ROAM
  • Runaway (symmetrical)
  • Overspeed - mechanism overspeed
  • Asymmetry
  • Movement (Uncommanded) of surfaces
31
Q

SYSTEMS -

When is the PTU inhibited?

A
  • During and 40 seconds after cargo door operation
  • Tow pin in with split engine masters
  • Parking brake set with split engine masters

Lights and Switches guide

32
Q

SYSTEMS -

If the ECAM control panel fails which buttons still work?

A
  • ALL
  • STS
  • RCL
  • CLR
  • EMER CANC

Frontier Airbus (6 decks)

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