Memory Items Flashcards

1
Q

What are the memory items associated with the TAWS warning ‘PULL UP’? ″PULL UP″
– ″TERRAIN AHEAD PULL UP″
– ″OBSTACLE AHEAD PULL UP″
(A380) What are the memory items
associated with any of the “PULL UP’ TAWS Warnings?

A

Announce: “PULL UP - TOGA” and simultaneously:
* AP OFF
* PITCH PULL UP (to full back stick)
* THRUST LEVERS TOGA
* SPEED BRAKE LEVER CHECK RETRACTED
* BANK WINGS LEVEL or ADJUST
* DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.

When flight path is safe and the warning stops: reduce pitch and accelerate. When speed is above VLS and V/S is positive: clean up aircraft as required.

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2
Q

What are the memory items associated with TAWS cautions ‘TERRAIN TERRAIN’, ‘TOO LOW TERRAIN’, ‘TERRAIN AHEAD’, and ‘OBSTACLE AHEAD’?

A

During night or IMC apply the EGPWS WARNINGS procedure. During daylight and VMC with terrain and obstacles clearly in sight: FLIGHT PATH – ADJUST.

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3
Q

What are the memory items
associated with TAWS
CAUTIONS?
– “SINK RATE”
– “GLIDE SLOPE”

A

Above 1000 ft AAL IMC or above 500 ft AAL VMC:
FLIGHT PATH – ADJUST.
- Below 1000 ft AAL IMC or below 500 ft AAL VMC:
Go around consider

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4
Q

Above 1000 ft AAL IMC or above 500 ft AAL VMC:
FLIGHT PATH – ADJUST.
- Below 1000 ft AAL IMC or below 500 ft AAL VMC:
TAWS caution

A

Flight path - adjust

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5
Q

What are the memory items
associated with “TOO LOW GEAR”
and “TOO LOW FLAPS” TAWS

A

Go around

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6
Q

What are the memory items
associated with a Reactive Wind
shear alert (WINDSHEAR
WINDSHEAR WINDSHEAR)
warning or a pilot detected windshear encountered

A
  1. TAKEOFF
    o Before V1 – RTO if significant sped variations occur
    below V1 and if sufficient runway remains
    o After V1 – Announce: “WINDSHEAR TOGA” and
    apply TOGA / ROTATE at VR / SRS follow
  2. AIRBORNE: Initial climb or landing
    - Announce: “WINDSHEAR TOGA” and:
    • TOGA / AP (keep if engaged) / SRS follow
    • DO NOT CHANGE CONFIG
    (FLAPS/SLATS/GEAR) UNTIL OUT OF
    WINDSHEAR
    If necessary crew may apply full back stick
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7
Q

What are the memory items
associated with an Unreliable
Airspeed Indication on A380?

A

Announce: “UNRELIABLE SPEED” and then if safe conduct of
flight is impacted:
AP, A/THR, F/Ds - OFF
PITCH/THRUST - BEFORE THR RED ALT
• Below 10000 ft – 12.5˚/TOGA
• Above 10000 ft – 10˚/TOGA
- AFTER THR RED ALT
IF derated climb engaged – Select all
THR Levers - MCT
• Below 10000 ft –12.5˚/CLB
• Between 100 and 250 – 10˚/CLB
• Above 250 – 5˚/CLB,
FLAPS - Maintain current config (below FL250)
- Flaps (if CONF FULL) – Select CONF 3
Speed brake - check retracted
Landing gear - maintain below FL250

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8
Q

TCAS traffic alerts

A

TCAS MODE check armed
• Announce: “TCAS BLUE”
For TA:
• IF A/THR is off – select ON (Recommended)
• Do not perform a maneuver based on TA only
• Note: ensure ATC instructions are followed, AFS
selections will not “disarm” TCAS Mode
For all RA, except CLIMB RA during approach in CONF 3 or
FULL:
• If AP engaged & when TCAS mode engages Monitor
the vertical speed and state “TCAS”
• If AP off
 FD orders follow (the AP can be engaged)
• Monitor vertical speed
Any CLIMB RA during approach in CONF 3 or FULL:
• Perform Go-around
• Monitor vertical speed
• Notify ATC
When “CLEAR OF CONFLICT”:
• Follow AP/FD
• Notify ATC
• Adjust Speed, Lateral and Vertical Guidance
If TCAS MODE not available:
• Announce: “TCAS, I HAVE CONTROL”
For all RA, except CLIMB RA during approach in CONF 3 or
FULL RA:
• AP (if engaged) OFF
• FDs OFF
• Adjust/Maintain Pitch to keep VSI in green
Any CLIMB RA during approach in CONF 3 or FULL:
• Perform Go-around
• Monitor Vertical Speed
When “CLEAR OF CONFLICT”:
• Notify ATC
• Adjust Lateral and Vertical Guidance
• Engage AP/FD as required

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9
Q

What are the company stabilisation approach criteria?

A

An approach is considered stabilized when the following
parameters are met:
1. All briefings are complete.
2. The aircraft is on the vertical and lateral flight path.
3. Only small changes in heading/pitch are necessary to
maintain the flight path, whilst remaining within OM-B
limitations.
4. The indicated airspeed shall be within a range from
Vref/VLS up to target speed +10 kt (deviation is
permitted below 1,000 ft AAL down to 500 ft AAL only
when specifically instructed by ATC to maintain a specific

  1. The thrust setting is appropriate for the aircraft
    configuration (deviation is permitted below 1,000 ft AAL
    down to 500 ft AAL only when specifically instructed by
    ATC to maintain a specific speed).
  2. The aircraft is in the briefed landing configuration.
  3. Rate of descend is no greater than:
    • 1,000 ft per minute for CAT C aircraft, or
    • 1,200 ft per minute for CAT D aircraft.
  4. All checklists have been completed.
  5. ILS approaches must be flown within 1 dot of glide slope
    and localizer.
  6. During non-precision approaches, the course deviation
    must stay within ½ dot or 2.5° for VOR approaches and
    5° for NDB approaches.
    Momentary exceedance of these parameters is allowed provided
    immediate corrective action is taken. A momentary excursion is
    defined as a deviation lasting only a few seconds and where every
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10
Q

What are the limitations regarding taxi with a deflated or damaged tires?

A

 No deflated nose
landing gear tire in the
case of towing with
tow barless towing.
 Max speed is 3 kt.
 Maxi NSW angle is 30
degrees.
 Up to 9 tires can be
deflated, with the
following max per
landing gear:
- One tire deflated on
the nose LDG GR.
- Two tires deflated
per body landing
gear, provided they
are not on the same
axle.
- Two tires deflated
per wing landing
gear provided they
are not on the same
axle.
For runway vacating only,
the 2 deflated tires on the
body or wing can be on the
same axle.
For taxi, the two deflated
tires can be located on the
center axle of the body

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11
Q

What are the engine starter limitations for the 380?

A

Three (3) attempts of 5 min continuous with a 2 min
cool down between attempts.
When the starter accumulates 15 min of use, a 30min
cool down is required.
Note: tailwind >25kts may have adverse effect on start.
It may be necessary to reposition the airplane into the wind.

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12
Q

What are the pre-requisites for using
NAV mode in the terminal area?

A

NAV mode may be used in terminal area provided that:
 NAV PRIMARY is
available, or (350)
 GPS PRIMARY is
available, or (380)
 HIGH accuracy is displayed and the appropriate
RNP is checked or entered on the MFD, or
 Aircraft navigation is crosschecked with navaid raw

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13
Q

Is it authorized to fly a RNP APCH
without GPS PRIMARY?

A

No. FCOM/PRO/SPO/PBN requires at least 1 GPS
to start a RNP APCH. (New PBN chart naming for
RNAV(GNSS) approaches)

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14
Q

What are the mandatory precautions that
must be taken if performing an automatic
landing in CAT 1 or better weather
conditions (Practice LVP
Approach/Autoland)?

A
  1. Practice low visibility approaches and/or Autoland
    are only permitted on runways certified for LVP,
    with prior ATC coordination and assurance of
    protection against signal disturbance. (OM-A
    8.4.12).
  2. The crew is aware that LOC or GS beam
    fluctuations, independent of aircraft systems, may
    occur and the PF is prepared to immediately
    disconnect the AP and take appropriate action,
    should unsatisfactory guidance occur.
  3. At least CAT 2 (LAND 2) capability is displayed on
    the FMA, and CAT 2/CAT 3 procedures are used.
  4. Visual references are obtained at an altitude
    appropriate to the performed CAT 1 approach
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15
Q

What is the max fuel temp

A

+53 degrees

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16
Q

What is the minimum fuel temperature?

A

Jet A -40 degrees

Jet A1 -47 degrees

17
Q

What is the minimum fuel quantity for take off?

A

Before pushback, if at
least one fuel transfer tank
is not empty, ensure that
the fuel quantity in each
feed tank is more than 4000kgs

18
Q

On ground, what is the approximate APU
fuel consumption, with BOTH PACK ON
and GEN ON?

19
Q

On ground, what is the approximate APU
fuel consumption, with BOTH PACK ON
and GEN ON?

20
Q

What are the memory items associated with Stall Recovery?

A

Announce – “STALL, I HAVE CONTROL”
• NOSE DOWN PITCH CONTROL – APPLY
• BANK – WINGS LEVEL
- When out of stall (no longer stall indications):
• THRUST – INCREASE SMOOTHLY AS NEEDED
• SPEEDBRAKES – CHECK RETRACTED
• FLIGHT PATH – RECOVER SMOOTHLY
- If in clean configuration and below 20,000 ft:
• Select Flap 1

21
Q

13.What are the memory items
associated with a STALL
WARNING AT LIFT-OFF?

A

Announce: “STALL, TOGA 12.5°”
• THRUST – TOGA
• PITCH – 12.5°
• BANK – WINGS LEVEL

22
Q

What are the maximum
allowable bank angles during
takeoff?

A

• Minor heading changes (up to 10 degrees bank) are not
considered to be a turn
• 15 degrees at/above 300 ft AGL
• 30 degrees at/above 500 ft AGL

23
Q
  1. What are the maximum
    permissible rates of
    climb/descent?
A

During climb or descent, the maximum vertical speed shall not
exceed:
• 2,000 ft/min when within 2,000ft of the cleared flight
level/altitude.
• 1,500 ft/min when within 1,000ft of the cleared flight
level/altitude.
Higher rates are permissible during climb, cruise, descent, and
approach only when:
• Both PF and PM confirm the absence of traffic in the vicinity
that may compromise separation or result in a TCAS
TA/RA; or
• When explicitly requested by ATC.
Flight crew shall be particularly vigilant concerning the flight
guidance modes and aircraft performance when approaching the
cleared altitude/flight level (i.e., high altitude level change,
turbulence, etc.).

24
Q
  1. Maximum vertical speeds
    approaching Terrain/Obstacles
A

Below 10,000 ft AGL, at no time must rates of descent exceed the
following values:
• 5,000 ft/min down to an altitude 5,000 ft AGL
• 4,000 ft/min down to an altitude 4,000 ft AGL
• 3,000 ft/min down to an altitude 3,000 ft AGL
• 2,000 ft/min down to an altitude 2,000 ft AGL
• 1,500 ft/min down to an altitude 1,000 ft AGL