SOP/Airline Policy Flashcards

1
Q

When RWYCC is reported for different parts of the runway, which RWYCC shall be used?

A

Use the lowest value to determine maximum crosswind component and for performance calculation.

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2
Q

Who will announce the PRELIMINARY TAKEOFF PERF DATA crosscheck?

A
  • PF will announce values and PM will cross check values independently by reviewing the values on his/her device.
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3
Q

Who will announce the FINAL TAKEOFF DATA performance crosscheck?

A
  • CM2 will announce values (as described on PER chapter) and CM1 will crosscheck values independently.
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4
Q

USE OF AUTOBRAKE
To avoid landing with unduly high autobrake settings, the FLD with autobrake may exceed the LDA as long as all of the following conditions are satisfied: (3)

A
  • The RWYCC is 5 or 6
  • The LD with autobrake is less than the LDA
  • The FLD with maximum manual braking is less than the LDA.
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5
Q

For Factored Landing Distance Azores Airlines AIRBUS fleet uses ____ safety margin on top of Landing Distance (LD) calculation.

A
  • 15%
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6
Q

What is the Factored Landing Distance Formula and Criteria?

A
  • FLD = LD x Safety Margin x MEL/CDL penalty ≤ LDA
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7
Q

PERF GO AROUND page - THR RED ALT and ACC ALT:

A
  • 1500ft AAL/1500FT AAL
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8
Q

PERF GO AROUND page - ENG OUT ACC ALT:

A
  • MSA or published GA Altitude, whichever is lower.
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9
Q

What AUTOBRAKE mode should be used for CATII, CATIII approaches?

A
  • MED mode
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10
Q

Stabilisation criteria: (14)

A
  • Acceptable lateral deviation, if below:
    • ILS/VOR/RNP AR – 1 dot
    • RNP – 0.3 NM deviation
    • NDB – 5º
    • Visual approach – within a lateral position such that the required bank angle to resume the correct track does not imply a bank angle greater that 30º
  • Acceptable Vertical deviation, if below;
    • ILS -1 Dot
    • RNP AR /RNP – 75 feet deviation
    • 2D approach 100 feet deviation from profile
    • Visual – 4 white lights if PAPI available
  • The aircraft is in the desired landing configuration
  • The thrust is stabilized, usually above idle, in order to maintain the target approach speed along the desired final approach path
  • Speed not greater than VAPP+10kts or less than VAPP-5kt
  • The V/S is within -1000 FPM and 300 FPM
  • The flight crew does not detect any excessive flight parameter deviation
  • All briefings and checklists have been completed.
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11
Q

Which aircraft has a tailwind limit of 15 kt? What approach technique shall be used if tailwind landing is greater than 10kt? (3)

A
  • CS-TKP
  • Decelerated approach is NOT permitted
  • The aircraft speed should be stabilized at around VREF + 5 kt in final
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12
Q

Which approach types should be flown using the EARLY STABILISED TECHNIQUE? (5)

A
  • 2D
  • ABNORMAL CONFIGURATION
  • LAND ASAP AMBER
  • LAND ASAP RED
  • MULTIPLE FAILURES
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13
Q

Which approach types should be flown using the DECELERATED TECHNIQUE? (4)

A
  • 3D
  • 3D RNP-AR
  • SINGLE ENGINE 3D
  • CATII/III
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14
Q

Consideration to call ATC ‘PAN PAN’ and ‘MAYDAY’

A
  • MASTER CAUTION, ‘PAN PAN’ should be considered
  • LAND ASAP AMBER, ‘PAN PAN’ is mandatory
  • LAND ASAP RED and/or MASTER WARNING, ‘MAYDAY’ is mandatory
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15
Q

ALTERNATE FUEL calculation: for alternates within 200NM and for distances greater than 200NM

A
  • FL220
  • FL310
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16
Q

An aerodrome is considered to be ADEQUATE if: (8)

A
  • The aerodrome is scheduled to be open at the expected time of use;
  • The length of at least one runway is sufficient to allow operation within the performance requirements of the aircraft used;
  • The runway expected to be used is at least 45m wide;
  • Navaids and runway lighting needed for the approved approaches, ATC facilities, meteorological information, communications and at least one approach procedure are available at the expected time of use;
  • The aerodrome pavement strength is compatible with the aircraft weight or a derogation is obtained from the aerodrome authority;
  • For International flights, Police, Customs and Immigration authority services are available;
  • Ground service facilities for fueling, de-/anti-icing, catering and general handling using normal operating procedures;
  • Rescue and Fire Fighting Services are available.
17
Q

USE OF SUMMARIES (8 steps)

A

1 - ECAM ACTION
2 - STATUS
3 - CRUISE SUMMARY
4 - FUEL
5 - LANDING PERFORMANCE
6 - STATUS
7 - APPROACH, LANDING, GO-AROUND
8 - FMGS PREPARATION

18
Q

SATA SBTY CHECKS: (5)

A

SELFO
- Summary
- Engine Failure
- Landing Gear
- Flaps/Slats
- Overweight

19
Q

CALLOUTS - FLIGHT PARAMETERS - GO AROUND

A
  • “BANK”, if the bank angle becomes greater than 7 °
  • “PITCH”, if the pitch attitude becomes greater than 20 ° up or less than 10 ° up
  • “SINK RATE”, if there is no climb rate.
20
Q

PERFORMANCE - IN FLIGHT FAILURE
Which flap setting should the flight crew select for landing?

A
  • The one requested by the ECAM
21
Q

BRAKING - What is the maximum pressure when braking using alternate braking?

A
  • 1000PSI
22
Q

Crosswind/Tailwind takeoff - PROCEDURE

A
  1. ‘TAKEOFF’ - ANNOUNCE
  2. THRUST - 50 % N1
  3. SIDESTICK - FULL FORWARD
  4. BRAKES - RELEASE
  5. Increase thrust rapidly to about 70 % N1
  6. Progressively to reach takeoff thrust by 40 kt ground speed
  7. THRUST LEVERS - FLX or TOGA
23
Q

Crosswind/Tailwind takeoff
In which condition do you apply this technique?

A
  • Tailwind
  • Crosswind above 20kt