SOP/Airline Policy Flashcards
When RWYCC is reported for different parts of the runway, which RWYCC shall be used?
Use the lowest value to determine maximum crosswind component and for performance calculation.
Who will announce the PRELIMINARY TAKEOFF PERF DATA crosscheck?
- PF will announce values and PM will cross check values independently by reviewing the values on his/her device.
Who will announce the FINAL TAKEOFF DATA performance crosscheck?
- CM2 will announce values (as described on PER chapter) and CM1 will crosscheck values independently.
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)
- 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.
For Factored Landing Distance Azores Airlines AIRBUS fleet uses ____ safety margin on top of Landing Distance (LD) calculation.
- 15%
What is the Factored Landing Distance Formula and Criteria?
- FLD = LD x Safety Margin x MEL/CDL penalty ≤ LDA
PERF GO AROUND page - THR RED ALT and ACC ALT:
- 1500ft AAL/1500FT AAL
PERF GO AROUND page - ENG OUT ACC ALT:
- MSA or published GA Altitude, whichever is lower.
What AUTOBRAKE mode should be used for CATII, CATIII approaches?
- MED mode
Stabilisation criteria: (14)
- 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.
Which aircraft has a tailwind limit of 15 kt? What approach technique shall be used if tailwind landing is greater than 10kt? (3)
- CS-TKP
- Decelerated approach is NOT permitted
- The aircraft speed should be stabilized at around VREF + 5 kt in final
Which approach types should be flown using the EARLY STABILISED TECHNIQUE? (5)
- 2D
- ABNORMAL CONFIGURATION
- LAND ASAP AMBER
- LAND ASAP RED
- MULTIPLE FAILURES
Which approach types should be flown using the DECELERATED TECHNIQUE? (4)
- 3D
- 3D RNP-AR
- SINGLE ENGINE 3D
- CATII/III
Consideration to call ATC ‘PAN PAN’ and ‘MAYDAY’
- MASTER CAUTION, ‘PAN PAN’ should be considered
- LAND ASAP AMBER, ‘PAN PAN’ is mandatory
- LAND ASAP RED and/or MASTER WARNING, ‘MAYDAY’ is mandatory
ALTERNATE FUEL calculation: for alternates within 200NM and for distances greater than 200NM
- FL220
- FL310