1. A320/321 minimum on max turbulence?
 Below FL 200: 250kts; At or Above FL 200: 275kts or M 0.76
2. How long to avoid the wake turbulence on RW?
    From Heavy to medium 3min; Same type of A/C 2min
3. Minimum oil quantity
    9.5qts + 0.5 qts per hour of flight
4. Battery uses which source to charge
    External power on ground for 20min.
5. Cycling to start the engine? How long?
    4 cycles per 2min
6. Brake modes?
    Normal braking, Alternate Braking w/ Anti-skid ON, Alternate Braking w/ Anti-skid OFF,
      Parking Breaks
7. Max cabin pressure altitude?
    14,000ft
8. EGT Lim; APU EGT limit?
    EGT Limits: Starting 725, Max Cont. 915, T/O or G/A Normal: 950, T/O or G/A OEO:950
    APU EGT:742
9. Brake fan (Before taking – off, after landing)
    Before t/o: 300 w/o break fans, 150 with break fans
    After landing: if temp exceeds 500 turn on break fans, delay brake fans 5min after
      landing
10. Noise abatement
11. One engine inoperative
12. Take off briefing (abnormal)
     For any failure before V1, Capt will call “stop or go” and I will revert to PM duties
       In case of failure after V1, continue t/o. no action shall be done before 400ft.
       Reaching 400ft AGL, ECAM actions
       Reaching EO acceleration altitude: If the engine is secured, level off, accelerate and
       clean-up. Otherwise, continue climb until the engine is secured but not above
       maximum EO acceleration altitude
       At green dot, open climb, MCT, resume ECAM, after t/o climb checklist
       Engine out routing: EO SID, SID, radar vector, immediate return.
       Monitor my flying, advise me if there are any deviations from the standard
       Unless you have anything to add…
13. Icing condition
    - OAT and TAT is less than 10C with visible moisture.
14. MEL, CDL
    - MEL (Minimum Equipment List) – Prepared by the Operator / Company. Limitations of
      the a/c operation in case the system is inoperative or malfunctioned.
    - CDL (Configuration Deviation List) – Deals with structural parts on an a/c whether it has
      been missing or fallen off.
15. NOTAM (decode)
16. Weather (avoid thunderstorm, Decode, metar, taf)
17. Performance (V1/VR/V2. VMU, VMCG, VMCA)
     VMCG (Velocity of Minimum Control on Ground) – minimum speed at which the a/c
       remain controllable on ground in an event of an engine failure. (lateral excursion of
       30ft)
     V1 (Decision Speed) – Commit to fly, Go or no- go decision. Minimum speed at which
       the pilot can continue t/o after an engine failure.
     VMU (Velocity of Minimum Unstick) – minimum speed at which you can lift the
       nosewheel off the ground but still unable to t/o.
     VR (Rotation Speed) – speed which makes lift-off possible
     VMCA (Velocity of Minimum Control in the Air) – Minimum speed in the air that
       directional control can be maintained with one engine inoperative.
     V2 (T/O safety Speed) – Speed at which the a/c may safely climb with one engine
       inoperative.
18. RVSM
    - Reduce Vertical Separation Minima.
       FL 290 to FL 410
       Required Equipments: 2PFDs (alt function) , 2ADRs, 1XPDR, 1AP, 1FCU, 1FWC (Alert
       function)
19. APU EGT limit, start limit (Eng, battery)
    - APU ECG – 742
    - APU Start below 25,000 – 900
    - APU Start at or above 25,000 – 982
20. Engine EGT limit, MCT time limit
    - Start - 725
       Cont- 915
       TOGA/GA (Norm) – 950 for 5min
       TOGA/GA (OEI) – 950 for 10min
21. Hydraulic: how many systems, yellow electric pump
    - 3 Main Independent Fully Automatic HYD systems.
    - Yellow Electric pump is pressurized by ENG2 w/ a normal pressure of 3000PSI.
22. How many electric source?
     4 in flight, 5 on ground:
          1. Engines 1 & 2
          2. External Power
          3. APU
          4. RAT
          5. Battery (On ground)
23. Memory item
     10:
          1. Emer Descent
          2. Unreliable a/s
          3. Stall Recovery
          4. Stall at lift-off
          5. EGPWS Warning
          6. EGPWS Cautions
          7. TCAS
          8. Loss of Breaking
          9. Windshear
          10. Windshear Ahead
24. ETOPS
    - Extended Operations
       Extended-range Twin-engine Operational Performance Standard
       Enhanced Twin Engine Operational Procedure
25. Different between wind shear and wind shear ahead (Action)?
     Windshear: Actual windshear condition
        Windshear Ahead: Predictive windsear. A situation that can be avoided.
26. Which Hydraulic system use electric to operate
     Blue and Yellow HYD
27. Which Hydraulic system use electric pump
     Blue and Yellow HYD
28. Limitations of flaps/slats
    - F1: Slats 18, Flaps 0, VFE 230
       1+F: Slats 18, Flaps 10, VFE 215
       F2: Slats 22, Flaps 15, VFE 200
       F3: Slats 22, Flaps 20, VFE 185
       FFULL: Slats 27, Flaps 35, VFE 177
29. Limitation of landing gear
    - Max Tire Speed: 195
       1 Tire: 7
       2 Tires: 3
30. RAT (What is RAT and purpose of it and limitation)
    - Deploys automatically if AC bus 1 & 2 is inoperative. It can be deployed manually at
       the overhead panel and stowed manually on ground. Normal pressure: 2,500PSI
    - Minimum RAT speed: 140kts
31. Maximum altitude for using flap
     20,000
32. Difference between green and yellow system
    - Green HYD is pressurized by ENG1 while Yellow is pressurized by ENG2
33. Golden rules
    - Fly, navigate, communicate in this order and with appropriate task sharing
    - Use proper automation at all times
    - Understand FMA at all times
    - Take over when anything goes unexpected.
34. Service Ceiling? Can we go higher?
    - 39,800ft, Yes. Service ceiling is to prevent structural damage and safety limit.
35. Weight limitation
    - Max Taxi: 77 400
    - MTOW: 77 000
    - MLW: 66 000
    - MZFW: 62 500
    - Min Wt: 37 230
36. Normal hydraulic operating pressure
    -  3 000PSI +/- 200PSIs
37. Approach Procedure
    - PABBA
38. T/O Briefing
39. Control Change with Airbus (FMA, FCU, ND, EFIS)
40. Standard Call-outs
     1. Emer Descent – “Emergency Descent”
     2. Unreliable a/s – “Unreliable Speed”
     3. Stall Recovery – “ Stall, I have controls”
     4. Stall at lift-off- “Stall, TOGA 15”
     5. EGPWS Warning – “Pull up, TOGA”
     6. EGPWS Cautions
     7. TCAS – “TCAS, I have controls”
     8. Loss of Braking – “Loss of Braking”
     9. Windshear – “Windshear, TOGA”
     10. Windshear Ahead – Windshear, TOGA”
41. Mayday vs PanPan
     Emergency calls: Mayday needs immediate assistance while PanPan does not require
      immediate assistance.
42. Windshear MI All Situation (Ex. On the RWY, after TO)
    - Windshear and Windshear Ahead procedures
43. After Eng strt flow
    - Small J (PM), 4 (PF)
44. Alt Cruise Sequence
    -
45. Above g/s how can you capture
    - Cleared for APP, Arm APP, Command Flaps (F2,3,FULL)
           *At least Config 2. LDG down
    - Crank ALT knob to the right (select higher ALT)
    - Intercept LOC
    - V/S 1,500 to 2,000
    - Intercept G/S
46. Given speed – Follow chart CAT for DA
47. FLOWs
48. App briefing
49. After call sign for wake turbulence
     Light, Medium, Heavy, Super
50. Pilot Incapacitation
    - Take Over, Side-stick priority (40s)
    - Fly, Navigate, Communicate
    - Emergency Call ATC: “Mayday3x, Single pilot operation, pilot incapacitation.”
    - Request: “Req to hold over….”
    - Once established: “Attention, Purser to cockpit please”
    - Tighten shoulder harness and secure, recline the seat upright, push the seat back.
    - Ask for doctor or company rated qualified pilot/s
    - Prepare for the approach
    - Teach or ask the purser to guide you with the checklist
    - Land ASAP
    - Request for medical assistance
51. Land ASAP Amber or Red?
   -   Amber: Assess the situation then land to the nearest suitable aerodrome
   -   Red: Land to the nearest suitable aerodrome.
52. Why do we switch off FD during TCAS?
    - To avoid possible confusion between FD bar orders and TCAS aural and VSI orders.
    - To ensure A/THR speed mode.