Flows & Procedures Flashcards

1
Q

Electric Power Up Procedure - Arriving to cold aircraft

A
  1. Mx Status - Check
  2. Ldg Gear Control Handle - Down
  3. ENG MASTER 1 and 2 - OFF
  4. ENG MODE - NORM
  5. RADAR - OFF
  6. Batteries - > 25.5V, AUTO
  7. Elec Power/Air Cond - Establish
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2
Q

IRS INIT

A

ADIRS - NAV
MCDU — FMGC — Check Data Base
INIT —— Enter From/To
IRS INIT —— Verify

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3
Q

Preflight - Prior to every Flight

A

CA FLOW:

➤ Flight Forms - Onboard
➤ ADIRS - NAV
➤ RCDR GND CTL - ON
➤ EFIS Control Panel - Set 
➤ FCU - Check
➤ TERR ON ND - As required 
➤ Standby Altimeter/ISIS - Set QNH
➤ Park BRK - ON
➤ ACP- Set
➤ RMP - Set
➤ MCDU - Set
➤ ND - Check
➤ PFD - Check
➤ Oxygen - Check
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4
Q

Before Start Flow

*Trigger: After Fueling is done, 10 minutes prior to Departure

A
CA FLOW:
➤ AML - Onboard, Reviewed
➤ FUEL Panel - Set
➤ ELEC Panel - Check
➤ Air Cond Panel - Set
➤ Seat Belts Sign - ON
➤ ECAM - Check
➤ Window - Closed and Locked
➤ EFB, PED - Set, Off
— Accomplish Before Start Checklist
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5
Q

Before Pushback

*Trigger: Cabin Ready Report/Door Closed

A

CA FLOW:

➤ Flightdeck Door - Closed and Locked
➤ Slides - Armed
-A319/320: 6 Slides armed
- A321: 8 Slides armed
➤ N/W STRG DISC Memo - Check
➤ Beacon - On

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6
Q

Close out verification and brief Captain

A

Flight number/ aircraft number
Fuel Pred page - ZFW and ZFCG
Perf TO - DATA change:
V1,Vr,V2
Flaps/THS(trim seting) FLEX TO TEMP (if Applies)
Brief: OM1 2C.3.10 Weight: (TPS vs current)
Flex TOW ≤ ATOW or TOGA TOW≤PTOW
Winds: (TPS VS current)
Temperature: (TPS VS current)
FLEX: Current temp < TPS assumed temp (AT)
TOGA: Current temp < TPS TEMP
Configuration changes: spds, flex, flaps, bleeds
Discrepances: W/B, SECOK
Example: “We’re under the assumed takeoff weight by about 1000 lbs. We’re under
the assumed temp of 40, there is no tailwind.”

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7
Q

After Start
Trigger: After ground equipment is clear,
Engine(S) Stable (no gray box N2)

Captain - “I have Salute”
Flaps_____

A

CA FLOW:
~~~
➤ Spoilers - ARM
➤ ACP - Set
➤ ENG ANTI ICE - ON or Off
~~~

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8
Q

Before Takeoff

*Trigger: After Closeout reviewed, both engines running and flaps set for takeoff

A

CA FLOW:

➤ Flight Controls - Check
➤ Thrust Bump (If Required) - Engaged
➤ Takeoff Data/Flex - Check

Accomplish Before Takeoff Check (Down to the line)

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9
Q

Before Taking the Runway
*Trigger: When approaching #1 for takeoff

A

FO FLOW:

➤ FMA - Check
➤ Runway and FMS - Check

— Accomplish Before Takeoff Check (Below the line)

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10
Q

Pilot Monitoring

*Trigger: After Flap and Slat retraction

A
➤ Air Cond - Check
➤ Landing Gear - Check
➤ Flaps - Check
➤ Spoilers - Disarmed
➤ Cabin Vertical Speed - Check
— Accomplish After Takeoff Checklist Silently
“After Takeoff Checklist complete”

*Climbing through 10,000 ft

FO FLOW:
➤ ECAM - Check

*Climbing through Transition Altitude
➤ BARO SET - PULL STD
➤PFDs - Crosscheck
“Transition, Standard”

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11
Q

Pilot Monitoring - Descent Flow

*Trigger: Descending through 18,000ft

A
➤ Seat Belts - ON
➤ ECAM - Check
➤ TERR on ND - As required
➤ MCDU - Set
➤ Changeover Report - Sent

—Accomplish Descent Checklist

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12
Q

After Landing

  • Trigger: After Aircraft has cleared the runway
A

CA FLOW

➤ Exterior Lights - As Required
➤ Flaps Up
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13
Q

SHUTDOWN

*Trigger: After Aircraft is parked with parking brake set

A

CA FLOW:

➤ Seat Belts Signs - OFF
➤ Anti Ice - OFF
➤ Engine 2 Master - OFF

After ground/APU Power is established

➤ Engine 1 Master - OFF
➤ Flaps - Check
➤ Y ELEC PUMP - OFF
➤ Fuel Pumps - OFF
➤ APU Bleed - As Required
➤ GPWS LDG FLAP 3 - OFF
➤ Beacon - OFF
➤ ECAM - Check (Oil, Hyd, O2, STS)
➤ AML - Completed, if Required
➤ APU - OFF

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14
Q

CAMI Procedure

A
  • Confirm FMS inputs with the other pilot when airborne
  • Activate the input
  • Monitor mode annunciations to ensure autoflight systems perform as desired, and
  • Intervene if necessary
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15
Q

Origination Flow

  • Forms and Manuals - Check
A
  • AML
  • Two QRCs
  • Flight Deck Forms (Yellow Book)
  • Jumpseat Briefing Card
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16
Q

Origination Flow

ECAM CHECK

A
  1. Oil Quantity: 13 quarts
  2. Hydraulic Quantity — Within Normal Fill Range
  3. Oxygen Quantity — Check
    * If less than 1000psi see Limitations
  4. STS — Check
    - Class II messages do not affect dispatch
    * Except
    - Air Bleed
    - DMC 1/3 and DMC 2/3 (both together)
17
Q

Origination Flow

ELEC Panel - Check

A
  1. ECAM ELEC PAGE —— Select
  2. BAT 1 and BAT 2 — OFF and then ON
    * 10 seconds after selecting ON check on ECAM ELEC page that both battery charge currents are below 60 amps and decreasing
  3. ECAM ELEC page —— Deselect
  4. GEN 1 and GEN 2 FAULT Lights — Illuminated
  5. Remaining Pushbutton Lights — Extinguished
  6. EXT PWR AVAIL/ON Lights — AVAIL/ON as appropriate
18
Q

FMGS Preflight Sequence

SET UP THE BOX - DDIIFIPPS

A
DATA - BIAS
DATA - NAVAIDS DESELECT
INIT A
INIT B
F-PLAN
INIT - WINDS
PERF - CRUISE
PERF  DESCENT
SEC F-PLN (Eng-Out or Copy Active)
19
Q

Flight Control Check

A

Sidestick

“Full Up”
“Full Down”
“Neutral”
“Full Left”
“Full Right”
“Neutral”

Rudder

“Full Left”
“Full Right”
“Neutral”

20
Q

MCDU Descent Preparation

Backward Z
*F-PLN - RAD NAV - PROG - PERF

A

1) F-PLN
2) RAD NAV
3) PROG
4) PERF
5) FUEL PRED
6) SEC F-PLAN

21
Q

Origination Equipment Check

FO Side - PEGACROC

A
PBE - Humidifier-Blue / Seal - Intact
Extinguisher - Pressure Green / Pin Secured.
Gear Pins
Axe (Crash Axe)
Circuit Breakers (Back Wall)
Rain Repellent
Observer’s Life Vests
Compartmentalized Areas
22
Q

RCDR Panel - Check

A
  • PARK BRK —— ON
  • LOUD SPEAKER VOLUMES —— OFF
  • INT/RAD Switches —— SET TO INT
  • Interphone Volume Reception —— OUT
  • RCDR GND CTL —— ON
  • CVR TEST ——— Press and Hold
  • Check Low frequency signal/tone through loud speakers. If none,
  • Apply brakes with Brake Pedals and hold
  • SET PARK BRK to OFF
  • Perform CVR TEST using a headset plugged into the overhead CVR Panel
  • Set PARK BRK to ON
  • INT/RAD Switch ——— Neutral
  • Interphone Volume Reception —— As Required
23
Q

Arrival Set-Up

ABBBCA

A
  • ATIS
  • Blue Pages
  • Build It - Backward Z
  • Brief It
  • Checklist
  • Activate Approach (10,000ft)
24
Q

Periodic System Checks

AHEFOE

A
Altimeters - Crosscheck
HYD - Quantity and Pressure
ELEC - Parameters, GEN loads
FUEL - Quantity, Temp, Distribution
DOORS - Oxygen Pressure
ENG - Oil Pressure and Temp
25
Q

Undue Activation of Alpha Protection
At any time, with a speed above VLS, the aircraft goes to a continuous nose down pitch rate that cannot be stopped with backward sidestick inputs, immediately

A

A. One ADR pb ——— KEEP ON
B. Two ADR pbs ——— OFF

Note: In case of dispatch with one ADR inoperative, select only one ADR to OFF

26
Q

“FIX” Strategy

A

Identify - Problem and Procedure
eXecute - The Procedure
Manage - Evaluate and Plan

  • PF: FLY - Maintain Aircraft Control
    “My Aircraft”