Flows & Procedures Flashcards
Electric Power Up Procedure - Arriving to cold aircraft
- Mx Status - Check
- Ldg Gear Control Handle - Down
- ENG MASTER 1 and 2 - OFF
- ENG MODE - NORM
- RADAR - OFF
- Batteries - > 25.5V, AUTO
- Elec Power/Air Cond - Establish
IRS INIT
ADIRS - NAV
MCDU — FMGC — Check Data Base
INIT —— Enter From/To
IRS INIT —— Verify
Preflight - Prior to every Flight
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
Before Start Flow
*Trigger: After Fueling is done, 10 minutes prior to Departure
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
Before Pushback
*Trigger: Cabin Ready Report/Door Closed
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
Close out verification and brief Captain
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.”
After Start
Trigger: After ground equipment is clear,
Engine(S) Stable (no gray box N2)
Captain - “I have Salute”
Flaps_____
CA FLOW:
~~~
➤ Spoilers - ARM
➤ ACP - Set
➤ ENG ANTI ICE - ON or Off
~~~
Before Takeoff
*Trigger: After Closeout reviewed, both engines running and flaps set for takeoff
CA FLOW:
➤ Flight Controls - Check ➤ Thrust Bump (If Required) - Engaged ➤ Takeoff Data/Flex - Check
Accomplish Before Takeoff Check (Down to the line)
Before Taking the Runway
*Trigger: When approaching #1 for takeoff
FO FLOW:
➤ FMA - Check ➤ Runway and FMS - Check
— Accomplish Before Takeoff Check (Below the line)
Pilot Monitoring
*Trigger: After Flap and Slat retraction
➤ 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”
Pilot Monitoring - Descent Flow
*Trigger: Descending through 18,000ft
➤ Seat Belts - ON ➤ ECAM - Check ➤ TERR on ND - As required ➤ MCDU - Set ➤ Changeover Report - Sent
—Accomplish Descent Checklist
After Landing
- Trigger: After Aircraft has cleared the runway
CA FLOW
➤ Exterior Lights - As Required ➤ Flaps Up
SHUTDOWN
*Trigger: After Aircraft is parked with parking brake set
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
CAMI Procedure
- 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
Origination Flow
- Forms and Manuals - Check
- AML
- Two QRCs
- Flight Deck Forms (Yellow Book)
- Jumpseat Briefing Card
Origination Flow
ECAM CHECK
- Oil Quantity: 13 quarts
- Hydraulic Quantity — Within Normal Fill Range
- Oxygen Quantity — Check
* If less than 1000psi see Limitations - STS — Check
- Class II messages do not affect dispatch
* Except
- Air Bleed
- DMC 1/3 and DMC 2/3 (both together)
Origination Flow
ELEC Panel - Check
- ECAM ELEC PAGE —— Select
- 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 - ECAM ELEC page —— Deselect
- GEN 1 and GEN 2 FAULT Lights — Illuminated
- Remaining Pushbutton Lights — Extinguished
- EXT PWR AVAIL/ON Lights — AVAIL/ON as appropriate
FMGS Preflight Sequence
SET UP THE BOX - DDIIFIPPS
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)
Flight Control Check
Sidestick
“Full Up” “Full Down” “Neutral” “Full Left” “Full Right” “Neutral”
Rudder
“Full Left”
“Full Right”
“Neutral”
MCDU Descent Preparation
Backward Z
*F-PLN - RAD NAV - PROG - PERF
1) F-PLN
2) RAD NAV
3) PROG
4) PERF
5) FUEL PRED
6) SEC F-PLAN
Origination Equipment Check
FO Side - PEGACROC
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
RCDR Panel - Check
- 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
Arrival Set-Up
ABBBCA
- ATIS
- Blue Pages
- Build It - Backward Z
- Brief It
- Checklist
- Activate Approach (10,000ft)
Periodic System Checks
AHEFOE
Altimeters - Crosscheck HYD - Quantity and Pressure ELEC - Parameters, GEN loads FUEL - Quantity, Temp, Distribution DOORS - Oxygen Pressure ENG - Oil Pressure and Temp
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. 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
“FIX” Strategy
Identify - Problem and Procedure
eXecute - The Procedure
Manage - Evaluate and Plan
- PF: FLY - Maintain Aircraft Control
“My Aircraft”