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A220-300 Checklist Light

Airbus A220‑300

Comprehensive Normal & Abnormal Checklist ASOP
For flight‑simulation training only – NOT for real‑world aviation use.
Version 1.0 – 28 Mar 2026

How to Use

  1. Flows first – complete the panel flow silently.
  2. Challenge/Response checklist – verify critical items.
  3. Read‑and‑do checklist – any blue‑striped (memory) item.
  4. Keep PF heads‑up whenever aircraft is moving.

Legend

  • PF – Pilot Flying PM – Pilot Monitoring
  • Italic – Call‑outs Bold – Memory item/trigger
  • (A) – Automatic call/alert (M) – Manoeuvre

Normal Operations Checklists

1 Power‑Up / Acceptance

ItemAction
Parking BrakeSET
Battery 1 & 2ON (verify ≥24 V)
External PowerON (if AVAIL)
APU MasterON → START
APU GeneratorON BUS (when avail)
IRS (2)NAV
OxygenTESTED, 100 %
Gear Pins / CoversREMOVED & STOWED

2 Preliminary Cockpit Preparation

ItemAction
CVRTest
Emergency Exit LightsARMED
EICASCHECKED (CAS clear)
ELTARMED

3 Cockpit Preparation (Flows)

Panel FlowAction
Overhead → Glareshield → PedestalComplete flow pattern
Fuel PumpsON (verify qty)
Hydraulic Pumps (Green & Yellow)ON
Window HeatON
Pressurization (IASC)AUTO
Probe HeatOFF (until engine start)
Displays / Pro Line FusionNORMAL, AUTO BRT
Checklist ItemResponse
”Cockpit preparation checklist.”PM initiates
Gear pins & coversRemoved
IRSAligned
Fuel qty_____ kg, balanced
Take‑off briefingCompleted
ChecklistComplete

4 Before Start

PF TriggersPM Response
Flight Deck DoorCLOSED & LOCKED
ACARSINITIALIZED
Fuel___ KGS, Pumps ON
Passenger SignsON & AUTO
WindowsLOCKED
FCPV2 ___, HDG ___, ALT ___
Take‑off SpeedsV1 ___, VR ___, V2 ___
FMS PreflightCOMPLETED
Trims (Rudder & Aileron)FREE & ZERO
BeaconON
TransponderAUTO / XPDR
Parking BrakeSET
EICAS StatusCHECKED

5 Engine Start (Normal – FADEC Auto Start)

StepAction
APU BleedON
Engine Start Selector (Eng 1)START
FADECManages start automatically
MonitorN2 rotation, EGT rise (limit 1 054 °C)
At idle stabilisationOil pressure & parameters GREEN
Engine 2Repeat procedure
Both stableAPU Bleed OFF, Start Selectors OFF
Aborted Start – Engine Start Selector OFF immediately. FADEC initiates automatic dry crank (~60 s at ~30 % N2) if engine is hot. EGT start limit 1 054 °C.

6 After Start

ItemAction
APUOFF (if not required)
Generators 1 & 2ON
Probe HeatON
Anti‑IceAS REQD
Flight ControlsCHECKED (full travel, FBW)
FlapsT/O CONFIG (2 or 3)
Stabilizer Trim___ UNITS
Checklist ItemResponse
”After‑start checklist.”PM initiates
Anti‑ice____
Trims (rudder & aileron)Zero
Flaps__/____
Stabilizer trim__ units
EICASChecked
AutobrakeRTO

7 Taxi

ItemLimit
Taxi Speed straight≤ 30 kt
Turns≤ 10 kt
Nosewheel SteeringTILLER (±70°) / RUDDER PEDALS (±7°)
Brake check at first movement “Brakes checked” - electric brakes, verify normal operation on EICAS.

8 Before Take‑Off – Up to the Line

ItemAction
Flight ControlsCHECKED
FCPVERIFY (V2, HDG, ALT)
FlapsCONFIRM setting (2 or 3), GREEN
V‑SpeedsANNOUNCED
Stabilizer Trim___ UNITS
CabinSECURE

9 Before Take‑Off – Below the Line (entering runway)

ItemAction
TCASTA/RA
Engine Start SelectorsCONT
StrobesON
TransponderTA/RA
Completion Call”Cabin ready, below‑the‑line complete.”

10 Take‑Off Roll & Initial Climb (Call‑Out Memory)

PMPF
”80 knots""Checked"
"V 1"
"Rotate”Rotate to ≈ 15° pitch
”Positive climb""Gear up”

11 After Take‑Off / Climb

TriggerAction
Acc Alt reachedClimb Thrust (CLB)
Flap retractionOn schedule (speed bugs)
Engine BleedsON
10 000 ft”10 000 – Lights off.”
STD QNHSET both (above trans alt)

12 Cruise (Hourly)

ItemAction
Fuel checkFOB vs Plan (±300 kg)
SystemsEICAS CAS clear
Waypoint sequenceNEXT & ETA compare
Cruise speedM 0.76 – M 0.80

13 Descent Preparation

ItemAction
ATIS / STARRECEIVED & INSERTED
Approach BriefingCOMPLETED
Landing DataVREF ___, Minimums ___
Pressurization (IASC)LAND ALT ___
Autobrake___ (LO, MED, or MAX)
EICASCHECKED

14 Approach Checklist

ItemResponse
AltimetersSet (QNH)
Minimums__ ft
Approach briefingConfirmed
Seat beltsON

15 Landing

Height AGLCall‑outConfiguration
1 000 ft”Stable/Unstable”Gear DOWN, Flaps 4 or 5
500 ft”Landing”Final scan
50/40/30/20/10 ft(A)Flare
Ground spoilers auto‑deploy on touchdown. Reverse thrust at touchdown, reverse idle at 60 kt. Electric brakes – verify deceleration on EICAS.

16 After Landing

ItemAction
Speed BrakeDOWN
FlapsUP (0)
Probe HeatAS REQD
APUSTART (if req)
Engine Start SelectorsOFF
StrobesOFF
TransponderSTBY
Weather RadarOFF
Completion Call”After‑landing checklist complete.”

17 Shutdown

ItemAction
Parking BrakeSET
Engine Start Selectors (1 & 2)OFF
Seat BeltsOFF
BeaconOFF
Fuel PumpsOFF
Hydraulic PanelSET

18 Secure Aircraft

ItemAction
IRS (both)OFF
Emergency Exit LightsOFF
Window HeatOFF
Batteries 1 & 2OFF
Post‑flight reportSent

Abnormal / Memory Items (Extract)

ENGINE FIRE or SEVERE DAMAGE (In‑Flight)

StepAction
1Autothrust (if engaged) → DISENGAGE
2Thrust Lever (affected) → CONFIRM → IDLE
3Engine Start Selector (affected) → CONFIRM → OFF
4Fire Push Button → CONFIRM → PUSH
5If CAS fire persists → AGENT 1 discharge, hold 1 s
6After 30 s if still lit → AGENT 2 discharge, hold 1 s

EMERGENCY DESCENT

ItemAction
Announce”EMERGENCY DESCENT” (×3)
SIGNSON
Passenger OxygenON
Engine Start Selectors (both)CONT
Thrust LeversREDUCE (minimum)
Speed BrakeFLIGHT DETENT
Target SpeedVMO 330 kt / MMO M 0.82
DescendLowest safe alt or 10 000 ft
(See QRH for full procedure.)

Quick‑Reference Flap Schedule (A220‑300)

ConfigPlacard Limit (VFE)Typical Use
Flaps 0 (UP)330 kt / M 0.82Cruise / clean
Flaps 1220 ktInitial deceleration
Flaps 2200 ktTake‑off (light weight)
Flaps 3200 ktTake‑off (heavy weight)
Flaps 4180 ktLanding (normal)
Flaps 5160 ktLanding (heavy / short / contaminated)
Gear Limits: VLO extend 250 kt · VLO retract 220 kt · VLE 250 kt

Revision History

RevDateNoteAuthor
1.028 Mar 2026Initial checklist issueACVA Team

Disclaimer

These checklists are abridged adaptations of Airbus / Bombardier public‑domain procedures for simulation. They do not replicate proprietary FCOM text and must not be used for commercial operations.