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Synaptic A220-300 Emergency Procedures
Immediate Action Procedures
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6 procedures
- 1Master warningCANCEL, aural LEFT (RIGHT) ENGINE FIRE
- 2ECL - L(R) ENG FIRE non-normal checklist, follow the displayed steps
- 3Affected ENG RUN switchCONFIRM and OFF
- 4L(R) ENG FIRE switch - PUSH (closes fuel, bleed and hydraulic SOVs, arms bottles)
- 5BTL 1DISCHARGE, wait 30 seconds
- 6If fire persists: BTL 2DISCHARGE (either bottle feeds either engine)
- 7Above MSA: SHUTDOWN L(R) ENG procedure, no relight after a fire
- 8Land at nearest suitable airport
- 1MAYDAYDECLARE on guard frequency
- 2ECLfollow the displayed non-normal checklist
- 3APUSTART (APU bleed assisted start up to 23,000 ft)
- 4Windmill relight: speed above 250 kts, maximum altitude 27,000 ft
- 5Air starter assisted relight: speed below 250 kts
- 6ENG RUN switchOFF then ON for the relight attempt
- 7Emergency descentINITIATE if cabin altitude is rising
- 8Nearest runwayPLAN direct approach
- 1Abort decisionMAKE before V1
- 2Thrust leversIDLE (both)
- 3Autobrake RTOVERIFY active, add manual braking as required
- 4Ground spoilersVERIFY deployed (automatic, no arm position)
- 5Reverse thrustMAXIMUM (both engines)
- 6Aircraft stoppedSET park brake, assess
- 7ATCNOTIFY rejected takeoff, advise aircraft state
- 8If evacuation required: CABIN CREW PAEVACUATE, EVACUATE
- 1EDM - AUTOMATIC if cabin altitude exceeds 14,500 ft above 25,000 ft
- 2Crew oxygen masksON, establish communication
- 3EDM engages AP and AT, thrust to idle, ALT SEL to 15,000 ft, HDG hold
- 4Descent speed is set to Vmo -10 kts or Mmo -0.02M automatically
- 5SpoilersDEPLOY MANUALLY, they do not extend automatically
- 6Transponder 7700 and seat belt sign are set on automatic activation
- 7At 15,000 ft: ALT and HDG mode, speed 250 kts
- 8ATCADVISE, set 10,000 ft or MEA if higher
- 1Autopilot and autothrottleOFF
- 2Pitch and thrustSET from the memory items, then the ECL table
- 3ADS reversion pushbuttonUSE to select the alternate air data source
- 4ISI - CROSS-CHECK against both PFDs to identify the faulty source
- 5Speed trim bugUSE, the A220 has conventional speed stability
- 6Do not exceed 250 kts below 10,000 ft
- 7ATCADVISE, request vectors and a long final
- 8Land as soon as practical
- 1TOGAPRESS, call GO-AROUND, FLAP 2 (4)
- 2Pitch - ROTATE to maximum 10 deg nose up (aft fuselage strike above 10 deg)
- 3SpeedVGA
- 4Positive climbLANDING GEAR UP
- 5At acceleration altitude: FLC, SPD at or above green dot
- 6FlapsRETRACT on F3, F2, F1, F0 speeds
- 7Flaps up and above green dot: AFTER GO AROUND checklist
- 8ATC - NOTIFY go-around, state intentions, then re-plan with FORDEC
FLIGHT2.23.0Checklist
Synaptic A220-300MSFS 2024 · Emergency Procedures · 6procedures · 48 steps
Engine Fire - In Flight8 steps
| 01 | Master warningCANCEL, aural LEFT (RIGHT) ENGINE FIRE | |
| 02 | ECL - L(R) ENG FIRE non-normal checklist, follow the displayed steps | |
| 03 | Affected ENG RUN switchCONFIRM and OFF | |
| 04 | L(R) ENG FIRE switch - PUSH (closes fuel, bleed and hydraulic SOVs, arms bottles) | |
| 05 | BTL 1DISCHARGE, wait 30 seconds | |
| 06 | If fire persists: BTL 2DISCHARGE (either bottle feeds either engine) | |
| 07 | Above MSA: SHUTDOWN L(R) ENG procedure, no relight after a fire | |
| 08 | Land at nearest suitable airport |
Dual Engine Failure - In Flight8 steps
| 01 | MAYDAYDECLARE on guard frequency | |
| 02 | ECLfollow the displayed non-normal checklist | |
| 03 | APUSTART (APU bleed assisted start up to 23,000 ft) | |
| 04 | Windmill relight: speed above 250 kts, maximum altitude 27,000 ft | |
| 05 | Air starter assisted relight: speed below 250 kts | |
| 06 | ENG RUN switchOFF then ON for the relight attempt | |
| 07 | Emergency descentINITIATE if cabin altitude is rising | |
| 08 | Nearest runwayPLAN direct approach |
Rejected Takeoff8 steps
| 01 | Abort decisionMAKE before V1 | |
| 02 | Thrust leversIDLE (both) | |
| 03 | Autobrake RTOVERIFY active, add manual braking as required | |
| 04 | Ground spoilersVERIFY deployed (automatic, no arm position) | |
| 05 | Reverse thrustMAXIMUM (both engines) | |
| 06 | Aircraft stoppedSET park brake, assess | |
| 07 | ATCNOTIFY rejected takeoff, advise aircraft state | |
| 08 | If evacuation required: CABIN CREW PAEVACUATE, EVACUATE |
Emergency Descent8 steps
| 01 | EDM - AUTOMATIC if cabin altitude exceeds 14,500 ft above 25,000 ft | |
| 02 | Crew oxygen masksON, establish communication | |
| 03 | EDM engages AP and AT, thrust to idle, ALT SEL to 15,000 ft, HDG hold | |
| 04 | Descent speed is set to Vmo -10 kts or Mmo -0.02M automatically | |
| 05 | SpoilersDEPLOY MANUALLY, they do not extend automatically | |
| 06 | Transponder 7700 and seat belt sign are set on automatic activation | |
| 07 | At 15,000 ft: ALT and HDG mode, speed 250 kts | |
| 08 | ATCADVISE, set 10,000 ft or MEA if higher |
Unreliable Airspeed8 steps
| 01 | Autopilot and autothrottleOFF | |
| 02 | Pitch and thrustSET from the memory items, then the ECL table | |
| 03 | ADS reversion pushbuttonUSE to select the alternate air data source | |
| 04 | ISI - CROSS-CHECK against both PFDs to identify the faulty source | |
| 05 | Speed trim bugUSE, the A220 has conventional speed stability | |
| 06 | Do not exceed 250 kts below 10,000 ft | |
| 07 | ATCADVISE, request vectors and a long final | |
| 08 | Land as soon as practical |
Go-Around - Missed Approach8 steps
| 01 | TOGAPRESS, call GO-AROUND, FLAP 2 (4) | |
| 02 | Pitch - ROTATE to maximum 10 deg nose up (aft fuselage strike above 10 deg) | |
| 03 | SpeedVGA | |
| 04 | Positive climbLANDING GEAR UP | |
| 05 | At acceleration altitude: FLC, SPD at or above green dot | |
| 06 | FlapsRETRACT on F3, F2, F1, F0 speeds | |
| 07 | Flaps up and above green dot: AFTER GO AROUND checklist | |
| 08 | ATC - NOTIFY go-around, state intentions, then re-plan with FORDEC |