FCOM VOL 2 (Type Rating)

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Question English Answer English
What do PLT and CPLT identify in the A220 FCOM?
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Physical crew positions: PLT is the left pilot position and CPLT is the right pilot position.
What are OEB Immediate Actions?
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Actions identified in an Operations Engineering Bulletin that must be memorized and immediately applied without referring to the OEB.
When do MMEL requirements cease to apply?
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After the thrust levers are advanced at the start of takeoff.
When may a tripped circuit breaker normally be reset or cycled in flight?
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Only when an explicit FCOM or QRH procedure specifies that action.
Up to what altitude is the basic A220 approved for flight in icing conditions?
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Up to 35,000 ft.
What is the basic maximum landing approach-path angle in Chapter 2?
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3.5 degrees unless modified by an applicable supplement.
Can structural MTOW or MLW be further restricted?
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Yes. Performance considerations may impose a lower permitted weight.
What effect does landing-gear retraction have on the A220 CG position?
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The effect is negligible.
What is the A220 VMO at and below 8,000 ft?
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300 KIAS.
What is the A220 high-altitude maximum operating Mach number?
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Mach 0.82.
What are the A220 VFE values for FLAP 1 through FLAP 5?
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FLAP 1: 230 KIAS; FLAP 2: 210 KIAS; FLAP 3: 210 KIAS; FLAP 4: 190 KIAS; FLAP 5: 170 KIAS.
What is the maximum landing-gear extension speed on the A220?
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250 KIAS.
What is the maximum landing-gear retraction speed on the A220?
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220 KIAS.
What is the maximum speed with the landing gear extended?
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250 KIAS.
What is the recommended turbulence penetration speed on the A220?
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265 KIAS at or below 10,000 ft, or 280 KIAS above 10,000 ft, or Mach 0.75, whichever is lower.
What is the maximum windshield-wiper operating speed?
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250 KIAS.
What is the A220 tire limit speed?
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195 knots ground speed.
Does operating below VA make rapid alternating control inputs structurally safe?
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No. Rapid and large alternating control inputs may cause structural failure at any speed, including below VA.
What restriction applies to full control inputs in Direct Mode?
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Full elevator, rudder and aileron inputs and maneuvers near stall angle of attack must be confined to speeds below VA.
What is the A220 maximum operating altitude?
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41,000 ft.
What are the maximum and minimum ambient temperatures approved for A220 takeoff and landing?
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Maximum +52.5°C and minimum -54°C.
What are the A220 maneuvering limit load factors with flaps up and flaps down?
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Flaps up: -1.0 g to +2.5 g; flaps down: 0.0 g to +2.0 g.
At what OAT does the A220 FCOM define cold-weather operations?
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At an OAT of 0°C or below.
Is takeoff permitted with frost, ice, snow, or slush adhering to an A220 critical surface?
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No.
When is engine operation prohibited in ground fog?
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When OAT is below -18°C.
When is takeoff prohibited in ground freezing fog?
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When ground freezing fog exists and visibility is less than 150 m (500 ft).
Is infrared deicing approved on the A220?
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No. Infrared deicing is prohibited.
What is the ground temperature threshold for required cowl anti-ice use?
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OAT 10°C or below when the specified moisture or surface-contamination conditions exist.
How are in-flight icing conditions defined for A220 anti-ice limitations?
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TAT 10°C or below with visible moisture, except when SAT is -40°C or below.
What is the takeoff temperature threshold for required wing anti-ice use?
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OAT 5°C or below with the specified visible-moisture or runway-contamination conditions.
What are the key A220 wing anti-ice limitations in flight?
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Do not hold in icing with flaps/slats extended; wing anti-ice must be OFF above 35,000 ft and must not be ON above TAT 15°C.
What action is required when A220 SLD icing is identified?
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Select wing and cowl anti-ice ON and leave the icing conditions; continued operation in SLD icing is prohibited.
When is A220 ground engine ice shedding required?
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At OAT 3°C or below with visible moisture.
What is the A220 ground engine ice-shedding schedule?
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Momentarily increase to at least 60% N1 at intervals not exceeding 30 minutes, with the final ice shedding within 5 minutes before takeoff.
What speed correction is required for a FLAP 5 approach and landing in icing conditions?
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Increase VREF, VAC, and VGA by 5 KIAS.
What is the maximum approved runway slope for A220 takeoff and landing?
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±2%.
What is the basic maximum A220 tailwind component for takeoff and landing?
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10 kt.
What source must be used for the A220 Smoke/Fire/Fumes procedure?
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The QRH.
What are the maximum wind limits for passenger and cargo door operation?
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40 kt for opening or closing and 65 kt with the door held open.
What are the A220 pressurization differential-pressure limits?
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Maximum positive 8.8 psid, maximum negative -0.5 psid, and no more than 1.0 psid at initial touchdown.
What are the A220 autopilot minimum engagement and minimum use heights in the applicable configuration?
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Minimum engagement 400 ft AGL; minimum use 80 ft AGL.
What is the minimum APU oil temperature for starting?
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-40°C.
What are the APU start-attempt limitations?
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No more than three starts or start attempts in one hour, with at least two minutes between attempts.
What is the general maximum altitude for APU bleed-air extraction?
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23,000 ft, subject to the detailed pack, occupant, and temperature limitations.
What is the maximum altitude with A220 slats or flaps extended?
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20,000 ft.
What are the limitations for manually extended A220 flight spoilers?
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At least 300 ft AGL and at least VREF + 10 KIAS; MAX spoilers are for emergencies only.
What happens to fuel remaining in a tank when its fuel quantity indicator reads zero?
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It is considered unusable.
What is the minimum A220 fuel quantity for go-around?
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442 kg (975 lb) per wing under the specified level-aircraft and maximum 10-degree nose-up climb-attitude conditions.
What are the A220 bulk-fuel temperature limits relevant to takeoff?
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Maximum bulk fuel temperature is +52.5°C and takeoff is prohibited below -37°C.
What must be the status of manual fuel transfer and gravity crossflow for takeoff?
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They must be OFF.
Can A220 FPLN UPLINK be used in flight?
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No. Its use in flight is prohibited and any REQUEST PENDING must be cleared before takeoff.
When must NAV mode be selected for a localizer approach?
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Before the Final Approach Fix.
What speed mode must be used when flying VAPP in final landing configuration?
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MAN SPD.
Is QFE altimeter setting permitted on the A220?
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No. QFE operation is prohibited.
What is the minimum engine oil temperature for takeoff?
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49°C.
How long may maximum takeoff thrust normally be used?
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5 minutes, extendable to 10 minutes for an OEI contingency.
What cooling period is required after three engine start attempts or four minutes of continuous cranking?
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30 minutes.
How long must an engine normally operate at or near idle before shutdown?
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At least three cumulative minutes; near idle is up to 40% N1.
What is required in Engine Takeoff Wind Zone 3?
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Takeoff is prohibited.
What applies if either wing tank contains more than 2,830 kg of fuel?
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Unattended APU operation is prohibited and the left engine must be started first.
When is manual fuel transfer required on the ground if a wing tank exceeds 2,830 kg?
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When the center tank contains less than 10,670 kg; transfer fuel from the affected wing tank to the center tank until below 2,830 kg.
What do the symbols 🔹 and 🔹🔹 mean in A220 normal procedures?
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🔹 means first flight of the day; 🔹🔹 means once a day.
Why must the first four Power-on steps be performed from memory?
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Because the ECL is not available before the batteries are turned on.
What are the first four A220 Power-on memory actions?
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PARK BRAKE ON; BATT 1 AUTO; BATT 2 AUTO; ECL on DU2.
How long should the crew wait between aircraft power-off and power-on?
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15 seconds.
How long should Ground Service Mode be OFF before aircraft power-up?
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At least one minute.
How long must the APU switch be held in START during the Power-on procedure?
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At least 3 seconds, then allow it to return to RUN.
What must occur before electrical-system configuration changes are made during APU start?
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APU GEN must show online on the ELEC synoptic.
What must be done before another APU start attempt after an APU SHUTDOWN advisory during start?
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Set the APU switch to OFF.
When must the A220 Cabin Inspection be completed?
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Before the first flight of the day or after any crew change.
How long must the cabin ceiling and sidewall lights remain BRIGHT before the first flight?
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At least 30 minutes.
What indications are expected during a lavatory smoke-detector self-test?
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The detector sounds, the status indicator turns red, and the ceiling advisory panel flashes orange.
What is the required condition of thrust-reverser and fan-cowl latches during the walkaround?
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Latched and flush.
What is the required thrust-reverser condition during the external walkaround?
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Stowed.
What is the expected position of the MFS and ground spoilers during the walkaround?
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Flush with the upper wing surface.
Can clear ice form on an A220 wing when ambient temperature is above 0°C?
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Yes, if cold-soaked fuel at 0°C or below chills the wing skin and moisture freezes on it.
When must pilots specifically ensure that the upper wing is free of clear ice?
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When fuel temperature is 0°C or below and high humidity or visible moisture is present.
What is the first required response to a TLAF NOT A RUNWAY or RUNWAY DISAGREE alert?
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Confirm the aircraft position.
What must not be done during the APU start cycle?
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Do not make electrical-system configuration changes until APU GEN is online.
What must be done if APU SHUTDOWN appears during the APU start cycle?
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Set the APU switch OFF before attempting another start.

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