A220 - Limitations Flashcards
(204 cards)
1
Q
Under what category is the airplane certified for day and night operations?
A
Transport Category
2
Q
What are the visibility conditions the airplane is certified to operate in?
A
VFR (Visual Flight Rules) and IFR (Instrument Flight Rules).
3
Q
Is the airplane certified for extended overwater flights?
A
Yes, it is certified for extended overwater flight.
4
Q
nder what conditions is the airplane certified for ETOPS operations?
A
ETOPS of 75 minutes, only when conducted wholly within Canadian Domestic Airspace or Benign Areas of Operation.
5
Q
What is the maximum altitude at which the airplane is certified for flight in icing conditions?
A
35,000 feet.
6
Q
What is the maximum certified approach path angle for landings?
A
3.8 degrees.
7
Q
If the approach angle is greater than 3.5 degrees, where should guidance be found?
A
Refer to AOM 1.05.00 – Approaches with Approach Angle Greater than 3.5 Degrees up to 3.8 Degrees.
8
Q
What is the Maximum Ramp Weight (MRW) for aircraft [101–124]?
A
68,039 kg
9
Q
What is the Maximum Takeoff Weight (MTOW) for aircraft [101–124]?
A
67,585 kg
10
Q
What is the Maximum Landing Weight (MLW) for aircraft [101–124]?
A
57,833 kg
11
Q
What is the Maximum Zero Fuel Weight (MZFW) for aircraft [101–124]?
A
55,111 kg
12
Q
What is the Minimum Flight Weight (MFW) for aircraft [101–124]?
A
36,287 kg
13
Q
What is the Maximum Ramp Weight (MRW) for aircraft [125–135]?
A
70,307 kg*
14
Q
What is the Maximum Takeoff Weight (MTOW) for aircraft [125–135]?
A
69,853 kg*
15
Q
What is the Maximum Landing Weight (MLW) for aircraft [125–135]?
A
57,833 kg
16
Q
What is the Maximum Zero Fuel Weight (MZFW) for aircraft [125–135]?
A
55,111 kg
17
Q
What is the Minimum Flight Weight (MFW) for aircraft [125–135]?
A
36,287 kg
18
Q
Why are the MRW and MTOW values lower than the original OEM limits on certain aircraft?
A
Because Air Canada limits them through LSTC Q-LSA22-009/D and AFMS-1-030807. These weights can be modified per the STC.
19
Q
Where can you find the specific MTOW for an individual aircraft?
A
On the registration placard installed in the flight deck, on both the Captain and First Officer’s side.
20
Q
Can the Maximum Takeoff Weight (MTOW) and/or Maximum Landing Weight (MLW) be further limited?
A13:
A
Yes, they may be further limited due to performance considerations
21
Q
What is the maximum speed (VFE) with FLAP 1 extended?
A
230 KIAS
22
Q
What is the maximum speed (VFE) with FLAP 2 extended?
A
210 KIAS
23
Q
What is the maximum speed (VFE) with FLAP 3 extended?
A
210 KIAS
24
Q
What is the maximum speed (VFE) with FLAP 4 extended?
A
190 KIAS
25
What is the maximum speed (VFE) with FLAP 5 extended?
170 KIAS
26
What is the maximum speed for landing gear extension (VLO)?
250 KIAS
27
What is the maximum speed for landing gear retraction (VLO)?
220 KIAS
28
What is the maximum recommended turbulence penetration speed (VRA) at or below 10,000 feet?
265 KIAS
29
What is the maximum recommended turbulence penetration speed (VRA) above 10,000 feet?
280 KIAS or 0.75 Mach, whichever is lower.
30
When flying in moderate to severe turbulence above 10,000 feet, what determines the turbulence penetration speed limit?
The lower of 280 KIAS or 0.75 Mach.
31
The windshield wiper must not be operated at more than
250
32
The tire limit speed is
195 Ground Speed
33
What are the maneuvering limit load factors with flaps up?
−1.0 g to 2.5 g
34
What are the maneuvering limit load factors with flaps down?
0.0 g to 2.0 g
35
Procedure A — Temperature Limitations for Takeoff
Under Procedure A, is takeoff permitted if turnaround time is ≤120 minutes and OAT is above −54°C?
Yes, takeoff is permitted.
36
Under Procedure A, if turnaround time exceeds 120 minutes, what conditions must be met for takeoff?
The aircraft must be electrically powered during turnaround and cabin temperature maintained to prevent freezing in the water system.
37
Under Procedure A, is takeoff allowed when OAT is below −54°C?
No, takeoff is prohibited.
38
Under Procedure B, is takeoff allowed when OAT is between 0°C and −30°C?
Yes, takeoff is permitted.
39
Under Procedure B, when is takeoff prohibited if the airplane was exposed to temperatures below −30°C?
If it was exposed for more than 2 hours in the preceding 12 hours with engines shut down.
40
Is engine operation permitted in ground fog conditions when OAT is below −18°C?
Is engine operation permitted in ground fog conditions when OAT is below −18°C?
41
Is infrared deicing allowed during cold weather operations?
No, it is prohibited.
42
When must the cowl anti-ice system be ON during ground operations?
When OAT is 10°C or below and:
* Visible moisture in any form is present, or
* Operating on runways, ramps, or taxiways with snow, ice, standing water, or slush.
43
What defines icing conditions in flight?
icing conditions exist at a TAT of 10°C or below and visible moisture in any form is present, except when SAT is -40°C or below.
44
When must the cowl anti-ice system be AUTO or ON during flight?
* When in icing conditions, or
* When ICE is annunciated by the ice detection system.
45
When must the wing anti-ice system be ON for takeoff during ground operations?
Visible moisture in any form is present, or
Operating on runways with snow, ice, standing water, or slush.
46
When must the wing anti-ice system be AUTO or ON during flight?
* When in icing conditions, or
* When ICE is annunciated by the ice detection system.
47
What are the restrictions on wing anti-ice use?
* Do not hold in icing conditions with flaps/slats extended.
* Must be OFF above 35,000 ft.
* Use is prohibited when TAT is above 15°C
48
Is operation in Super-cooled Large Droplet (SLD) icing conditions allowed?
No, continued operation in SLD icing is prohibited.
49
What indicates SLD icing conditions?
ice accretion on the flight compartment side windows.
50
What anti-ice systems must be ON in SLD icing?
Both wing and cowl anti-icing systems must be ON.
51
What must you do when side window icing occurs in SLD conditions?
Leave icing conditions.
52
When must engine ice shedding (ground) be performed?
* When OAT is 3°C or below and visible moisture is present.
* Run engine up to at least 60% N1 every 30 minutes.
* First run-up should be done as soon as practical during taxi-out.
53
How to address engine vibrations in flight due to icing?
Apply a momentary increase in thrust up to CLB thrust.
54
What speed corrections are required for approach and landing in icing conditions with FLAP 5?
Increase V_REF, V_AC, and V_GA speeds by 5 KIAS.
55
Maximum runway slopes approved for takeoff and landing are:
±2%
56
What is the maximum tailwind component approved for takeoff?
15 knots.
57
What must be referenced for takeoff with tailwind components above 10 knots?
Standard Operating Procedures – Take-off, High Wind Procedure.
58
What is the maximum tailwind component approved for landing?
15 knots.
59
What must be referenced for landing with tailwind components above 10 knots?
AOM 1.05.00 – Take-Off and Landing with Tailwind Components Greater Than 10 Knots
60
What is the maximum positive differential pressure?
8.8 psid
61
What is the maximum negative differential pressure?
-0.5 psid
62
What is the maximum pressure differential allowed at touchdown?
1.0 psid
63
How long can the doors be closed with packs off, no ground ventilation (LPGC), and passengers on board?
No more than 15 minutes (except during deicing operations)
64
During deicing operations with packs off, what should be done?
Minimize the time the packs are off
65
What is the limit for operating without ECS or external cooling (LPGC) when OAT is above 40°C (104°F)?
30 minutes
66
What does an external air conditioning source provide?
Conditioned air to the flight compartment and cabin
67
What must crews avoid when using an external air conditioning source?
Do not operate the packs to prevent damage to the aircraft’s air conditioning system
68
What is the minimum height for autopilot engagement?
400 feet AGL
69
What is the minimum height for autopilot use?
80 feet AGL
70
When must autothrottle be disconnected?
Before touchdown during touch and go procedures
71
What must be done to approach speed during approach and landing with autothrottle?
Increase approach speed by 5 knots
72
Is AURAL WARN INHIB allowed during APPR2 (no Autoland)?
No, operation is prohibited
73
What engine configurations are allowed for APPR2 (no Autoland)?
Single or Dual
74
What engine configuration is required for LAND 2 or LAND 3 (Autoland)?
Dual
75
What is the acceptable approach glideslope angle for APPR2?
2.5° to 3.25°
76
What is the maximum runway slope for APPR2?
2.0% upslope, 2.0% downslope
77
What is the maximum runway slope for Autoland (LAND 2 or 3)?
0.8% upslope, 1.0% downslope
78
What is the minimum runway width required for LAND 2 or LAND 3?
45 meters (150 feet)
79
Is autopilot required for both APPR2 and LAND 2/3 operations?
Yes, ON for both
80
Is autothrottle required for APPR2?
ON or OFF (Use is recommended)
81
Is autothrottle required for LAND 2 or LAND 3?
ON
82
Is Autoland available in APPR2 mode?
No
83
Is Autoland available in LAND 2 or LAND 3?
Yes
84
What is the minimum autopilot use height for APPR2?
Applicable (standard rules apply)
85
What are the CAT III minimums?
50 ft DH / RVR 600 (175 m)
86
What is the maximum airport pressure altitude for autoland (LAND 2 or LAND 3)?
8466 feet.
87
At what height are wind components (including gusts) measured for autoland limitations?
10 meters (33 feet) tower height
88
What is the headwind limit for APPR 2?
25 knots
89
What is the headwind limit for LAND 2 or LAND 3 with CAT II or III weather?
25 knots
90
What is the demonstrated headwind limit for LAND 2 or LAND 3 with CAT I or better weather?
29 knots.
91
What is the crosswind limit for APPR 2?
15 knots*.
92
What is the crosswind limit for LAND 2 or LAND 3 with CAT II or III weather?
15 knots
93
What is the demonstrated crosswind limit for LAND 2 or LAND 3 with CAT I or better weather?
24 knots*
94
What is the tailwind limit for all autoland configurations (APPR 2, LAND 2, LAND 3)?
10 knots.
95
What does the asterisk (*) next to crosswind limits indicate?
Use the most limiting value and refer to the Maximum Recommended Crosswind for Landing.
96
What may occur during (V) ALTS CAP mode with the flight director?
The flight guidance/autopilot may not maintain the selected airspeed—crew intervention may be required.
97
What is the maximum continuous load allowed on the AC generator?
75 kVA.
98
What is the maximum permissible continuous load on TRU 1 - 2
350 amps.
99
What is the maximum permissible continuous load on TRU 3?
225 amps.
100
What is the maximum altitude with slats and flaps extended?
20,000 feet.
101
What is the minimum height AGL for manually extending flight spoilers?
500 feet AGL.
102
What is the minimum speed for manually extending flight spoilers?
VREF + 10 KIAS.
103
When is the use of MAX spoilers permitted?
Only in emergency situations.
104
Why is the use of MAX spoilers restricted to emergencies only?
Because they can cause unexpected structural loads leading to early fatigue or damage in turbulence or during high-g maneuvers.
105
What must flight crew do if MAX spoilers are extended during flight?
Report it to maintenance post-flight for appropriate action.
106
What is the maximum permissible fuel imbalance between the left and right main tanks?
454 kg.
107
Is fuel usable when the fuel quantity indicator reads zero?
No, it is not usable.
108
What is the maximum usable fuel load for the left main tank?
3050 kg (3770 L).
109
What is the maximum usable fuel load for the right main tank?
3050 kg (3770 L).
110
What is the maximum usable fuel load for the center tank?
11,300 kg (13,968 L).
111
What is the total maximum usable fuel load for all tanks combined?
17,400 kg (21,508 L).
112
What is the minimum fuel quantity required for a go-around per wing?
442 kg (with the airplane level and 10° nose-up attitude).
113
What is the maximum bulk fuel temperature for starting and operating?
52.5°C.
114
At what bulk fuel temperature is takeoff prohibited?
Below -37°C.
115
What must be the status of manual transfer and gravity crossflow during take-off?
Both must be OFF.
116
When is unattended APU operation prohibited?
If either wing tank quantity is greater than 2830 kg.
117
What message requires following a non-normal procedure during fuel transfer?
FUEL LEAK SUSPECT.
118
What must be done when operating on the ground if either wing tank exceeds 2830 kg?
Start the left engine first.
119
When must a manual fuel transfer be done from the wing to the center tank?
* If either wing tank > 2830 kg, and
* Center tank < 10,670 kg.
120
Can TACAN be selected from the navigation database?
No, selection of TACAN from the navigation database is prohibited.
121
Is it allowed to enter Place/Bearing/Distance (PBD) waypoints that use an airport identifier?
No, this is prohibited.
122
What must flight crews verify regarding STAR and approach procedures in the FMS?
Speed constraints on the last waypoint of a STAR and first waypoint of an approach procedure must be verified and corrected as needed.
123
Is use of the FPLN UPLINK function in flight allowed?
No, it is prohibited.
124
What must be done with any “REQUEST PENDING” before takeoff?
It must be cleared.
125
Can uplink flight plans contain PBD waypoints?
No, they must not contain Place/Bearing/Distance waypoints.
126
Are altitude changes allowed in the final approach segment of any FMS approach?
No, except for automatic FMS temperature compensation, altitude changes (including FAF and step-down fixes) are prohibited.
127
What is the maximum leg distance for RNAV-1/RNP-1?
200 nautical miles (nm)
128
What is the maximum leg distance for RNAV-2/RNP-2?
400 nautical miles (nm)
129
What is the maximum leg distance for RNP-4?
500 nautical miles (nm)
130
What is the maximum leg distance for RNP-10?
500 nautical miles (nm)
131
Where is RNAV-1/RNP-1 typically used?
On SIDs (Standard Instrument Departures) and STARs (Standard Terminal Arrival Routes)
132
Where is RNAV-2 typically required?
133
Where is RNP-4 or RNP-10 typically required?
In Oceanic/Remote airspace (e.g., WATRS, parts of the Gulf of Mexico)
134
Are distance limitations applicable on random point-to-point routes under ATC surveillance?
No
135
Are distance limitations applicable on V or J airways?
No
136
Where is FMS navigation prohibited due to latitude?
North of 73°N and south of 60°S
137
Can FMS be used as a primary navigation source beyond the FAF for ILS, LOC, LOCBC, LDA, SDF, and IGS approaches?
No, it is prohibited.
138
What speed mode must be used when flying a V APP in the final landing configuration?
MAN SPD (Manual Speed)
139
Can OPT ALT and MAX ALT on FMS PERF – CLB and CRZ pages be used for flight planning?
No, it is prohibited.
140
How must true headings be entered?
in the xxxT format
141
Is operation using QFE altimeter setting allowed?
No, it is prohibited.
142
What must be ensured before starting or continuing RVSM operations?
All required RVSM equipment must be operational as specified.
143
RVSM Required Equipment: What is the requirement for the autopilot?
Must be operational.
144
RVSM Required Equipment: What is the requirement for the altitude alerting system?
Must be operational.
145
RVSM Required Equipment: How many altitude reporting transponders must be operational?
At least one (1) must be operational.
146
RVSM Required Equipment: How many air data computers must be operational?
Two (2) must be operational.
147
Can airplane navigation be based on the TAWS terrain display?
No. Airplane navigation must not be predicated upon the terrain display.
148
What must be done with the TAWS TERR switch when taking off or landing within 15 NM of an airport not in the TAWS database?
The TERR switch must be selected to INHIB to avoid unwanted alerts.
149
TLAF: What limits must be observed when proceeding onto the departure runway?
Do not exceed 35 knots ground speed or 55% N1 until within 10° of runway heading.
150
HUD: What is the purpose of the flare guidance on the HUD?
The HUD flare guidance is for advisory purposes only on all approaches.
151
What is the minimum oil temperature for an APU start?
The minimum oil temperature for an APU start is −40°C.
152
How many APU starts/start attempts are permitted within one hour?
A maximum of three starts/start attempts are permitted within one hour.
153
What is the required delay between APU start attempts?
A two-minute delay must be observed between start attempts.
154
Is APU starting and operation permitted outside the aircraft’s operating envelopes?
APU starting and operation is only permitted within the aircraft's Altitude and Temperature/Altitude and Speed operating envelopes as shown in AOM 1.01.20.
155
What is the altitude limit for APU bleed air extraction?
The altitude limit for APU bleed air extraction is 23,000 feet.
156
What factors affect the altitude limit for APU bleed air extraction?
Air-conditioning pack operation affects the altitude limit based on:
Number of cabin occupants
Outside air temperature
(See APU Bleed Air section for more details).
157
158
159
Front
Back
160
What type of engines are used on the aircraft?
PurePower™ PW1524G-3, quantity two.
161
What is the engine warm-up procedure for temperatures below −40°C?
Engine start is prohibited below −40°C.
162
What is the engine warm-up procedure for temperatures below −6°C?
Idle is required below −6°C.
163
What is the engine warm-up procedure for temperatures between −6°C and 21°C?
30% N1 is required between −6°C and 21°C.
164
What is the engine warm-up procedure for temperatures from 21°C to 49°C?
50% N1 is required from 21°C to 49°C.
165
What is the engine warm-up procedure for temperatures above 49°C?
No limit is imposed for temperatures above 49°C.
166
What is the maximum EGT for max takeoff thrust?
1054°C for up to 5 minutes.
167
What is the oil pressure minimum for max takeoff thrust?
50.3 PSIG minimum.
168
What is the oil temperature range for max takeoff thrust?
49°C to 163°C.
169
What is the N1/N2 time limit for max continuous thrust?
Continuous operation is allowed at 100% N1/N2.
170
What is the maximum EGT for max continuous thrust?
1016°C for continuous operation.
171
What is the maximum N1 for reverse thrust?
100% N1 is allowed for reverse thrust.
172
What is the oil pressure range for reverse thrust?
50.3 / 175.3 PSIG.
173
What is the minimum oil temperature for reverse thrust?
49°C to 163°C.
174
What is the operating temperature range for ground idle (SLS)?
-40°C to 163°C.
175
What is the operating temperature range for flight idle?
-40°C to 163°C.
176
What is the starting EGT limit?
1054°C for starting.
177
What is the operating temperature range for starting?
-40°C to 163°C.
178
What is the limitation for oil temperature above 163°C?
Maximum of 174°C for up to 20 minutes. Total operation between 163°C and 174°C must not exceed 20 minutes.
179
What is the maximum N1 above 29,100 feet?
The maximum N1 is 95.2% above 29,100 feet.
180
What must be reported when the HMU is inoperative?
Any exceedance of more than 40 continuous seconds must be reported.
181
What should the engine indications be used for?
The engine limit display markings on the EICAS must be used to determine compliance with the maximum/minimum limits and precautionary ranges.
182
What should be done when operating thrust reversers in cold weather (−40°C to −20°C)?
If turnaround time exceeds 120 minutes, the thrust reversers must be cycled two times before take-off on contaminated runways.
183
What is the limitation for thrust reverser cycles if the OAT is less than −40°C?
Thrust reversers must be cycled before take-off until the last deployment cycle time is equal to or less than 2.5 seconds.
184
How long must a 30-minute cooling period be observed after engine start attempts?
After three start attempts or four minutes continuous cranking, a 30-minute cooling period is required.
185
What is the limitation for engaging the starter on the ground?
Do not engage the starter on the ground if indicated N2 rpm exceeds 20%.
186
What is the engine operating envelope for starting and operation?
Engine starting and operation is permitted within the aircraft's Altitude and Temperature/Altitude and Speed operating envelopes as shown in AOM 1.01.20.
187
What is the minimum time required to operate the engine at or near idle before shutdown?
The engine must be operated at or near idle for a minimum of 3 minutes (5 minutes recommended) before shutdown.
188
What is the definition of near idle?
Near idle is defined as up to 40% N1.
189
What is the limitation for restarting an engine after a high power shutdown?
The affected engine must not be re-started after a high power shutdown (greater than 40% N1), unless guidance in AOM 1.03.71 is used.
190
What is the restriction on emergency in-flight restarts?
There is **no restriction** on emergency in-flight restarts.
191
What are the maximum crosswind and tailwind components for starting on the ground?
Maximum crosswind: 43 kts, Maximum tailwind: 18 kts.
192
What are the maximum crosswind and tailwind components for taxi?
There are **no limits** for taxiing.
193
What is the maximum wind speed for ice shedding at 60% N1?
Maximum crosswind: 43 kts, Maximum tailwind: 18 kts.
194
What is the requirement for high power ground runs (>60% N1)?
Maintenance runs must be done with the aircraft headed into wind.
195
What is the mximum oil consumption?
.38L or .4qt per hour
196
197
Front
Back
198
Where can the oil grades be found?
Refer to Aircraft maintenance publication.
199
What is the maximum allowable oil consumption?
The maximum allowable oil consumption is 0.38 l/hr (0.4 qt/hr).
200
What is the approved use of thrust reversers?
Thrust reversers are approved for **ground use only**.
201
Is activation of reverse thrust levers in flight allowed?
No, activation of the reverse thrust levers in flight is prohibited.
202
Is the use of thrust reversers for backing up allowed?
No, use of thrust reversers for backing up is prohibited.
203
Are go-around maneuvers or touch-and-go allowed after thrust reverser deployment?
No, go-around maneuver and touch-and-go are prohibited after deployment of the thrust reversers.
204
