1
Q
Maximum Takeoff Weight
A
156,300Lbs
2
Q
Maximum Ramp Weight
A
157,000Lbs
3
Q
Maximum Landing Weight
A
129,500lb
4
Q
Minimum Flight Weight
A
80,000lb
5
Q
Maximum Zero Fuel Weight
A
123,000lb
6
Q
Maximum Flap Speed- Flaps 1
A
220kt
7
Q
Maximum Flap Speed- Flaps 2
A
200kt
8
Q
Maximum Flaps Speed- Flaps 3
A
200 KIAS
9
Q
Maximum Flaps Speed- Flaps 4
A
180 KIAS
10
Q
Maximum Flaps Speed- Flaps 5
A
160 KIAS
11
Q
Maximum Landing Gear Extension Speed
A
250kt
12
Q
Maximum Landing Gear Retraction Speed
A
220 KIAS
13
Q
Maximum Lading Gear Extended Speed
A
250kt
14
Q
Turbulence Penetration speed Below 10,000’
A
265kt
15
Q
Maximum Turbulence Penetration Speed Above 10,000’
A
280kt or 0.75M whichever is lower
16
Q
Windshield Wiper Speed
A
250 KIAS
17
Q
Tire Speed Limit
A
195 knots ground speed
18
Q
Maximum Pressure Altitude For Takeoff & Landing
A
8000’
19
Q
Maximum Operating Altitude
A
41,000’
20
Q
Maximum Ambient Temperature For Takeoff & Landing
A
52.5*C
21
Q
When is engine operation prohibited on the ground?
A
In ground fog conditions with OAT below -18*C
22
Q
When must cowl anti-ice system be on (ground)?
A
When OAT is 10C or below and visible moisture is present. Or when OAT is 10C or below and operating on contaminated surfaces.
23
Q
When must cowl anti-ice be on in air?
A
Cowl anti-ice must be ON or AUTO when in icing conditions or when ice is annunciated by the ice detection system.
24
Q
When must the wing anti-ice be on on the ground?
A
When OAT is 5C or below and visible moisture in any form is present. Or when OAT is 5C or less and operating on contaminated surfaces.
25
When must wing anti-ice be on in the air?
When in icing conditions or when ice is annunciated.
26
What are the restrictions on holding in icing conditions?
Do not hold with Flaps/slats extended
27
When must the wing anti-ice be turned OFF?
Above 35,000’
28
When is engine ice shedding performed?
When OAT 3*C or below and visible moisture in any form is present.
N1 to 60% momentarily within 30 minute intervals.
First run-up must be as soon as practicable.
29
Maximum crosswind for RCC 6
32 knots for takeoff
29 knots for landing
30
Maximum crosswind for RCC 4
27 knots
31
Maximum crosswind for RCC 3
20 knots
32
Maximum crosswind for RCC 2&1
10 knots
33
Maximum wind speed for cargo and PAX door operations?
40 knots
34
Maximum wind speed for cargo door held in open position?
65 knots
35
Maximum tailwind for takeoff & landing
15 knots
36
Maximum positive differential pressure
8.8 psid
37
During landing (at touchdown) the pressure differential must not exceed what value?
1 psid
38
Minimum height for auto pilot engagement?
400’ AGL
39
Minimum height for auto pilot use?
80’ AGL
40
Minimum oil temperature for APU start?
-40*C
41
How many APU start attempts?
3 start attempts in 1 hour with a 2 minute delay between starts.
42
Maximum altitude for APU bleed air extraction?
23,000’
43
Maximum AC Generator load?
75 KVA continuous
44
Maximum permissible continuous load on:
TRU 1&2
TRU3
TRU 1&2- 350 amps
TRU 3 - 225 amps
45
Maximum altitude with slat/flaps extended?
20,000’
46
Minimum height with flight spoilers manually extended?
500’ AGL
47
Minimum speed with flight spoilers manually extended?
VREF +10 knots
48
What’s the restriction on using Maximum Spoilers?
Use is prohibited except in an emergency
49
Maximum fuel imbalance
1000 LBS
50
Maximum usable fuel load
Left Main
Right Main
6725 LBS
51
Maximum usable fuel:
Center Tank
24,900 LBS
52
Maximum usable fuel:
Total
38,350lbs
53
Minimum fuel quantity for go-around?
975 LBS per wing with a maximum climb attitude of 10* nose up.
54
Maximum bulk fuel temperature for starting and operating?
52.5*C
55
Minimum bulk fuel temperature for takeoff?
-37*C
56
Maximum crosswind component for engine starting on ground?
43 knots
57
Maximum tailwind component for starting engines on the ground/
18 knots
58
Engine starter limitations
After 3 start attempts, or after 4 minutes of continuous cranking, a 30 minute delay cooling period is required.
Do not engage starter on the ground if N2 is above 20%
59
Engine warm-up
Oil temperature below -40*C
Engine start is prohibited.
60
Engine warm-up, oil temperature below -6*C
N1 idle
61
Engine warm up
Oil temperature between -6*C and 21*C
N1 30%
62
Engine warm-up, oil temperature from 21C to 49C
N1 50%
63
Engine warm-up
Oil temperature 49*C and above
No limit
64
Maximum negative differential pressure
-0.5 psid
65
Maneuvering limit load factor:
Flaps Up
-1.0g to 2.5g
66
Maneuvering limit load factor:
Flaps Down
0.0g to 2.0g
67
Maximum landing gear operating altitude?
20,000’
68
Kinds of Airplane Operations
VFR & IFR
Extended range operations
Extended overwater flight
Flight in icing conditions up to 35,000’
Landings with approach path no greater than 3.5*
69
Maximum operating speed VMO below 10,000’
300 KIAS
70
Maximum operating speed above 10,000’
VMO= 330kt
MMO= M 0.82
71
Design maneuvering speed in direct mode only?
300 KIAS
M 0.80
72
Limitations on F-BUG
It may be necessary to wait until below F-BUG in the case of F1 to F2 movement due to weight, turbulence, or margin of safety.
Flap deployment below F-BUG speed is only permitted during wings-level flight.
Operations below F-BUG speed is limited to F-BUG minus 10kt.
Banking maneuvers are prohibited at speeds below F-BUG
Use of speed brakes is prohibited while maneuvering if flight is at or below F-BUG
73
Taxi Speeds: Straight Dry
30 Knots GS
74
Taxi Speeds: Straight Contaminated
10knots-GS
75
Taxi Speeds: Turn Dry
10knots-GS
76
Taxi Speeds for turns- Contaminated
5 knots-GS
77
Maximum ambient temperature approved for takeoff and landing?
52.5*C
78
When must engine ice shedding be performed?
When OAT is 3*C or below and visible moisture in any form is present.
Engine run-up must be performed, momentarily, to a minimum of 60% N1at intervals no greater than 30 minutes.
The first run-up must be done as soon as practical.
79
Speed Corrections For Approach and Landing In Icing Conditions With Flap 5
If there is evidence of ice accretion:
VREF, VAC, VGA speeds must be increased by 5 KIAS.
80
What is the maximum runway slopes approved for takeoff and landing?
+/- 2%
81
When must you use High Wind takeoff?
If crosswind component exceeds 30 knots.
82
Tail Wind-Systems Limitation
It is prohibited to land with tailwinds greater than 10 knots with any failed system where an OLD or QRH additive factor is required.
83
When can you not use APU bleed air for takeoff?
When OAT is at or below 15* C.
84
Permissible Loads On DC Systems
The maximum permissible continuous load on TRU 1 and 2 is 350 amps.
The maximum permissible continuous load on TRU 3 is 225 amps. (Momentary Excedence of 225 amps on TRU 3 may be observed during APU start).
85
What is the Maximum Landing Gear BTMS Temperature For Gear Retraction?
The maximum brake temperature (BTMS) for gear retraction is BTMS value 13.
86
What is the Maximum allowable oil consumption?
0.4 qt/hr.
87
What is the maximum cross wind component for takeoff and landing with one thrust reverser inoperative?
Wet runway limited to 25 knots.
88
Minimum ambient temperature approved for take-off and landing?
-54 degrees Celsius
89
Cold Weather Operations
Takeoff is prohibited with frost, ice, snow or slush adhering to any critical surface.
Critical surfaces:
Wings
Horizontal stabilizer
Vertical stabilizer
Control surfaces
Engine inlets
90
Cold Weather Operations
Operation of the airplane is prohibited if the airplane, with the engines shut down, has been exposed to a ground ambient temperature below 30*C for a period exceeding two hours in the preceding 12 hours.
A220
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