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A220 - Air Canada > Perf. & Lim. > Flashcards

Perf. & Lim. Flashcards

1
Q

Can a refuelling be performed on battery power?

A

YES

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2
Q

MRW?

A

70,307 kg

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3
Q

MLW?

A

57,833 kg

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4
Q

MTOW?

A

69,853 kg

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5
Q

Max. Tailwind Tkof & Lndg?

A

15 kt
Above 10 kt refer Special Procedure

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6
Q

Max. pressure diff. ?

A

-0.5 / +8.8
+1 max. at landing

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7
Q

Can you use PACKS when ext. air cart is connected?

A

NO

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8
Q

Min AP engagement height?

A

400 ft

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9
Q

Lowest AP use height?

A

80 ft

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10
Q

During APP & LDG with A/T, approach speed must be?

A

Increased by 5 kt

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11
Q

Max. AC Load?

A

75 kVA

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12
Q

Max. DC Load TRU 1 & 2?

A

350 amp

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13
Q

Max. DC Load TRU 3?

A

225 amp

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14
Q

Max. altitude with flaps?

A

FL200

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15
Q

Lowest height with spoilers manually extended?

A

500 ft AGL

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16
Q

Min. speed with spoilers manually extended?

A

Vref + 10 kt

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17
Q

When can MAX spoilers be used?

A

Emergency ONLY

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18
Q

Max. fuel imbalance?

A

454 kg

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19
Q

Max. fuel quantity L & R tanks?

A

3050 kg

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20
Q

Max. fuel quantity Center tank?

A

11,300 kg

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21
Q

Max. TOTAL FUEL quantity?

A

17,400 kg

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22
Q

Max. FL in icing conditions?

A

FL350

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23
Q

Max. APP path angle?

A

3.8
>3.5 refer to Performance section

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24
Q

MZFW?

A

55,111 kg

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25
Q

Minimum Flight Weight?

A

36,287 kg

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26
Q

VMO > 8,000 ft?

A

330 kt

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27
Q

MMO?

A

M 0.82

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28
Q

VMO < 8,000 ft?

A

300 kt

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29
Q

VFE FLAP 1?

A

230 kt

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30
Q

VFE FLAP 2?

A

210 kt

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31
Q

VFE FLAP 3?

A

210 kt

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32
Q

VFE FLAP 4?

A

190 kt

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33
Q

VFE FLAP 5?

A

170 kt

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34
Q

VLO EXTENSION?

A

250 kt

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35
Q

VLO RETRACTION?

A

220 kt

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36
Q

VLE?

A

250 kt

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37
Q

TURBULENCE SPEED < 10,000 ft?

A

265 kt

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38
Q

TURBULENCE SPEED >10,000 ft?

A

280 kt

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39
Q

WINDSHIELD WIPER SPEED?

A

250 kt

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40
Q

TIRE LIMIT SPEED?

A

195 kt

41
Q

Max. AIRPORT ALTITUDE?

A

10,000 ft

42
Q

Max. FL?

A

410

43
Q

Max. TKOF TEMP?

A

52.5 c

44
Q

Min. TKOF TEMP?

A

-54 c

45
Q

Load Factor FLAPS UP?

A

-1.0 to +2.5 g

46
Q

Load Factor FLAPS DOWN?

A

0.0 to +2.0 g

47
Q

Min. Engine operation temp. in ground fog?

A

-18 c

48
Q

Cowl anti-ice must be ON on the ground when?

A

+10 c or below with any visible moisture
+10 c or below if contam. on ground

49
Q

Cowl anti ice must be on in flight when?

A

In icing conditions
When ICE is annunciated

50
Q

Wing anti-ice must be ON on the ground when?

A

+5 c or below with any visible moisture
+5 c or below if contam. on ground

51
Q

Wing anti-ice must be ON in flight when?

A

In icing conditions
When ICE is annunciated

52
Q

Wing anti-ice should be OFF above what level?

A

FL350

53
Q

Wing anti-ice is prohibited above what temp?

A

TAT > 15 c

54
Q

Ice shedding procedure on ground?

A

OAT 3 c or below and visible moisture
Min. 60% N1 every 30 minutes

55
Q

During an APP in icing conditions, Vref Vac and Vga must be increased by?

A

+ 5 kt

56
Q

Min. fuel tank temp. for Tkof?

A

-37 c

57
Q

Max. fuel tank temp. for start?

A

+ 52.5 c

58
Q

Unattended APU use, fuel quantity limitations?

A

Max. 2830 kg in either wing tank
Transfer to center tank if necessary

59
Q

Max. brake temp. (BTMS) for tkof?

A

6 units

60
Q

Max. brake temp. (BTMS) for gear retract?

A

13 units

61
Q

Min. oil temp. for APU start?

A
  • 40 c
62
Q

APU start limitations?

A

Max. 3 per hour
2 minute delay between starts

63
Q

Max. altitude APU use?

A

FL230

64
Q

ENG. warm-up with oil below -40 c?

A

Engine start prohibited.

65
Q

ENG. warm-up with oil below -6 c?

A

Idle only

66
Q

ENG. warm-up with oil between - 6 c and +21 c?

A

30% N1

67
Q

ENG. warm-up with oil between 21 c and 49 c?

A

50% N1

68
Q

ENG. warm-up with oil above 49 c?

A

No limit

69
Q

Max. EGT Tkof?

A

1054 c

70
Q

Max. EGT Continuous?

A

1016 c

71
Q

Above 290, max. N1 is?

A

95.2%

72
Q

ENG start limitations?

A

After 3 attempts or 4 min cranking, a 30 minute cooling period is required. Do not engage starter if N2 on ground > 20%

73
Q

Max. X-wind for start and ice shedding?

A

43 kt

74
Q

Max. tail-wind for start and ice shedding?

A

18 kt

75
Q

Can an defuel be performed on battery power?

A

NO. AC power is needed.

76
Q

Hydraulic system nominal pressure?

A

3,000 psi

77
Q

What is the backup to Hyd. Engine Driven Pump 1A?

A

PTU

78
Q

What is the backup to Hyd. Engine Driven Pump 2A?

A

AC Motor Pump ACMP 2B

79
Q

What is the backup to Hyd. AC Motor Pump 3A?

A

AC Motor Pump ACMP 3B

80
Q

The RAT hydraulic pump provides press. to what system?

A

System #3

81
Q

What happens in case of a Hyd. overheat in a system?

A

Fluid is drained overboard

82
Q

PTU pump is driven by fluid from which system?

A

By #2 system’s fluid

83
Q

Hyd. ACMP 2B is driven by what type of current?

A

AC current 115 VAC from AC BUS 1

84
Q

When does the backup ASMP 3B runs?

A

When ACMP 3A fails
For TKF & LDG

85
Q

Hyd. ACMP 3A and 3B are driven by what type of current?

A

AC current 115 VAC from AC BUS 2

86
Q

What systems are not powered by the RAT?

A

Nose Steering
Reverses
PTU
GND Spoilers
Gear

87
Q

RAT operates at what nominal pressure?

A

2,850 psi

88
Q

When would the PTU operate on AUTO?

A

QTY in system 1 is 5% & system 2 is running and when either:
TKF thrust is applied
SLAT/FLAP is in position 4 or 5
ALT FLAP is selected
EDP 1A fails or left engine inoperative
Parking brake is OFF during right single engine taxi

89
Q

When would ACMP 2B operate on AUTO?

A

QTY in system 2 is 5% & AC power available and when either:
TKF thrust is applied
SLAT/FLAP is in position 4 or 5
ALT FLAP is selected
EDP 2A fails or right engine inoperative
Parking brake is OFF during left single engine taxi
EDP 1A fails or left engine inoperative

90
Q

When would ACMP 3B operate on AUTO?

A

QTY in system 3 is 5% & AC power available and when either:
TKF thrust is applied
In flight SLAT/FLAP is out of zero
On ground during SLAT/FLAP deployment
One second after ACMP 3A fails

91
Q

What are the two modes of the FlyByWire system?

A

NORMAL and DIRECT

92
Q

Nose up pitch compensation is active until what bank angle?

A

33 deg. Beyond that aft sidestick must be applied

93
Q

At what speed does the YD activates?

A

70 kt

94
Q

What is the 1/2 bank mode max. bank angle?

A

15 degrees

95
Q

At what altitude is 1/2 bank mode auto activated?

A

31,500 ft

96
Q

What cabin altitude triggers the Emerg. Desc. Mode?

A

14,500 ft

97
Q

OEI cruise speed?

A

310 KIAS

98
Q

Max. diversion time and distance?

A

60 min / 390 nm

99
Q

Max. cabin pressure differential?

A

8.8 psi / -0.5 psi

A220 - Air Canada (1 decks)

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