AOM 1 Flashcards

1
Q

MTOW

A

67,585

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2
Q

MLW

A

57,833

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3
Q

MZFW

A

55,111

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4
Q

MMO

A

0,82

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5
Q

VMO

A

330

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6
Q

VFE 1

A

230

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7
Q

VFE 2

A

210

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8
Q

VFE 3

A

210

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9
Q

VFE 4

A

190

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10
Q

VFE 5

A

170

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11
Q

VLO Down

A

250

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12
Q

VLO Up

A

220

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13
Q

VLE

A

250

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14
Q

Turbulence speeds

A

265 below 10,000
280 or 0.75 above 10,000

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15
Q

Max ambient temp

A

52.5c / -54c

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16
Q

Manœuvring loads

A

-1.0g / +2.5g flaps up
0.0g / +2.0g flaps down

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17
Q

Cowl anti-ice on the ground at…

A

+10c and below with moisture/contamination

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18
Q

Wing anti-ice on the ground at…

A

+5c or below with moisture/contamination

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19
Q

Wing anti-ice OFF in flight at…

A

TAT above +15c

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20
Q

Engine run up needed when…

A

OAT 3c or below with moisture/contamination. 60% N1 at max 30min intervals.

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21
Q

Approach in icing conditions, Vref, VAC and VGA must be increased by

A

5 kts

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22
Q

Max runway slopes

A

+/- 2%

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23
Q

Max tailwind takeoff and landing

A

15 kts
High wind procedure beyond.

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24
Q

Max diff pressure

A

8.8 psi

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25
Q

Max neg diff pressure

A

-0,5 psi

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26
Q

Min height AP engagement

A

400 ft

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27
Q

Min height AP usage

A

80 ft

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28
Q

Minimums CAT III restricted to

A

50 ft DH and RVR 600

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29
Q

APPR 2, LAND 2, LAND 3, wind limits

A

Headwind 25
Crosswind 15
Tailwind 10

30
Q

Max altitude flaps extended

A

20,000 ft

31
Q

Minimum height to use spoilers

A

500 ft

32
Q

Minimum speed to use spoilers

A

Vref + 10

33
Q

Wing tank capacity

A

3,770 L / 3,050 kg

34
Q

Center tank capacity

A

13,968 L / 11,300 kg

35
Q

Total fuel capacity

A

21,508 L / 17,400 kg

36
Q

Max fuel temp for operation

A

52.5c

37
Q

Min fuel temp for takeoff

A

-37c

38
Q

APU unattended is prohibited if wing tank has more than

A

2,830 kg

39
Q

Left engine must be started first if either wing tank has more than

A

2,830kg

40
Q

If either wing tank has more than 2,830 and center tanks is less than 10,670

A

Fuel transfer required

41
Q

Max brake temp takeoff

A

6 units

42
Q

Max brake temps for gear retract

A

13 units

43
Q

Min oil temp for APU start

A

-40c

44
Q

of APU starts

A

3 max per hour
2min delay between each

45
Q

Max altitude for APU bleed use

A

23’000ft

46
Q

Max wind door operation
Max wind door opened

A

40 kts
65 kts

47
Q

Min oil temp engine start

A

-40c

48
Q

Max N1 with oil below -6c

A

Idle

49
Q

Max N1 with oil between -6c and 21c

A

30%

50
Q

Max N1 with oil between 21c and 49c

A

50%

51
Q

Reversers cycling

A

If turnaround more than 120min then cycle twice before takeoff:

5min prior between -40c and -20c
2min prior below -40c

52
Q

Max wind starting and run ups

A

43kts crosswind
18kts tailwind

53
Q

OEI cruise speed

A

310

54
Q

60min max diversion distance

A

390nm

55
Q

75min max diversion distance

A

481

56
Q

Max takeoff alternate distance

A

351

57
Q

Flight will be planned to arrive with an EFOB of

A

1,300kg

58
Q

APU fuel burn

A

Elec 100kg/hr
Elec + Bleed 115kg/hr

59
Q

Flight crews must ensure that arrive at destination within —– of the last service check.

A

72hrs

60
Q

In-charge must be advised to purge the water tank if the turn around is

A

More than 3 hours at -20c or below
Or if advised by DXP

61
Q

Normal descent speed

A

290/0.78

62
Q

Normal climb speed

A

250 below 10,000
290/0.76 above 10,000

63
Q

Default VPA angle

A

2.7 degrees

May be adjusted by no more than 0.4

64
Q

Landing configuration max bank angle at Vref

A

25 degrees

65
Q

Landing configuration in icing conditions max bank angle is 25 degrees at what speed

A

Vref + 5

66
Q

30 degrees bank turns in landing configuration: Vref must be increased by

A

5 kts
10 kts in icing conditions

67
Q

A220 Approch category

A

Usually Category C
Category D if required

68
Q

Max crosswind for landing RCC 6&5

A

29kts

69
Q

High wind takeoff procedure is for tailwind of

A

10kts and more

70
Q

3.5 to 3.8 degrees approaches max tailwind and restrictions

A

5kts
FLAP 5
Press Alt 1,500ft max
ISA + 25 max