Limitations Flashcards

1
Q

Flight manoeuvring load acceleration limits

A
  1. Clean config = -1 to +2.5G
  2. Other config = 0g to +2G
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2
Q

Approach Category

A

Cat C

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3
Q

Rescue and firefighting services

A

Category 6

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4
Q

Runway slope

A

Plus / mins 2%

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5
Q

Runway Altitude limits

A

-2,000 feet to 9,200 feet

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6
Q

Nominal and minimum runway widths

A

Nominal = 45m
Minimum = 30m

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7
Q

Maximum crosswind limit

A

38kts (including gusts)

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8
Q

Crosswind limit for second and first officers

A

Dry Runway = 20kts
Wet = 15kts

(Except when flying with training capt)

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9
Q

Max tailwind for takeoff and landing

A

15kts

(Note: +10kts means full flap required)

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10
Q

Maximum wind for passenger door operation

A

65kts

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11
Q

Max wind for FWD and AFT cargo door operations

A

40kts

If nose into wind or cargo doors on leeward side = 50kts

(Must be closed before 65kts)

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12
Q

Minimum taxi width

A

15m

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13
Q

Cockpit window open maximum speed

A

200kts

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14
Q

Maximum Flaps / Slats speeds

A

0 = VMO/MMO
1 = 230
1 plus F = 215
2 = 200
3 = 185
Full = 177

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15
Q

Maximum operating speed

A

VMO = 350
MMO = M 0.82

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16
Q

VLE (max speed with landing gear extended)

A

280 / 0.67

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17
Q

VLO extension (max speed extend gear)

A

250 / M 0.60

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18
Q

VLO Retraction (max speed to retract)

A

220 / M 0.54

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19
Q

Maximum tire speed

A

195

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20
Q

VMCL

A

Minimum control speed for landing

113

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21
Q

Minimum Control speed on narrow runway

A

Runway 30m……. +2.5
Runway 35m……. +1.5
Runway 40m……. 0

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22
Q

Wipers maximum operating speed

A

230

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23
Q

Max taxi speed during turn if very heavy

A

20

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24
Q

Maximum taxi weight

A

73,900

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25
Q

Maximum take off weight

A

73,500kg

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26
Q

Maximum landing weight

A

64,500

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27
Q

Maximum zero fuel weight

A

61,000

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28
Q

Minimum weight

A

37,230

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29
Q

Takeoff alternate range

A

320nm

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30
Q

En-route alternate range

A

400nm

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31
Q

With passengers on board - recommend max time without air conditioning

A

20 mins

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32
Q

Avionics ventilation. During ground operations, limit use of electric power supply (in normal avionics ventilation system configuration) as follows

A

OAT Below 49 (no limit)
49 to below 55 (2 hours)
55 to below 60 (1 hour)
60 to 64 (0.5 hours)

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33
Q

Cabin pressure. Max positive differential. Max negative differential. Safety relief valve setting

A

Max positive……. 9 PSI
Max negative…. -1.0 PSI
Relief valve………. 8.6 PSI

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34
Q

Minimum cabin alt selection

A

Minus 2,000

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35
Q

Max normal cabin altitude

A

8,000 ft

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36
Q

Cab Alt warning

A

9,550 ft (plus or minus 350)

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37
Q

Max Operating altitude

A

39,800

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38
Q

Max cabin altitude selection

A

14,000

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39
Q

Cabin outflow valve closure altitude

A

15,000

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40
Q

Autopilot. Minimum value at takeoff

A

100ft AGL and at least 5 seconds after liftoff

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41
Q

Autopilot. Minimum value:

In approach with F-G/S mode

A

200ft AGL

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42
Q

Autopilot. Minimum value:

In approach with FINAL APP, V/S or FPA mode

A

250ft AGL

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43
Q

Autopilot. Minimum value:

In circling approach

A

Category C = 500 AGL

Category D = 600 AGL

44
Q

Autopilot. Minimum value:

ILS approach when CAT1 is displayed on the FMA

A

160ft AGL

45
Q

Autopilot. Minimum value:

ILS approach when CAT2 Or CAT3 SINGLE or CAT3 DUAL is displayed on the FMA

A

0ft if autoland

46
Q

Autopilot. Minimum value:

GLS approach when CAT1 Is displayed on the FMA

A

160 AGL

47
Q

Autopilot. Minimum value:

GLS approach when AUTOLAND is displayed on the FMA

A

Zero if autoland

48
Q

Autopilot. Minimum value:

LPV approach (with SLS) when APPR1 is displayed on the FMA

A

160 AGL

49
Q

Autopilot. Minimum value:

PAR approach (Precision Approach Radar)

A

250 AGL

50
Q

Autopilot. Minimum value:

After manual go around

A

100 AGL

51
Q

Autopilot. Minimum value

“In all other phases”

A

500ft

52
Q

ILS Cat 2

Minimum decision height

A

100ft

53
Q

ILS CAT 2

How many autopilot must be engaged in APPR mode? What must be displayed on the FMA?

A

At least one autopilot

FMA - “CAT 2” or “CAT 3 SINGLE” or “CAT 3 DUAL”

54
Q

ILS CAT 2

Can you plan a manual landing following a CAT 2 Approach?

A

No - it’s not permitted

55
Q

ILS CAT 3 PASSIVE (SINGLE)

Minimum decision height?

A

50 ft

56
Q

ILS CAT 3 FAIL PASSIVE SINGLE

Autothrust required? Other info?

A

A/THR must be used in selected or managed speed

At least one autopilot must be engaged in APPR mode and “CAT 3 SINGLE” or “CAT 3 DUAL” must be shown on FMA

57
Q

ILS CAT 3 FAIL OPERATIONAL (Dual)

Alert height? Other info

A

100 ft

Both autopilots must be engaged in APPR mode and “CAT 3 DUAL” must be displayed on FMA

58
Q

ILS CAT 3 FAIL OPERATIONAL (Dual)

Cat 3 with DH - what is the decision height?

A

25 ft (Jet2)

59
Q

ILS CAT 3 FAIL OPERATIONAL (Dual)

Cat 3 without DH- what is min RVR?

A

75m

60
Q

GLS CATEGORY 1 - decision height?

A

200 ft

Without auto landing - at least one autopilot in APPR mode and “CAT 1” or “LAND” displayed on the FMA

GLS auto land is not permitted

61
Q

Autoland - Maximum wind conditions for ILS CAT 2 or CAT 3 and GLS CAT 1

A

Headwind…. 30 kts
Crosswind…. 20 kts
Tailwind…….. 10 kts

62
Q

APU - after 3 consecutive starts - how long must flight crew wait before another attempt?

A

1 hour

63
Q

APU - max N speed?

A

107%

64
Q

APU - Max EGT for APU start (below 35,000)?

A

1,090 degrees C

65
Q

APU - Max EGT for APU start (above 35,000)?

A

1,120 degrees C

66
Q

APU - Max EGT for APU running?

A

675 degrees C

67
Q

APU - 2 restrictions for APU Start/Shutdown whilst fuelling or defuelling

A
  1. If the APU failed to start or following an auto shutdown - do not start the APU
  2. If there is a fuel spill (perform a normal APU shutdown)
68
Q

APU BLEED

Max altitude to assist with engine start?

A

20,000 ft

69
Q

APU Bleed

Max altitude for air conditioning and pressurisation (single pack operation)?

A

22,500 ft

70
Q

APU Bleed

Max altitude for air conditioning and pressurisation (dual pack operation)?

A

15,000 ft

71
Q

Is it permitted to use APU Bleed air for wing anti-ice?

A

No

72
Q

Thrust setting / EGT Limits

Takeoff and go around (all engines operative)

A

Time: 5 mins
EGT: 950

73
Q

Thrust setting / EGT Limits

Takeoff and go around (one engine inoperative)

A

Time: 10 mins
EGT: 950

74
Q

Thrust setting / EGT limits

Max continuous thrust

A

Time: no limit
EGT: 915 degrees

75
Q

Thrust time limit / EGT limit

For starting (on ground and in flight)

A

Time: no limit
EGT: 725 degrees

76
Q

Engine Shaft Speeds

N1
N2

A

N1….. 104%
N2…. 105%

77
Q

Oil

Max continuous temperature

A

140 degrees C

78
Q

Oil

Maximum transient temperature (15 mins)

A

155 degrees

79
Q

Oil

Minimum starting temperature

A

Minus 40 degrees

80
Q

Oil

Minimum temperature before take off

A

Minus 10 degrees

81
Q

Oil - minimum quantity

A

9.5qt plus estimated consumption (average is 0.5qt per hour)

82
Q

Minimum oil pressure

A

13 PSI

83
Q

Oil pressure - when does cold start bypass valve open?

A

305 PSI

84
Q

Starter information

A
  1. Standard start includes 3 start attempts (this is one cycle)
  2. For ground starts - wait 20 seconds between cycles
  3. 15 min wait between failed cycles
85
Q

Flex Takeoff - is it permitted on contaminated runways?

A

No

86
Q

Flex Takeoff

TFFLEX cannot be (3 things)?

A
  1. Higher than TMAXFLEX, equal to ISA plus 53 degrees C (68 degrees)
  2. Lower than flat temp (TREF)
  3. Lower than actual OAT
87
Q

Maximum altitude with flaps / slats extended

A

20,000 ft

88
Q

Fuel temp for Jet A1 (min and max)?

A

Min…. Minus 43
Max…. Plus 54

89
Q

Fuel imbalance at takeoff. If inner tanks balanced, what is max asymmetry in the outer tanks?

A

370 kg

90
Q

Fuel imbalance at landing. If inner tanks balanced, what is max asymmetry in the outer tanks?

A

690 kg

91
Q

Minimum fuel quantity at take off

A

1,500 kg

92
Q

Definition of icing conditions?

A
  1. OAT (on ground) or TAT (in flight) is at or below 10 degrees C AND there is visible moisture in any form
93
Q

Definition of severe ice accretion?

A

Approximately 5mm thick

94
Q

Does the aircraft have rain repellant?

A

No - it has been deactivated

95
Q

Definition of thin hoarfrost

A

Thin hoarfrost is typically a white crystalline deposit which usually develops uniformly on exposed surfaces on cold and cloudless nights. You can clearly see things under it

96
Q

Maximum brake temperature for takeoff?

A

300 degrees (brake fans off)

97
Q

Maximum nosewheel steering angle?

A

85 degrees

98
Q

Taxi with deflated or damaged tires.

If maximum one tire per gear is deflated, what is maximum speed during turn?

A

7 kt

99
Q

Taxi with deflated or damaged tires.

If two tires are deflated on the same main gear (max one gear) - what is the maximum taxi speed

A

3 kt

100
Q

Taxi with deflated or damaged tires.

What is the maximum nosewheel steering angle?

A

30 degrees

101
Q

What is the APU Battery Restart Limit?

A

25,000

102
Q

What is the max altitude for APU operation?

A

The aircraft max altitude (39,800)

103
Q

Max NWS limit

A

95 degrees

104
Q

Max NWS with a motorised pushback

A

85 degrees

105
Q

Max nosewheel steering angle with deflated or damaged tyres

A

30 degrees