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Work Study > A330 > Flashcards

A330 Flashcards

1
Q

Maximum Runway Slope

A

+/- 2%

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2
Q

Maximum tailwind component for takeoff and landing

A

15 knots
10 knots for landing elevation above 11,000’
If landing with greater than 10 knots tailwind, FLAPS FULL is recommended

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3
Q

Maximum crosswind component for takeoff and landing

A

40 knots

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4
Q

MMO

A

M0.86

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5
Q

VMO

A

330 knots

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6
Q

VFE CONF 1

A

240 knots

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7
Q

VFE CONF 1+F

A

215 knots

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8
Q

VFE CONF 2

A

196 knots (select on approach up to 205 knots)

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9
Q

VFE CONF 3

A

186 knots

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10
Q

VFE CONF FULL

A

180 knots

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11
Q

VLE/VLO (Maximum speed for extending, retracting or operating with landing gear extended)

A

250 knots/M0.55

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12
Q

Maximum speed for landing gear gravity extension

A

200 knots

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13
Q

Maximum speed with a cockpit window open

A

230 knots

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14
Q

Maximum speed with wipers operating

A

230 knots

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15
Q

Maximum tyre speed

A

204 knots

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16
Q

Maximum operating altitude

A

41,450’

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17
Q

Maximum elevation for takeoff and landing

A

12,500’

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18
Q

Maximum temperature for takeoff and landing

A

ISA + 40° (+55°C at sea level)

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19
Q

Minimum TAT

A

-53°C

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20
Q

Flight manoeuvring load limits

A

-1g to +2.5g (clean)
0g to +2g (other configs)

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21
Q

Minimum runway width

A

45 metres

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22
Q

A330-200: VMCL (Minimum control speed - Landing)

A

118 knots

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23
Q

A330-200: VMCG (minimum control speed - ground) at sea level

A

112 knots

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24
Q

A330-200: VMCA (minimum control speed - air) at sea level

A

106 knots

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25
Q

A330-300: VMCL (minimum control speed - landing)

A

123 knots

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26
Q

A330-300: VMCG (minimum control speed - ground) at sea level

A

124 knots

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27
Q

A330-300: VMCA (minimum control speed - air) at sea level

A

122 knots

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28
Q

Maximum recommended crosswind with RCC 5 (good)

A

32 knots

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29
Q

Maximum recommended crosswind with RCC 4 (good/medium)

A

27 knots

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30
Q

Maximum recommended crosswind with RCC 3 (medium)

A

20 knots

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31
Q

Maximum recommended crosswind with RCC 2 (medium/poor)

A

20 knots

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32
Q

Maximum recommended crosswind with RCC 1 (poor)

A

15 knots

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33
Q

Takeoff is not recommended with the following runway conditions:

A

Wet ice
Water on top of compacted snow
Dry snow or wet snow over ice

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34
Q

Severe turbulence penetration speeds

A

Up to FL200: 240 knots
Up to FL350: 260 knots
Above FL350: M0.8 (A330-200)

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34
Q

Severe turbulence penetration speeds

A

Up to FL200: 240 knots
Up to FL350: 260 knots
Above FL350: M0.8 (A330-200)

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34
Q

Severe turbulence penetration speeds

A

Up to FL200: 240 knots
Up to FL350: 260 knots
Above FL350: M0.8 (-200)
M0.78 (-300)

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35
Q

Ground wind limits with open doors

A

40 knots while opening or closing all doors

50 knots if aircraft nose into wind
50 knots for opening or closing FWD/AFT cargo doors if on the downwind side

60 knots while open

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36
Q

Maximum difference between Captain & First Officer’s altitude display on the ground

A

20 feet

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37
Q

Maximum difference between Captain or First Officer’s altitude display and the ISIS on the ground

A

60 feet

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38
Q

Maximum difference between Captain or First Officer’s altitude display and the standby altimeter on the ground

A

300 feet

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39
Q

Maximum difference between Captain or First Officer’s altitude display and gate elevation

A

60 feet
- Up to 75 feet is permitted for one sector only

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40
Q

In flight RVSM altimeter discrepancy (cruise altitudes)

A

120 feet between PFDs
320 feet between standby altimeter and either PFD
See RVSM table in FCOM

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41
Q

What requirements are there for a landing above maximum landing weight in case of in flight turn back or diversion?

A

Overweight landing procedure is to applied

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42
Q

Maximum takeoff weight

A

-200D & -300: 233,000kg
-200L: 238,000kg

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43
Q

Maximum Landing Weight

A

EBA-D: 180,000kg
EBE-V: 182,000kg
QPA-J: 187,000kg

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44
Q

With passengers on board, maximum time without air conditioning

A

20 minutes

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45
Q

Must not use bleed air from the APU and from the HP Air Start Unit at the same time

A

Prevent adverse effect on the Bleed Air System

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46
Q

Must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time

A

Prevent adverse effect on the Air Conditioning System

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47
Q

Maximum cabin differential pressure

A

9.25 psi

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48
Q

Maximum negative differential pressure

A

-0.73 psi
-1.00 psi for EBA-D

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49
Q

Pressurisation safety valve setting

A

8.85 psi

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50
Q

Minimum height for autopilot engagement

A

100 feet AGL
At least 5 seconds after liftoff

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51
Q

Minimum height for autopilot disconnection for a manual landing

A

FMA CAT 1: 160 feet AGL
FMA CAT 2 or 3: 80 feet AGL
FINAL APP, V/S, or FPA modes: 250 feet AGL
All other phases of flight or AP modes: 500 feet AGL

OP DES or DES modes can be used in approach, above 500’ only if FCU altitude is set to the higher of 500’ AGL or MDA

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52
Q

Maximum wind speeds for autoland

A

Headwind: 35 knots
Crosswind: 20 knots (15 knots if below 550 metres RV/RVR)
Tailwind: 10 knots

Applies to Tower-reported winds only, not ND display

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53
Q

Glide slope angles for autoland

A

2.5° to 3.25°

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54
Q

Allowed landing configuration for Autoland

A

Config 3 or FULL

If one engine is inoperative, only Config 3 is approved, with all procedures complete by 1000’

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55
Q

Automatic rollout is approved on what runway surface conditions?

A

Dry or Wet

Performance on contaminated runways has not been demonstrated

56
Q

Maximum weight for autoland in an emergency

A

229,000kg

57
Q

Reverse thrust limitations

A

Maximum reverse thrust should not be used below 70 knots
Idle reverse thrust permitted to aircraft stop

58
Q

FLEX takeoff thrust is not permitted on contaminated runways

A

FlySmart EFB will not protect against this limitation

59
Q

Engine thrust limitations

A

TOGA/FLEX thrust modes: 5 minutes (10 minutes with one engine inoperative)

60
Q

Engine thrust limitations

A

TOGA/FLEX thrust modes:
Maximum Time: 5 minutes (10 minutes with one engine inoperative)
Maximum EGT: 975°C
MCT thrust mode:
Maximum EGT: 940°C
Engine Start on Ground:
Maximum EGT: 750°C
Engine Start in Flight:
Maximum EGT: 975°C

61
Q

Maximum N1 & N2 speeds

A

N1: 115.5%
N2: 113%

62
Q

Engine Oil Limitations: Maximum temperature

A

Maximum continuous temperature: 160°C
Maximum temperature for up to 15 mintues: 175°C

63
Q

Maximum continuous engine starter operation:

A

5 minutes

64
Q

Cooldown period between engine start attempts

A

30 seconds after first attempt, 10 minutes after each subsequent attempt

65
Q

Do not engage the engine starter when N2 is above?

A

30%

66
Q

Engine starter limitations: What is defined as a single cycle?

A

A standard automatic start with up to three start attempts

67
Q

APU maximum altitude to supply electrical load

A

41,450’

68
Q

APU maximum altitude to assist engine start

A

20,000’

69
Q

APU maximum altitude to supply both electrical load and bleed air

A

14,600’ (on ground)
17,500’ (dual packs)
22,500’ (single pack)

70
Q

Is the use of APU bleed air for wing anti ice permitted?

A

No

71
Q

Maximum altitude for APU start on battery power (EMER ELEC CONFIG)

A

25,000’

72
Q

APU cool down period following three consecutive APU start attempts

A

60 minutes

73
Q

APU maximum EGT

A

For start: 1250°C
Running: 650°C

74
Q

APU maximum N speed

A

107%

75
Q

Is APU start or shutdown permitted during fuelling operations?

A

Yes

76
Q

If the APU fails to start or following an automatic APU shutdown during fuelling operations:

A

Do not attempt another start of the APU

77
Q

APU: If a fuel spill occurs

A

Perform a normal APU shutdown

78
Q

Maximum altitude with flaps/slats extended

A

20,000’

79
Q

Extended flight in icing conditions with slats extended…

A

… should be avoided

80
Q

Avoid rapid/large alternating control inputs

A

Especially in combination with large changes in pitch, roll or yaw

81
Q

Approach based on radio navaids:
- What AP modes may be used?
- Do the navaids need to be installed/serviceable?
- Do navaids need to be monitored?

A

May be performed in NAV, APP NAV, or FINAL APP modes

If GPS PRIMARY available:
- Navaids may be unserviceable
- Airborne equipment may be inoperative or not installed
- Navaids need not be tuned or monitored during the approach

82
Q

RNAV approach:
- What AP modes can be used?
- What requirements must be met?

A

May be performed in FINAL APP or NAV/FPA modes

GPS PRIMARY must be available

Aircraft other than -200L require the approach to be validated and approved before using FINAL APP mode

83
Q

Maximum fuel temperature

A

+55 C

84
Q

Minimum fuel temperature

A

-44 C for Jet A1
-37 C for Jet A

85
Q

Maximum fuel imbalance (Inner Tanks)

A

2900kg to 7500kg depending on distribution

86
Q

Maximum fuel imbalance (Outer Tanks)

A

1480kg to 1730kg depending on distribution

87
Q

Minimum fuel quantity for takeoff

A

5200kg

ECAM alerts related to low fuel level in the wing tanks must not appear

88
Q

Maximum brake temperature for takeoff

A

300 C if brake fans OFF
150 C if brake fans ON (or used recently)

89
Q

Maximum taxi speed (normal operations)

A

30 knots

10 knots for turns of 90 degrees or more

90
Q

Maximum taxi speed (deflated tyres)

A

1 tyre deflated per gear: 7 knots while turning

2 tyres deflated on the same gear (max one main gear): 3 knots and max NWS angle 30 degrees

If tyre damage is suspected, an inspection is required prior to taxi

91
Q

Minimum crew oxygen pressure

A

1330psi

92
Q

In seat power supply system

A

Must be turned OFF for takeoff and landing

93
Q

Memory Items: Loss of Braking

A

Announce “Loss of Braking”
Reverse - Max
Brake pedals - Release
“Anti skid off” - Order
Antiskid/NWS switch - OFF
Brake pedals - Press
Max brake pressure - 1000psi
If still no braking: Parking brake - Use

94
Q

Memory Items: Emergency Descent

A

Announce “Emergency Descent”
Crew oxygen masks - Use
Signs - ON
Emergency Descent - Initiate
If A/THR not active: Thrust levers - Idle
Speedbrake - Full

95
Q

Memory Items: Stall Recovery

A

Announce “Stall - I have control”
Nose down pitch control - Apply
Bank - Wings level
When out of stall:
Thrust - increase smoothly as needed
Speedbrakes - check retracted
Flight path - recover smoothly
If in clean configuration and below 20,000’:
Flap 1 - Select

96
Q

Memory Items: Stall Warning at Liftoff

A

Announce “Stall - TOGA 15 Degrees”
Thrust levers - TOGA
Pitch attitude - 15 degrees
Bank - Wings level

97
Q

Memory Items: Unreliable Speed Indication

A

If the safe conduct of the flight is impacted:
Announce “Unreliable Speed”
AP - OFF
ATHR - OFF
FD - OFF
Pitch/thrust setting:
Below thrust reduction altitude: 15/TOGA
Above thrust reduction altitude: 10/CLB
Above 10,000’: 5/CLB
Flaps (If 0-3): Maintain current config
Flaps (If Full): Select flaps 3
Speedbrakes - Check retracted
Landing Gear - Up
When above MSA or circuit altitude, level off for troubleshooting

98
Q

Memory Items: EGPWS Warnings

A

Announce “Pull Up TOGA”
Simultaneously:
AP - OFF
Pitch - Pull Up
Thrust Levers - TOGA
Speedbrake - Check retracted
Bank - Wings level or adjust
Do not change configuration until clear of obstacle

99
Q

Memory Items - TCAS Warnings

A

Announce “TCAS - I have control”

At RA activation:
AP - OFF
FD - OFF
Vertical speed - adjust or maintain
ATC - Notify

If “CLIMB” RA during approach, in CONF 3 or FULL:
Go around - perform
Vertical speed - monitor

When “clear of conflict” is announced:
ATC - Notify
Lateral and Vertical guidance- adjust
AP/FD - as required

100
Q

Memory Items - Windshear during takeoff (after V1)

A

Announce “Windshear - TOGA”
Thrust levers - TOGA
Reaching VR - Rotate
SRS orders - Follow
Do not change configuration until out of windshear
Closely monitor the flight path and speed
Advise ATC “Windshear Escape”
Smoothly recover to normal climb when out of windshear

101
Q

Memory Items - Windshear warning (Airborne)

A

Announce “Windshear - TOGA”
Thrust levers - TOGA
AP (if engaged) - keep ON
SRS orders - Follow
Do not change configuration until out of windshear
Closely monitor the flight path and speed
Smoothly recover to normal climb when out of windshear

102
Q

What approaches can use Low Visibility Procedures (Captain PF)?

A

ILS (LOC/GS modes)
RNAV overlay, RNP LNAV, RNP LNAV/VNAV (FINAL APP mode)

(AP and/or FD must be coupled to a glide slope or glide path)

103
Q

Memory PA: Alert Order

A

“Attention! All passengers remain seated and await further instructions”

104
Q

Memory PA: Brace Order

A

“Brace - Brace - Brace”

105
Q

Memory PA: Ditching Order

A

“Attention! This is a ditching. Follow your crew member’s instructions”

106
Q

Memory PA: Emergency Descent

A

“Attention Cabin Crew. Emergency Descent”

107
Q

Memory PA: Evacuation Order

A

“Evacuate - Evacuate - Evacuate”

108
Q

Memory PA: Seat Belt

A

“All passengers and crew be seated and fasten seatbelts”

109
Q

Memory PA: Turbulence

A

“All passengers and crew be seated and fasten seat belts immediately”

110
Q

Engine Oil Limitations: Minimum temperature for engine start

A

Minimum temperature for engine start: -40°C

111
Q

Engine Oil Limitations: Minimum oil quantity

A

12 qt, plus estimated consumption at 0.56 qt/hour

112
Q

Engine Oil Limitations: Minimum oil quantity

A

Minimum oil quantity: 12 qt, plus estimated consumption at 0.56 qt/hour

113
Q

Engine Oil Limitations: Minimum oil pressure

A

Minimum oil pressure: 10 psi at idle, 30 psi at TO thrust

114
Q

Memory Items: Windshear warning (Takeoff before V1)

A
  • If there are significant variations in airspeed and airspeed trend below indicated V1, reject the takeoff
  • Flight crew must decide if there is sufficient runway remaining to stop the aircraft as indicated V1 may be reached later than expected
115
Q

Stable approach criteria:

A

-All normal checklists completed
- Fully configured for landing (by 1000’RA)
- Approach path is contained within the flight tolerances

116
Q

When must the aircraft be configured for landing?

A

Fully configured by 1000’RA for all approaches

117
Q

Maximum rate of descent (3000’ to 5000’ AGL)

A

Current height in fpm

118
Q

Maximum rate of descent (1000’ to 3000’)

A

2000fpm

119
Q

What is the latest point the nominated vertical approach path must be intercepted?

A

Must be established by the FAF/FAP if the use of an instrument procedure is required, otherwise intercept by 1000’ RA

120
Q

Tolerances for all approaches: Rate of descent

A

Maximum 1000fpm below 1000’RA

121
Q

Tolerance for all approaches: Visual approach path (VASI/PAPI)

A

No significant deviation from the nominated approach path

122
Q

Tolerances for all approaches: Tracking

A

Must be tracking the extended centreline by 500’ unless flying a published procedure

123
Q

Tolerances for all approaches: Airspeed

A

-5 to +10 knots when below 500’RA

124
Q

Tolerances for all approaches: Energy levels

A

Aircraft energy levels correct for the configuration/prevailing conditions
Be away of thrust/energy levels into the flare, and the effect on engine spool up time for a go around

125
Q

Tolerances for an ILS/LLZ/LDA

A

Localiser: 1/2 dot
Glide slope: 1/2 dot

126
Q

Tolerances for a VOR approach:

A

Tracking: 1/2 dot (2.5 degrees)

127
Q

Tolerances for an NDB approach:

A

5 degrees

128
Q

Tolerances for RNP LNAV approach

A

Lateral deviation 0.3nm from the initial/intermediate waypoint

Vertical: not below the minimum segment altitude

129
Q

Tolerances for an RNP LNAV/VNAV approach:

A

Lateral: deviation 0.3nm
Vertical: Prior to VIP - not below minimum segment altitude
After the VIP - vertical path minus 75’

130
Q

What approaches may be flown using decelerated approach procedures?

A

If flown with vertical guidance from a glideslope or glide path (i.e. APPR or FINAL APP modes)

OR

If the approach is flown in VMC

131
Q

Approach tolerances: When should the PM call “SPEED”?

A

Speed exceeds -5 to +10 knots below 500’RA

132
Q

Approach tolerances: When must the PM call “SINK RATE”?

A

Rate of descent exceeds 1000fpm below 1000’RA

133
Q

When must the PM call “BANK”?

A

Bank exceeds 7 degrees

134
Q

When must the PM call “PITCH”?

A

Pitch lower than 0 degrees or higher than 10 degrees

135
Q

Tolerances during Landing: when must the PM call “BANK BANK”?

A

Bank reaches 7 degrees

136
Q

Tolerances during Landing: When must the PM call “PITCH PITCH”?

A

Pitch reaches 7.5 degrees

137
Q

Tolerances during Go Around: When must the PM call “BANK”?

A

Bank exceeds 7 degrees

138
Q

Tolerances during Go around: When must the PM call “PITCH”?

A

Pitch less than 10 degrees or greater than 20 degrees

139
Q

Tolerances during go around: When must the PM call “SINK RATE”?

A

No climb rate

140
Q

Memory Items: Windshear during take-off (before V1)

A

If there are significant variations in airspeed and airspeed trend below indicated V1, reject the take-off

Aircraft may reach indicated V1 later than expected, so flight crew must ensure there is sufficient runway remaining to stop the aircraft.

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