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HAL Study > A330 Freighter Limitations Summary (Bold Qs should be memorized) > Flashcards

A330 Freighter Limitations Summary (Bold Qs should be memorized) Flashcards

1
Q

Length

A

208’ 11”

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2
Q

Wingspan

A

197’ 10”

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3
Q

Tail Height

A

55’ 3”

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4
Q

Minimum Turning width for 180-degree turn

A

157’

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5
Q

Max Taxi Weight (MTW)

A

515.6 Klbs

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6
Q

Max Takeoff Weight (MTOW)

A

513.6 Klbs

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7
Q

Max Landing Weight (MLW)

A

412.2 Klbs

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8
Q

Max Zero Fuel Weight (MZFW)

A

385.8 Klbs

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9
Q

Minimum Weight

A

266.7 Klbs

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10
Q

Flight Maneuvering Load Acceleration Limit: Clean configuration

A

-1.0g to +2.5g

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11
Q

Flight Maneuvering Load Acceleration Limit: Other than clean configuration

A

0g to +2.0g

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12
Q

Max. Altitude

A

41,450’

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13
Q

Max. Runway Altitude

A

12,500

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14
Q

Max. Runway Slope

A

±2%

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15
Q

Max. Takeoff Crosswind

A

32 kts (gusts included)

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16
Q

Max. Takeoff Tailwind

A

15 kts

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17
Q

Max. Landing Crosswind

A

40 kts (gusts included)

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18
Q

Max. Landing Tailwind

A

10 kts

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19
Q

Max wind to operate passenger/cargo doors

A

40 kts (50 nose into wind)

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20
Q

Max wind for passenger/cargo doors open

A

60 kts

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21
Q

Max wind for Main Deck Cargo Door operation

A

40 kts
*Main Deck Cargo Door must be closed before wind speed exceeds 60 kts

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22
Q

VMO/MMO

A

330 kts / M.86

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23
Q

VFE Flap 1 (1+F)

A

240 kts (215 kts)

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24
Q

VFE Flap 2 (1*)

A

196 kts (205 kts)

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25
Q

VFE Flap 3

A

186 kts

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26
Q

VFE Flap FULL

A

180 kts

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27
Q

Min. Control Speed for Landing (VMCL)

A

126 kts

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28
Q

Max. Altitude with flaps/slats extended

A

FL200

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29
Q

VLE/VLO

A

250 kts / M.55

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30
Q

Max. Tire Speed

A

204 GS

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31
Q

VLE for gravity gear extension

A

200 kts

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32
Q

Max. Windshield wiper speed

A

230 kts

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33
Q

Max Cockpit window open speed

A

230 kts

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34
Q

Speedbrakes

A

No Limitation

35
Q

Max. Positive Differential

A

9.25 psi

36
Q

Max. Negative Differential

A

-0.73 psi

37
Q

Safety Relief Valve Setting

A

8.85 psi to -0.26 psi

38
Q

Air Conditioning with LP Ground Unit

A

Do not use packs

39
Q

Air Conditioning with HP Ground Unit

A

Do not use APU bleed

40
Q

Autopilot minimum height for use: Takeoff

A

100’ AGL

41
Q

Autopilot minimum height for use: Non ILS approach

A

250’ AGL (MDA OpSpec C071)

42
Q

Autopilot minimum height for use: ILS when CAT 2 or CAT 3 not displayed

A

160’ AGL (DA-40 OpSpec C071)

43
Q

Autopilot minimum height for use: Go-around

A

100’ AGL

44
Q

Autopilot minimum height for use: All other phases

A

500’ AGL

45
Q

Max. Autoland Wind Limits: Headwind

A

25 kts (20 kts in OEI)

46
Q

Max. Autoland Wind Limits: Tailwind

A

10 kts

47
Q

Max. Autoland Wind Limits: Crosswind

A

15 kts (10 kts in OEI)

48
Q

Autoland Configuration Allowed

A

CONF 3 or CONF FULL

49
Q

HAL A330 Aircraft Approach Category [FOM 4.3]

A

Category “C”

50
Q

Smallest Outer Tank fuel imbalance limit

A

3260 lbs

51
Q

Max. fuel imbalance limits may be exceeded when

A

in “exceptional conditions”

52
Q

Max. fuel temperature for JET A/A1

A

+55°C

53
Q

Min. fuel temperature (inner tank)

A

-44°C ~ -54°C

54
Q

Min. fuel quantity for takeoff

A

11,461 lbs

55
Q

Hydraulics normal operating pressure

A

3000 psi +/- 200 psi

56
Q

Max. brakes temperature for takeoff

A

300°C

57
Q

Nosewheel steering angle limit

A

72°

58
Q

Rudder steering angle limit

A

6°

59
Q

Braked pivot turns (one main gear fully stopped)

A

Not Allowed

60
Q

Max. taxi speed with one/two tires deflated per gear

A

7 kts / 3 kts

61
Q

Max. NWS angle if two tires deflated on the same main gear

A

30°

62
Q

IRS Nav max. RNP-10 triple-IRS time without GPS update

A

6.2 hours from alignment

63
Q

Min. Courier Oxygen pressure (2 bottles)

A

1500 psi or higher for each bottle
*Refer to table 1 in FCOM-LIM-OXY

64
Q

LOW OIL LEVEL ECAM advisory

A

May start/operate for 15 hrs

65
Q

APU Starter Limits

A

After 3 starts need 60 minutes to cool

66
Q

APU Max. altitude for start and operation

A

41,450’ (aircraft ceiling)

67
Q

APU Max. altitude for battery-only start

A

25,000’

68
Q

APU Max. altitude for one pack bleed and electrics

A

22,500’

69
Q

APU Max. altitude for bleed engine start

A

20,000’

70
Q

APU Max. altitude for two pack bleed and electrics

A

17,500’

71
Q

APU Bleed for wing anti-ice

A

Not Permitted

72
Q

ENG EGT limits: Takeoff and Go-around

A

20s at 920°C 5m or (10m with engine failure) at 900°C

73
Q

ENG EGT limits: MCT

A

850°C

74
Q

ENG EGT limits: Starting Normal / In Flight

A

700°C / 850°C

74
Q

ENG Min. oil quantity (highest of)

A

15qts (6qts + est. consumption)
*Average estimated consumption = 0.7qt/hr

75
Q

ENG Starter Max. continuous operation

A

5m

76
Q

ENG Cooling period after 5m continuous operation or 3 cycles

A

30m

77
Q

ENG Starter Max starter engagement on Ground and In Flight

A

10% and 30% N3

78
Q

Reverse Thrust Selection in flight

A

Prohibited

79
Q

Backing aircraft using reverse thrust

A

Prohibited

80
Q

Max. reverse should not be used below

A

70 kts

81
Q

Max. temp. FLEX

A

ISA +60°C

82
Q

Min. temp. FLEX

A

Flat rating temp or OAT

83
Q

Reduced Thrust Takeoff use on contaminated runways

A

Not Permitted

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