Limitations Flashcards

1
Q

Max Altitude Flaps/Slats Extended

A

20,000ft

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2
Q

Manoeuvre Limit Load Factors

A

Slats and Flaps Retracted -1g to + 2.5g
Slats and Flaps Extebded 0g to + 2.0g

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3
Q

Icing Conditions Definition

A

TAT +10 degrees C or below with visible moisture in flight.
Same on the ground but in addition vis less than 1.6km.

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4
Q

Max Take Off Weight

A

330-200 = 230,000kg /233,000kg
330-300 = 233,000kg /242,000kg

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5
Q

Max Landing Weight

A

330-200 = 180,000kg / 182,000kg
330-300 = 186,000kg /187,000kg

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6
Q

Max Zero Fuel Weight

A

330-200 = 160,000kg / 170,000kg
330-300 = 171,000kg/175,000kg

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7
Q

C of G limits for take off

A

(Check if outside) 18-33% MAC

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8
Q

VMO/MMO

A

330kts IAS
0.86M

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9
Q

Maximum design manoeuvring speed

A

If alternate or direct law are active then full aileron or rudder application or manoeuvres close to stalling angle of attack should be confined to speeds below VA
VA =M.78 above 27000ft 252-304kts SFC-27000ft

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10
Q

VFE speeds

A

Flap1 = 240kts (Intermediate APP)
Flap 1+F =215kts (Take off)
Flap 2 = 196kts
Flap 3 = 186kts
Flap Full = 180kts

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11
Q

VLO/VLE

A

IAS 250kts/M0.55
Alternate extension = Max 200kts IAS

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12
Q

Maximum Runway Slope

A

+/- 2%

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13
Q

During Towing Nose Wheel Angle to not be exceeded

A

65 degrees
NB mechanical stop is 95 degrees

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14
Q

High Engine Vibration

A

N1>=5.7
N2>=5.6

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15
Q

High Oil Temp

A

Between 165-175 degrees for more than 15 mins or >175 degrees
Procedure involves reducing thrust and shutting down engine if problem persists.

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16
Q

Engine Low Oil Pressure

A

Alert triggers when <10PSI. Procedure involves reducing thrust and shutting down engine of problem persists.

17
Q

Minimum Oil Quantity

A

12qt + consumption (estimated at 0.56qt-0.87qt per hour)

Check this.

18
Q

ILS AR (Authorisation Required)

A

Aer lingus not cleared to conduct these kind of approaches.

19
Q

Aer Lingus not authorised to carry out RNP approaches associated with

A

Ground Based Augmented Systems
Satellite Based Augmented Systems
EGNOS European Augmented System (based off SBAS)
WAAS USA equivalent of EGNOS
LPV minima not to be used.

20
Q

Max Cross wind

A

EI DUO has a max crosswind of 45kts instead of the normal 40kts.

21
Q

Cross wind limitation

A

EIDUO has a crosswind limit of 45kts
All other aircraft are limited to the normal 40kts.

22
Q

Minimum pavement turn width

A

330-300 48m
330-200 45.2 m

23
Q

Width and dimensions

A

A330-300 and A330-200 60.3 m in width.
The 330-300 length is 63.69m and the 330-200 is 58.37m

24
Q

Number of passengers

A

330-300
317 passengers (30 business and 287 in economy.

330-200
271 passengers (24 in business and 247 in economy).

25
Q

Range

A

330-300 6350nm
330-200 7250nm
(The 330-200 has an additional centre tank of 32675kg)
Total fuel capacity is 76561kg for 330-300 and 109186kg for 330-200

26
Q

Cockpit window open speed limit

A

230kts

27
Q

Maximum tyre speed

A

204 kts

28
Q

Maximum wiper speed

A

230kts

29
Q

APU bleed with HP start unit

A

Must not use air from the APU bleed at the same time that the A/C is supplied with HP bleed air.-1

30
Q

Maximum differential pressure

A

9.25 PSI
Max -ve differential pressure -1 PSI
DUO max -ve pressure -0.73 PSI

Safety valve releases at 8.85PSI

31
Q

Engine oil quantity limitation

A

12 qts per side + consumption

Average consumption 0.56qts per hour. Up to 0.87qts per hour allowed provided route can be flown.