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3. FCOM - QRH > Limitations > Flashcards

Limitations Flashcards

1
Q

Flight Manoeuvring Load Acceleration Limits Clean:Slaps & flats extended:Slats extended ONLY:

A

Clean: -1g to +2.5g

Slaps & flats extended: 0g to +2g

Slats extended ONLY: 0g to +2g

FCOM - LIM - 10 - General

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2
Q

Weight Limitations: !! A320 !!(highest available option)

Maximum taxi weight (highest option available):

Maximum take off weight (breaks release, highest)

Maximum landing weight:

Maximum zero fuel weight:

Minimum weight:

A

FOR A320!!

Highest available option

Maximum taxi weight: 77,400 / 73,900

Maximum take off weigh: 77,000 / 73,500

Maximum landing weight: 66,000

Maximum zero fuel weight: 62,500

Minimum weight: 37,230

FCOM - Lim - 11 - Weight & CG

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3
Q

Weight Limitations: !! A319 !!(highest / lowest available )Maximum taxi weight: highest / lowestMaximum take off weight (breaks release) highest / lowestMaximum landing weight:Maximum zero fuel weight:Minimum weight:

A
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4
Q

Coldest acceptable

OUTSIDE AIR TEMPERATURE at FL399

A

-70

FCOM - Lim 12

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5
Q

Maximum allowable runway slope (mean)

A
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6
Q

Max runway altitude

A

9,200ft

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7
Q

Nominal runway width

A
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8
Q
A

38kt (gusts included)

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9
Q

Max tailwind

A

10kts

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10
Q

Max wind for passenger door operation

A

65kts

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11
Q

Max wind for cargo door operation

A

40kts OR 50kts if:

1) Nose into wind OR
2) Cargo door on LEEWARD side

Should be closed by 65

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11
Q

What wind MUST the cargo doors be closed by?

A

65kts

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12
Q
A
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13
Q

Maximum crosswind for TAKEOFF or LANDING (gust included) for:
Slush / Dry Snow / Wet Snow (up to 3mm)

Frost / Compacted snow (temp

A

29kt

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14
Q

Maximum crosswind for TAKEOFF or LANDING (gust included) for:

Dry Snow: >3mm
Wet snow: > 3mm
Compacted snow (OAT ABOVE 15)
Slippery When Wet

A

25kts

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15
Q

Maximum crosswind for TAKEOFF or LANDING (gust included) for:

Water: >3mm up to 12.7mm (1/2”)
Slush: >3mm up to 12.7mm (1/2”)

A

20kts

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16
Q

Maximum crosswind for TAKEOFF or LANDING (gust included) for:

ICE (cold & dry)

A

15kts

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17
Q

Maximum crosswind for TAKEOFF or LANDING (gust included) for:

Damp Wet (up to 3mm)

A

38kts

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18
Q

Take off is not recommended with what runway conditions?

A
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19
Q

What is the MMO?

A
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20
Q

What is VMO between 24,600 and 0ft?

A

350kts

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21
Q

A319 VMCA at 0ft Altitude

A
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22
Q

A319 VMCG at 0ft AltitudeConf 1+F: ?Conf 2: ?COnf 3: ?

A

At 0ft altitudeAll configs: 104.5

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23
Q

A320 VMCA at 0ft altitude

A

110ts(-2000 = 112 and +2000= 108)** shark and no sharks have the same VMCA

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24
Q
A
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25
Q
A
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26
Q

Maximum Flap / Slats speeds:Conf 1: ? Conf 1 + F: ?Conf 2: ?COnf 3: ?Conf FULL: ?

A
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27
Q

How many slat positions are there?

(i.e when you move the lever, the slats move to a new position.)

A

3.

Conf 2 + 3 slats are the same.

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28
Q
A
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29
Q

What is VLE and What is the VLE speed?

A

VLE = Max speed with landing gear extended.

280ts / 0.67

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30
Q

What is ‘VLO extension’ and what is the speed?

A

VLO Extension: Max speed the landing gear can be extended 250kt

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31
Q

What is ‘VLO retraction’ and what is the speed?

A

VLO Extension:

Max speed the landing gear can be retracted is 220kts

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32
Q

Maximum altitude at which the gear may be extended?

A

25,000ft

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33
Q

Speed at which the gear is hydraulically active?

A

260kts

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34
Q

Max wind for cargo door operation

A
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35
Q

Maximum tire speed?

A

195kts

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35
Q

Windshield wiper max speed?

A
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36
Q

Cockpit window open max speed?

A
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37
Q

A320 -

What WEIGHT should you consider for taxiing?

What speed restriction?

A

Taxi weight about 76,000kg.

Do not exceed a taxi speed of 20kts in a turn.

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38
Q

Ram air inlet pressure limitation?

A

Only open if diff. pressure

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39
Q

Air conditioning with LP ground unit?

What max airflow?

What other limitations?

A

Max airflow from ground cart of 1.2kg/s

Do not use conditioned air simultaneously from the packs and th LP ground unit (avoid chattering of non return valve)

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40
Q

APU with HP ground unit - what restrictions?

A

Do not use HP ground unit when APU supplies bleed air, to avoid bleed system damage.

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41
Q

Cabin pressurisation:Maximum positive diff pressure

A

9.0 PSI

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42
Q

Cabin pressurisation:

Maximum negative diff pressure

A

-1psi

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43
Q

Cabin pressurisation:

What is the safety Relief Valve setting?

A

8.6 PSI

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44
Q

Cabin altitude warning - what height?

A
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45
Q

Maximum cab altitude selection?

Minimum cabin altitude selection?

A

14,000ft and -2000ft

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46
Q

Max diff pressure and safety valve tolerance?

A

+/- 7hpa or 0.1 PSI

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47
Q

Avionics ventilation:During ground operations, limit the aircraft power supply with avionics ventilation system in the normal configurations follows:OAT = 49 = ?OAT = 55 = ?OAT = 60 = ?OAT = 64 = ?

A

OAT = 49 = No limitOAT = 55 = 2 hoursOAT = 60 = 1 hourOAT = 64 = 1/2 hour

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48
Q

Minimum height for use of autopilot on takeoff with SRS mode?

A
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49
Q

Minimum height for use of the autopilot in:

* Straight in , non precision approach = *

Circling approach =

ILS approach (Cat 1 ) =

PAR approach =

Go around (AP / FD engagement) =

All other phases =

Use of AP / FD in OPEN DES / DES mode not permitted in approach, unless:??

A

* Straight in , non precision approach = minima*

Circling approach = minima - 100ft

ILS approach (Cat 1 ) = 160ft AGL

PAR approach = 250ft AGL

Go around (AP / FD engagement) = 100ft AGL

All other phases = 500ft AGL

Use of AP / FD in OPEN DES / DES mode not permitted in approach, unless: Altitude is set to / above MDA or 500ft whichever is highest

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50
Q

Non precision approaches with engine out:DOES THE FOLLWING APPLY TO:1) A319?2) A3203) BothIf one engine is INOP, it is not permitted to use the autopilot to perform NPAs in the following modes: FINAL APP, NAV / v/s and nav / fpa. Only FD use is permitted.

A

1) A319 only.It is no longer applicable to ANY A320.

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51
Q

ILS Cat II Minimum decision height:

A

100ft AGL

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52
Q

ILS Cat II

How many Autopilots required?

A

At least ONE must be engaged in approach mode and Cat 3 single / dual must be displayed on FMAs.

(A/THR must be used selected or managed mode)

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53
Q

ILS Cat III Fail Passive (single)Minimum decision height?

A

50ft

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54
Q

ILS Cat III Fail Passive (single)

How many autopilots required?

A

At least ONE must be engaged in approach mode and Cat 3 single / dual must be displayed on FMAs.

(A/THR must be used selected or managed mode)

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55
Q

ILS Cat III Fail Operational (Dual)

What is the ALERT height?

A

100ft

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56
Q

ILS Cat III Fail Operational (Dual)

Cat III with DH = what is the minimum decision height?

A

20ft

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57
Q

ILS Cat III Fail Operational (Dual)

How many autopilots required with DH and Without?

A

2 Autopilots must be engaged in APPR mode and CAT 3 DUAL must be displayed.

A/THR must be used in selected or managed mode.

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58
Q

Cat III without DH

What is the minimum RVR?

A

75m

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59
Q

Engine out AUTOMATIC landing.

What flap setting is allowable for

a) A319
b) A320?

A

a) A319 can be automatically landed, single engine, with Flaps 3 or Flaps Fullb) A320 can only be automatically landed, single engine, in flaps Full.

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60
Q

What are the automatic landing / rollout wind limits for A320 Sharklets?

Headwind:

Tailwind:

Crosswind:

A

Headwind: 30

Crosswind (without rollout): 20

Crosswind (with rollout): 15

Tailwind: 10

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61
Q

Automatic landing limitations:Slope angle = Maximum Airport elevation = Maximum weight = A319 exception = Minimum elevation? =Sharklet exception = Roll out RWY conditions =

A
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62
Q

ILS Auto Landing in CAT 1 or better Auto landing in CAT 1 or better weather is possible on cat 1 ground installations or when ILS sensitive areas are not protected under which precautions?

A
  • Airline has checked that ILS beam quality and the effect of terrain profile before the runway has no adverse affect on AP / FD guidance. (in part. terrain within 300m must be evaluated)
  • Crew is aware that LOC / GS beam fluctuations may occur. PF read to immediately disco. AP and take appropriate action.
  • At least CAT 2 capability on FMA and Cat II / III procedures applied
  • Visual references are obtained at an altitude appropriate to the performed cat 1 approach, otherwise a go around must be flown.
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63
Q

ELECTRICAL

What is the max continuous load per generator?

A

100% (90 kva)

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64
Q

ELECTRICAL

Max cont. load per TR

A

200A

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65
Q

FLAPS & SLATSMaximum altitude with F&S extended

A

20,000ft

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66
Q

FUEL (NON shark)

Maximum imbalance allowed

INNER when heavier tank fuel quantity is:

FULL = 4300kg= 2250kg = 1500kg = OUTER: =

Special notes & exceptions =

A

NON SHARK INNER when:

FULL = 1500kg 4300kg= 1600kg2250kg = 2250kg 1500kg = NO LIMIT BELOW 2250kg quantityOUTER: = 690kg

****Special notes = ****

= Max imbalance (one fuel / one empty) allowed provided:1) Fuel content on one side (outer + inner) is equal to fuel content of other side (outer + inner)OR2) On the side of the lighter outer tank, the inner tank fuel quantity is higher than the opposite inner tank quantity. (up to a maximum of 3000kg higher)ANDIn exceptional circumstances (fuel system failures) the above-mentioned max fuel imbalance values may be exceed without sig. affecting aircraft handling qualities. The a/c remains fully controllable in all phases of flight?

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67
Q

FUEL (SHARKY AIRCRAFT)Maximum imbalance allowedTAKE OFF:INNER when heavier tank fuel quantity is:FULL = 3000kg= 1450kg = OUTER: = IN FLIGHT and LANDING:INNER when heavier tank fuel quantity is:FULL = 4300kg= 2250kg = 1500kg = OUTER: = Special notes & exceptions =

A
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68
Q

Is there a difference in FUEL IMBALANCE figures between SHARK and NON SHARK aircraft?

A

Yes. The shark let aircraft have a much more restrictive imbalance range for TAKEOFF.The rest remain the same.

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69
Q

Minimum FUEL temperature for JET A1

A

-43

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70
Q

Maximum fuel temperature for Jet A1

A

54

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71
Q

Minimum fuel quantity for take off

A

1500kg and wing low level warning must not be displayed on ECAM

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72
Q

Are there restrictions on centre tank fuel for take off?

A
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73
Q

For fuel, which tank must be emptied first?

A

The centre tank, followed by the wing tanks.

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74
Q

Can fuel types be mixed?

A

Yes, various types of fuel can be mixed in all proportions and the freezing point varies based on non-linear laws.

This is FCOM guidance only, maybe not OMA.

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75
Q

HYDRAULIC What is the normal operating pressure?

A

3000 PSI +/- 200

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76
Q

Maximum brake temperature for take off?

A

300

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77
Q

Is the brake system designed to hold the aircraft in a stationary position with a high thrust setting?

A
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78
Q

Taxi with deflated tiresWhat are the two limitations?

A
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79
Q

Nose Wheel Steering Handwheels MAX:

Towing and pus back max:

Towbarless towing max:

A

Handhweels: 75

Towing and push: 95

Towbarless: 85

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80
Q

Inertial Reference System:

1) Demonstrated between: ?
2) If all ADIRUs have the same magnetic variation table:

FLIGHTS USING NAV MODE PROHIBITED BETWEEN:

a) ?

B) ?

3) If ONE ADIRU has a different magnetic variation table:

FLIGHTS USE NAV MOVE PROHIBITED BETWEEN:a) b)c)

A

Inertial Reference System:1) Demonstrated between: 73N and 73S2) If all ADIRUs have the same magnetic variation table:FLIGHTS USING NAV MODE PROHIBITED BETWEEN:a) North of 73 NB) South of 60s3) If ONE ADIRU has a different magnetic variation table:FLIGHTS USE NAV MOVE PROHIBITED BETWEEN:a) North of 60N, between 30 W and 160 W ANDb) North of 73 N andc) South of 55 S

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81
Q

When should EGPWS enhanced function be inhibited ?

(TERR PB to OFF, on the GPWS panel)

A

When the aircraft is less than 15nm from the airfield AND1) Operations to / from runways not in the EGPWS database2) For specific approach procedures, which have previously been identified as pot. producing false terrain alerts

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82
Q

When must the ISIS bug functions NOT be used?

A

If both PFDs are lost

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83
Q

Minimum O2 bottle pressure takes in account:

A
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84
Q

APU: Low Oil level ecamWhat is the implication?

A

If no leak, APU may be started and maint. action required within next 10hr of APU operation

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85
Q

APU starter cycles - limit?

A
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86
Q

Maximum APU N speed (as shown on ecam)

What N does the APU auto shut down?

A

ECAM: 107% (actual = 106%)

(APU auto shuts down at 107% N, that appears on ecam)

(This corresponds to an actual N speed of 106%)

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87
Q

Maximum APU EGT?

A

Max EGT = 675Max for start

(35,000ft) = 1120

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88
Q

Within the APU start envelope, within how many attempts is the APU ‘guaranteed’ to start?

A

3 conservative start attempts

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89
Q

On BATTERY, what is the limit for APU start?

A

25.000ft. (emer elec config)

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90
Q

APU:

Below WHICH altitude and temperature can we expect full APU electrical output?

A

Below 25,000ft and below ISA + 35

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91
Q

Below which altitude can we use the APU to start an engine?

A

20.000ft.

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92
Q

Up to which altitude we use the APU to supply both packs?

93
Q

Below which altitude, can we use one pack from the APU?

94
Q

Can we use WAI with the APU bleed?

95
Q

ENGINE:

Take off and go around MAX EGT and TIME?

A

Max EGT: 950

5 min dual engine

10 min single engine

96
Q

ENGINE

Maximum time for MCT

Max EGT

A

No time limit

915 Celsius

97
Q

Engine start MAX EGT?

98
Q

Engine OIL:

Max continuous temperature?

Can we accept a transient temperature and if yes, how long?

A

Max continuous: 140

Max transient: 155

15 minutes

99
Q

Minimum ENGINE oil temperature for:Start:Take off:

A

Start: -40Take off: -10

100
Q

Minimum ENGINE oil quantity:

A

OMB

9.5qts + 0.5 / hour

101
Q

Max ENGINE n1 and n2

A

N1 = 104%

N2 = 105%

102
Q

Engine start cycle restrictions:

A
  • 4 consec cycles (max 2 mins each)
  • 20 second pause between attempts
  • after 4 attempts, 15 min cooling
  • No running engagement of the starter, when N2 > 20%
103
Q

What are the 5 restrictions for Reduced Thrust Takeoff?

A
  • Only permitted if airplane meets all app. perf requirements at planned take off weight,
  • Thrust reduced must not exceed 25% of full rated TO thrust. To meet this required, the flex temp must not be higher than ISA +53 (T MAX FLEX)
  • Assumed temp, must not be lower than flat rating temperature (or current OAT)
  • Not allowed on contaminated runways
  • Take off at reduced thrust is permitted for any inop item affecting perf, ONLY if the associated perf shortfall has been applied.
104
Q

Reduced Thrust Takeoff: A319What are the 5 restrictions?

105
Q

What is the T MAX FLEX for A319 and A320?

A

A319: ISA +60 (T MAX FLEX)

A320: ISA + 53

106
Q

Autoland limits for A319 (2 eng)

A

20 / 20 / 5

107
Q

Autoland limits for A319 (1 eng)

A

15 / 10 / 5

108
Q

Autoland limits for A320 (SH) with and without roll out

A

30/ 20 / 10 without rollout

30 / 15 / 10 with rollout

109
Q

Autoland limits for A320 (NO SH)

110
Q

Maximum levels of contamination for take off

A
  • 12.7mm of standing water (20 kt)
  • 12.7mm slush (20kt)
  • 25mm wet snow (25k)
  • 100m dry snow (25kt)
111
Q

%N for amber font

112
Q

%N for auto shutdown

A

107% or greater

113
Q

EGT for amber font

A

within 33C of current max EGT

114
Q

EGT for auto shutdown

A

computer calculated

115
Q

%N for AVAIL

A

99.5% or 95% for > 2 seconds

116
Q

Min batt voltage to start

A

25.5V, if less charge for 20 mins

117
Q

When can you press APU START?

A

5 seconds after MASTER SW has been depressed and no LOW OIL LEVEL advisory

118
Q

Max START EGT?

119
Q

Max operating EGT?

120
Q

When can you NOT check for the LOW OIL LEVEL during APU start?

A

Battery starts

121
Q

After turning batteries to AUTO how much time do you have to start the APU?

A

30 minutes

122
Q

After the batteries have been on for 35 minutes how much batt capacity is remaining?

123
Q

Approx how long until APU available after start is engaged?

124
Q

After AVAIL extinguishes during shutdown, how long do you leave batteries on for?

125
Q

Max service ceiling

126
Q

Max altitude to start on batteries only

127
Q

Max altitude to power one AC pack

128
Q

Max altitude to power two AC packs

129
Q

APU starter limit

A

After 3 consec starts attempts allow 60 minutes for cool down

130
Q

Max alt to start engines

131
Q

Max alt for APU anti-ice

A

TRICK, you can’t use APU for anti-ice

132
Q

What is the cooling period for emergency shutdown?

133
Q

NAV mode may be used in the terminal area, provided:

A
  • GPS PRIMARY
    or
  • The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed
    or
  • FMS navigation is cross-checked with NAVAID raw data
134
Q

Runway Slope (mean)

135
Q

Max crosswind for start

136
Q

Max operating altitude with slats and/or flaps extended is

137
Q

Minimum Height For Use Of Autopilot
Take off with SRS

A

100 ft AGL.
Note: Takeoff with SRS mode - An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff.

138
Q

Minimum Height For Use Of Autopilot

ILS approach when CAT 2 or CAT 3 is not displayed on the FMA

A

160 ft AGL

139
Q

Minimum Height For Use Of Autopilot

Straight-in non-precision approach

A

Applicable Minimum

140
Q

Maximum wind for passenger door operation

141
Q

Takeoff and GA (TOGA and FLEX)
Thrust Setting/EGT Limits

A

Takeoff and GA (TOGA and FLEX)
319 and 320 / 321 / NEO

635 °C / 650 °C / 1,083°C

5 min (10 min engine failure.)

142
Q

Maximum brake temperature for takeoff (brake fans (if installed) off)

143
Q

RunwayAltitude

144
Q

NominalRunwayWidth

A

45m(148ft)

145
Q

VLE

A

280kts (M .67)

146
Q

Oil Temperature (CEO)

A

Starting
-40 °C

Above Idle
-10°C

147
Q

APU Starter

A

After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.

148
Q

Minimum Height For Use Of Autopilot

UseoftheAPorFDinOPENDESor DES mode is not permitted in approach, unless the FCU altitude is set at or above:

A

Highest of:
Minimums or 500 ft (A319/A320) Minimum or 900 ft (A321)

149
Q

Fuel Temp

A

For JET A only, if TAT reaches -34C , monitor on FUEL SD page that fuel temperature remains higher than -36C

150
Q

Reverser Limits

A

Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.

151
Q

VLO (extension)

A

250kts (M .60)

152
Q

Cabin Pressure
• Maxpositivedifferentialpressure
• Maxnegativedifferentialpressure

A
  1. 0psi
    - 1.0psi
153
Q

Max Landing (320)

154
Q

Max Landing (657-687)

155
Q

MCT
Thrust Setting/EGT Limits

A

MCT
CEO / NEO

610 °C / 1,043°C

156
Q

Max Taxi speed (A320CEO)

A

When the taxi weight is higher than 67,550lbs (76,000kg): Caution: Do not exceed a taxi speed of 20 kt during a turn.

157
Q

Non-Precision Approaches with Engine-Out (319 and 657-668, 670, 671)

A

If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes:
FINAL APP
NAV V/S
NAV/FPA.
Only FD use is permitted.

158
Q

Minimum Height For Use Of Autopilot

Circling Approach

A

100 feet below Applicable Circling Minimums

159
Q

Max Landing (502-536)

A

137,788 lb

160
Q

Minimum Oil Pressure (901-905)

161
Q

Max Alt for landing gear extended

162
Q

VLO (retraction)

A

220kts (M .54)

163
Q

Fuel Imbalance, Inner tanks when one is full

A

TO / Flight&Landing
319 and 320s: (At TO / Flight and Landing)
1,102 / 3306

321:
882 / 2910

164
Q

Minimum Height For Use Of Autopilot

All other phases

A

500 ft AGL (A319/A320) 900 ft AGL (A321)

165
Q

Maximum Certified Altitude

166
Q

Max speed for Windshield Wipers

167
Q

STARTING (On Ground and Inflight)
Thrust Setting/EGT Limits

A

STARTING
CEO / NEO

635 °C / 1,083°C

168
Q

Wingspans

A

Non-Sharklet
111feet,10inches

Sharklet
117feet,5inches

169
Q

Maximum demonstrated crosswind

A

38kts (gust included)

170
Q

Reduced Thrust Takeoff Limits

A

FLEX takeoff is not permitted on contaminated runways

171
Q

Max crosswind with CAT II and III

A

Crosswind: 15 kts

172
Q

Max tire speed

173
Q

APU With HP Ground Unit

A

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.

174
Q

Starter Limitations

A

ALL CEO / NEO:

One Cycle = 1 / 2 consecutive start attempts

(CEO)Man start, 2 mins max start / 5 mins crack

For Ground Starts (auto or man), between cycle pause: 15 s / 35 s

After 3 cycles or 5 / 15 min continuous cranking (or cumulated NEO)
Cooling Period = 30 min / 15 min

Do not start, when
N2 is above 10% GND, 18 % FLT / 20%

175
Q

Tailstrike Pitch Attitudes

A

L/G Struts Compressed
319 - 13.9 degrees
320 - 11.7 degrees
321 - 9.7 degrees

176
Q

Max tailwind for:
Takeoff
Landing

A

Takeoff - 15kts
Landing - 10kts

177
Q

APU Bleed use with Air Start Unit

A

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.

178
Q

Packs use with the LP Air Conditioning Unit

A

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning system.

179
Q

What is the reduced usable fuel capacity of the Center Tank on 697 and 698 (Invicta-FRS system)

A

reduced usable capacity of up to 42.9 gallons

180
Q

ELAC Functions

A

Normal Elevators
Normal Ailerons
Normal Pitch and Roll

Alternate Pitch

Direct Pitch and Roll

Abnormal Attitude
Aileron Droop
Autopilot orders

181
Q

SEC Functions

A

Normal Roll

Alternate Pitch

Direct Pitch and Roll

Abnormal Attitude
Speed Brakes

182
Q

FAC Functions

A

Rudder Limitations
Turn Coordination
Rudder Dampening
Rudder Trim

Aircraft envelope

Windshear

Low Energy Warning

183
Q

NAV mode may be used in the terminal area, provided:

A
  • GPS PRIMARY
    or
  • The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed
    or
  • FMS navigation is cross-checked with NAVAID raw data
184
Q

Runway Slope (mean)

185
Q

Max crosswind for start

186
Q

Max operating altitude with slats and/or flaps extended is

187
Q

Minimum Height For Use Of Autopilot
Take off with SRS

A

100 ft AGL.
Note: Takeoff with SRS mode - An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff.

188
Q

Minimum Height For Use Of Autopilot

ILS approach when CAT 2 or CAT 3 is not displayed on the FMA

A

160 ft AGL

189
Q

Minimum Height For Use Of Autopilot

Straight-in non-precision approach

A

Applicable Minimum

190
Q

Maximum wind for passenger door operation

191
Q

Takeoff and GA (TOGA and FLEX)
Thrust Setting/EGT Limits

A

Takeoff and GA (TOGA and FLEX)
319 and 320 / 321 / NEO

635 °C / 650 °C / 1,083°C

5 min (10 min engine failure.)

192
Q

Maximum brake temperature for takeoff (brake fans (if installed) off)

193
Q

RunwayAltitude

194
Q

NominalRunwayWidth

A

45m(148ft)

195
Q

VLE

A

280kts (M .67)

196
Q

Oil Temperature (CEO)

A

Starting
-40 °C

Above Idle
-10°C

197
Q

APU Starter

A

After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.

198
Q

Minimum Height For Use Of Autopilot

UseoftheAPorFDinOPENDESor DES mode is not permitted in approach, unless the FCU altitude is set at or above:

A

Highest of:
Minimums or 500 ft (A319/A320) Minimum or 900 ft (A321)

199
Q

Fuel Temp

A

For JET A only, if TAT reaches -34C , monitor on FUEL SD page that fuel temperature remains higher than -36C

200
Q

Reverser Limits

A

Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.

201
Q

VLO (extension)

A

250kts (M .60)

202
Q

Cabin Pressure
• Maxpositivedifferentialpressure
• Maxnegativedifferentialpressure

A
  1. 0psi
    - 1.0psi
203
Q

Max Landing (320)

204
Q

Max Landing (657-687)

205
Q

MCT
Thrust Setting/EGT Limits

A

MCT
CEO / NEO

610 °C / 1,043°C

206
Q

Max Taxi speed (A320CEO)

A

When the taxi weight is higher than 67,550lbs (76,000kg): Caution: Do not exceed a taxi speed of 20 kt during a turn.

207
Q

Non-Precision Approaches with Engine-Out (319 and 657-668, 670, 671)

A

If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes:
FINAL APP
NAV V/S
NAV/FPA.
Only FD use is permitted.

208
Q

Minimum Height For Use Of Autopilot

Circling Approach

A

100 feet below Applicable Circling Minimums

209
Q

Max Landing (502-536)

A

137,788 lb

210
Q

Minimum Oil Pressure (901-905)

211
Q

Max Alt for landing gear extended

212
Q

VLO (retraction)

A

220kts (M .54)

213
Q

Fuel Imbalance, Inner tanks when one is full

A

TO / Flight&Landing
319 and 320s: (At TO / Flight and Landing)
1,102 / 3306

321:
882 / 2910

214
Q

Minimum Height For Use Of Autopilot

All other phases

A

500 ft AGL (A319/A320) 900 ft AGL (A321)

215
Q

Maximum Certified Altitude

216
Q

Max speed for Windshield Wipers

217
Q

STARTING (On Ground and Inflight)
Thrust Setting/EGT Limits

A

STARTING
CEO / NEO

635 °C / 1,083°C

218
Q

Wingspans

A

Non-Sharklet
111feet,10inches

Sharklet
117feet,5inches

219
Q

Maximum demonstrated crosswind

A

38kts (gust included)

220
Q

Reduced Thrust Takeoff Limits

A

FLEX takeoff is not permitted on contaminated runways

221
Q

Max crosswind with CAT II and III

A

Crosswind: 15 kts

222
Q

Max tire speed

223
Q

APU With HP Ground Unit

A

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.

224
Q

Starter Limitations

A

ALL CEO / NEO:

One Cycle = 1 / 2 consecutive start attempts

(CEO)Man start, 2 mins max start / 5 mins crack

For Ground Starts (auto or man), between cycle pause: 15 s / 35 s

After 3 cycles or 5 / 15 min continuous cranking (or cumulated NEO)
Cooling Period = 30 min / 15 min

Do not start, when
N2 is above 10% GND, 18 % FLT / 20%

225
Q

Tailstrike Pitch Attitudes

A

L/G Struts Compressed
319 - 13.9 degrees
320 - 11.7 degrees
321 - 9.7 degrees

226
Q

Max tailwind for:
Takeoff
Landing

A

Takeoff - 15kts
Landing - 10kts

227
Q

APU Bleed use with Air Start Unit

A

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.

228
Q

Packs use with the LP Air Conditioning Unit

A

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning system.

229
Q

What is the reduced usable fuel capacity of the Center Tank on 697 and 698 (Invicta-FRS system)

A

reduced usable capacity of up to 42.9 gallons

230
Q

ELAC Functions

A

Normal Elevators
Normal Ailerons
Normal Pitch and Roll

Alternate Pitch

Direct Pitch and Roll

Abnormal Attitude
Aileron Droop
Autopilot orders

231
Q

SEC Functions

A

Normal Roll

Alternate Pitch

Direct Pitch and Roll

Abnormal Attitude
Speed Brakes

232
Q

FAC Functions

A

Rudder Limitations
Turn Coordination
Rudder Dampening
Rudder Trim

Aircraft envelope

Windshear

Low Energy Warning

3. FCOM - QRH (6 decks)

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