Limitation Flashcards

1
Q

Max discrepancy Altimeters ( RVSM operation )

A

Between ADRs -> 20’

Between ADR and ISIS -> 30’

Check that the difference between each altitude indication (in the QNH reference) and the airport elevation is less than 75 ft

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2
Q

Welcome PA, Who and when?

A

Between 15-10 min before P/B, no need all pax on board

Coordinate with the Purser

He can delegate to another FC

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3
Q

Vmo reduces every 1000 feet and green dot

A
  • 7, the green dot doesn’t move much
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4
Q

Max temp

A

55

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5
Q

Land gear down or operation. Alt and speed

A

250 knots, M.55. 21,000. In Emergency you can disregard the altitude but never speed

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6
Q

Runway slope Max

A

+/- 2%

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7
Q

Max wind crossing. T/O and land.

And in case of Wx deterioration

A

Dry, Wet, Slush, Snow (until 3mm)

35 TO

40 landing

+3mm of Snow, Slush or Standing Water, or Slippery when Wet -> TO and Land -> 20knts

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8
Q

Tailwind for take and landing

A

15 knots.

EA if +10 knts only Flaps FULL to Land

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9
Q

Max crosswind when Slippery when wet,
Snow, water, slush +3mm

A

20 knots

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10
Q

Max speeds

A

340

M 0.89

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11
Q

Max design maneuvering speed Va

A

280

M 0.82

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12
Q

VMCL and VMCL2

A

120

145

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13
Q

Max speed for landing gear gravity extension

A

220

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14
Q

Max ground speed ( Max tire speed )

A

204

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15
Q

Max opening speed cockpit window

A

And Paks Off

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16
Q

Max closing speed cockpit window

A

160 knts

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17
Q

Max wipers speed

A

250

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18
Q

Normal cabin altitud

A

7,500

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19
Q

Min height for use autopilot

A

Take off 100’ or 5” after Liftoff or GA

Non precision or circling 200

ILS with APPR1 160

All other phases 500

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20
Q

Which app we can do Automatic app or Landing

A

GLS CAT I

ILS CAT II

ILS CAT III

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21
Q

Automatic app or automatic landing wind limitation

A

38 headwind

30 crosswind

15 tailwind

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22
Q

Auto land n-2 can we do?

Which condition?

A

only engines failure opposite side

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23
Q

Max imbalance tanks

A

Inner and feed 3,000
Middle 2,500
Outer 1,200

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24
Q

Jet A, Jet A1

A

Jet A -> 40

Jet A1 -> 47 And has to be 90% Jet A1

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25
Q

Deflected tire lim for taxi speed and angle of turn

A

3 knts

30 degrees

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26
Q

Brake temperature decrease by itself

A

2 degrees per min.

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27
Q

G/A min gradients APP and Land. And EOP climb gradient not depicted in the charts.

A

App (n-1)= 2,7%

Land (tren abajo)= 3,2%

EOP not depicted = 3,3%

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28
Q

Fuel consumption APU

A

600 kg/ 1 hour

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29
Q

When fill up trim tank?

A

Above 47 tones

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30
Q

Min Cabin Oxigen pressure for Dispatch

A

Himalaya 1650 or 1750

Other routes 1300

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31
Q

APU Starts lim start attempts and cooling period?

A

3 attempts of 60 seconds interval. After that wait 60 min

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32
Q

APU Max speed and altitude ( Start and Operation)

A

M 0.56 or 250 knts, except of all engine failure

Start APU -> FL 200

Operation-> 22.500’

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33
Q

Max altitud APU bleed air and electrical power

A

22,500

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34
Q

APU Bleed cannot use with?

A

Wing anti ice

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35
Q

No soft GA if?

A

Miss app gradien is more than 8%

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36
Q

Name Policy: Fuel policy apply once the released of the Fuel bowser

A

In-Flight Fuel Management

Continue towards the destination

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37
Q

When continue the flight towards the destination?

A

A) Expected Approach Time (EAT) not known:

If it is possible to reach at least 2 aerodromes at which a landing is assured with at least final reserve fuel remaining at touchdown, or

2 separate and independent runways at a single aerodrome within 2 hours of flying time, taking into account ATC delay.

B) EAT known:

Regardless of the number of runways, the flight may continue towards the destination aerodrome or hold, as long as landing is assured with at least final reserve fuel remaining at touchdown.

A landing is considered to be assured as long as, in the judgement of the Commander, the approach and landing could be completed in the event of any forecast deterioration in the weather and plausible single failures of ground or airborne facilities.

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38
Q

Landing is assured if:

A

It could be completed in the event of any:

FORECAST DETERIORATION in the weather and

PLAUSIBLE SINGLE failures of ground or airborne facilities.

Forecasts should be used to assess the probability of landing success when more than two hours from the relevant aerodrome.
Within two hours, actual weather reports and trend information may be used.

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39
Q

Mínimum Fuel

A

The Pilot-in-Command shall advise ATC when,

Having committed to land at a specific aerodrome,

Pilot calculates that any change to the EXISTING clearance to that aerodrome may result in landing with less than the planned final reserve fuel.

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40
Q

MAYDAY MAYDAY MAYDAY FUEL

A

When the Calculated USABLE fuel predicted to be available upon landing at the NEAREST aerodrome WHERE a SAFE landing can be made is less than the planned final reserve fuel.

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41
Q

When we will have Low Fuel Feed tanks?

A

Around 5,500 kg.

Each tanks Right 1+2 or Left 3+4 -> is below 1375 kg

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42
Q

Screen on the very right, name?

And the name of the system?

Divided into?

A

OIT: On board Information Terminal.

OÍS: On board Information System

Dividen into:
NSS Avionics and
FLT OPS

Displayed by the OIT (On board Information Terminal)

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43
Q

ADIRS acronym

A

ADIRS: Air Data Inertial Reference System

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44
Q

Max altitud with tailstrike

A

FL100

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45
Q

Name of the control to taxi the plane

A

Tiller, la r no se pronuncia

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46
Q

Reset spa or comunications

A

CIDS: Csbin Intercomunication Data System

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47
Q

ND display airport. Acronym?

A

OANS

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48
Q

Cabin altitud Rate?
of climb and descent?

A

Climb 1000

Descent 300

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49
Q

Sterile flight deck when? And meaning?

A

Close doors until passing 10,000

Passing 25,000’ until first door is opened

1000 to go

Essential duties required for a safe operation

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50
Q

No contact period

A

Take off until l/g retracts

Arrival: extension l/g until vacate the rwy

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51
Q

When u are lost during taxi. What can u do?

A

Req Progressive taxi Instructions

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52
Q

PA for cabin crew to be ready, in case of Abnormal situation

A

This is the captain, attention cabin crew at Stations

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53
Q

Policy- Cabin crew Start the Service ( During climb) when and how?

A

When?
The flaps have been fully retracted,
The aeroplane has reached an altitude of 5,000 feet AAL or above, and
The turbulence is expected to be none or light.

How?
Extinguishing the seatbelt sign,
Cycling the seatbelt sign,
Calling the Purser via the interphone, or
Announcing “Cabin Crew cleared for duties” via the PA.

54
Q

When PA arrival?

When briefing?

A

PA
- 20 min to top
- Not possible then ask purser to make a pax comfort PA and PF finalize when he is ready

Briefing between 20 and top

55
Q

Rate Max of descents

A

+ 5000 ——— 5000
5000-3000—-3000
3000-1000—-2000
Below————1000

These values can be exceeded but only momentary

56
Q

Priority App

A

Priority 1:
Precision Approach
Approach Procedure with Vertical Guidance (APV) to the runway threshold
Visual Approach with vertical guidance to the runway threshold.

Priority 2
Non-precision Approach (without vertical guidance to the runway threshold)

Priority 3
Circling Approach (enhanced coded approach procedure)

Priority 4
Visual Approach (without vertical guidance to the runway threshold)

Circling app not authorized during night

57
Q

Airport we don’t have charts. What can we do?

A

Visual app

58
Q

When do we need ceiling?

A

Circling and
Visual App

Only for planning the TO Alternate if the only app available is a NPA ( only for Planning)

59
Q

GLS APP. Ground facilities must be operative?

A

The associated ground station must be operative

60
Q

2 app speed techniques?

A

Decelerated app

Early stabilized app

61
Q

Holdings

Min outbound?

Time holding?

Fuel used 1 holding?

A

+14,000——— 1’30’’

Outbound 1’ -> Total Holding is 6 min ,

Outbound 1:30 -> Total Holding is 7 min

1 hold= 1 T

62
Q

How to increase the REC MAX?

A

1hour is 10.000 feet

63
Q

Min rwy and taxi ancho?

A

Rwy 45

Taxi 23

64
Q

Distance inner engines and outer?

A

Inner 30 m

Outer 51 m

65
Q

Fuel operation before and after releasing the Fuel bowser?

A

Before -> Basic Procedure or Pre-Flight Calculation Fuel

After -> In-flight Fuel Managment

66
Q

When ur OFP fuel is not enough u can req a new re clearance OFP, what is the name?

A

DPP: Decision Point Procedure

67
Q

m-CD (Mel)

A

m-CD) (m-Crew Deferral) symbol indicates the requirement for a maintenance procedure, which may be accomplished by the flight crew, provided the following conditions are observed:

The agreement by the flight crew to perform the maintenance

68
Q

Mel repetition depends on (o) or (m)

A

(o) The operational procedure must be applied, before each flight, unless a periodicity is clearly specified in the ‘REMARKS or EXCEPTI
(m) if no periodicity is defined, maintenance action is a one-time action to be accomplished before the first flight under relevant MEL item (e.g. a deactivation procedure). Otherwise, this is a repetitive action

69
Q

Separate and independent rwys

A

Separate Rwy (EASA):
Runways may overlay or cross in such a way that if one of the runways is blocked, it will not prevent the planned type of operations on the other runway.
Each runway shall have a separate approach procedure based on a separate navigation aid

Definition of Independent Runway I couldn’t find in manuals or internet. I found Independent App. As an Airmanship Separate runway definition covers all the meaning of Independent.

70
Q

OFP - When u don’t have enough fuel?

A

DPP Decision Point Procedure ( Reclearance)

71
Q

What are ur wx min to commit? It is a Technique

A

Select the best App I can do, IF:

  • Best App is CAT III or II -> take the minimum for CAT I
  • Best App is CAT I -> go for minimum for NPA
72
Q

Sector definition

A

The time between when an aeroplane first moves under its own power until it next comes to rest AFTER LANDING, on the designated parking position

I understand if u need to come back to the stand, that is not consider as a sector for FTL.

73
Q

Sector (OMA)

A

First move under its own power, until comes to rest after landing

74
Q

Missing pax

A

offloading of the checked baggage shall commence at STD-15.

75
Q

De icing time spend with 2 trucks?

A

25 min

76
Q

When it is 20 to top

A

ETA-50

77
Q

When can we start the App?

A

If the vis is less than the charts min, the flight can start the app if the capt considers there is reasonable expectations to meet the chart minima before reaching ABP Apr ban point

App Ban Point. An app cannot be continued if we reach tha ABP and the vis is lower than the applicable minimum

App Ban Point.
Cat I ———— outer marker or 1000
For circling ——Initial App Fix
CAT II/ III——— it is in LIDO

Note: for Circling and Visual — you need ceiling and visibility to start

78
Q

Rate of Climb 8%. How much is Vertical Speed?

A

Speed x Rate

Speed 210 -> 210x8 = 1700’/min

79
Q

Lights
Cockpit prep
Clear to line up
Clear to TO

A

Cockpit Prep -> AUTO (STROBE)————- AUTO or OFF (during day time)

Clear to Line up -> STROBE

Clear to TO -> Landing Lights and Nose TO

80
Q

What is the name of the short briefing before TO.

A

Departing Briefing Confirmation

81
Q

What are the names of External,

air to cool the plane from the ground

and air to start the engine?

A

Ground Power Unit

Air Conditioning Unit

Air-Starter Unit

82
Q

The FLD of the Basic autobrake may exceed the LDA?

A

As long as all of the following conditions are satisfied:

The RWYCC is 5 or 6

The LD with basic autobrake is less than the LDA

The FLD with maximum manual braking is less than the LDA.

83
Q

Wet Runway vs Reverse

A

When the runway is wet or contaminated, Airbus recommends the use of maximum reverse thrust.

The flight crew may use idle reverse in wet conditions when

LDA should therefore exceed the factored LD without reverse for the braking action corresponding to standing water (RWYCC 2, Braking Action Medium to Poor).

84
Q

Name of MEL Tree?

A

MEL-Preamble- Failures Prior to TO

85
Q

Best rate of climb - Best angle of Climb.
Climb FL 300 by Purpa or
Expedite until passing FL300

A

Climb FL 300 by Purpa -> Best angle of Climb -> Green Dot

Expedite until passing FL300 -> Besr Rate of Climb -> in the middle between ECON speed and Green dot

86
Q

What is the names of the Alternate Airports in the OFP?

A

Alternative Priority Listing

87
Q

Max Thrust during taxi

A

15%.

It is not a limitation, appears on the FCTM as a recommendation

People write a ASR when they use more than 15%

88
Q

Min Cabin Oxygen - Normal routes and Himalayan

A

Routes which Depressurization Strategies have been published in the OFP -> Half square ambar-> check FCOM limitations

Himalayas:

2 classes -> 1750 PSI
3 classes -> 1650 PSI

89
Q

TOPA remove Air Conditioner

How much more kilos can you take more?

A

8 Tonnes

90
Q

RWYCC

A

Runway Condition Code

91
Q

Plane and cabin book, nickname

A

Tech log

Cabinlog

92
Q

5G in USA

A

If plane no Upgrade + Reduce visibility destination -> Contact Dispatcher

Flight to USA + Plane no Upgrade 5G + NOTAM in USA of 5G -> CAT I

93
Q

Min taxiway

Min Runway Width

Min Runway for 180

Distance between Landing gear

Distance between Engines

A

Min Taxiway -> 23 m

Min Width Runway -> 45 m

Runway + shoulders -> 58 m

Landing Gear -> 15 m
Inner Engines -> 30 m
Outer Engines -> 50 m

94
Q

When to Stow the Reverse?

A

At Taxi Speed

95
Q

BTV - Dry and Wet lines - Brakes and Reverse?

A

Dry -> Full Brake + No Reverse
Wet -> Full Brake + Full Reverse

96
Q

BTV - Stop Bar

When appears?

What shows you?

A

Appears when plane is on Ground ( dissapair Dry or Wet line)

Stop Bar shows you:
When using BTV -> plane will reach 10 knts
Basic Autobrake -> plane will stop

97
Q

When BTV expects to pass the selected exit ?

A

Autobrake will change to Autobrake HI.

Triple click

FMA -> EXIT MISSED

Stop Bar will be Amber colour

98
Q

BTV - what happens when ROP predicts stop after End of Rwy?

A

Stop Bar in Red

Sound -> “MAX REVERSE” until apply max reverse

PFD -> “MAX REVERSE” until ROP detects Rwy is enough

99
Q

BTV - Turnaround Predictions

A

One with Max Reverse and other Reverse in Idle

Takes into account a fixed taxi phase

Cooling time necessary to reach 150 degrees after landing.

100
Q

How to call the escalerilla?

A

Mobile steps

101
Q

Dry and Wet lines - What altitude are changing his behavior?

A

Above 600’ -> lines no moving. Taking data from PERF Page

Below 600’ -> Lines moving. Taking Real data

102
Q

BTV - Speed at Exits

A

10 knts at 65m of the Exit

If Exit end of Rwy or Exit in the last 300 m -> target 10 knts at 300 m from the Runway End

103
Q

BTV - Turnaround Predictions

A

Takes into account a fixed taxi phase and

Cooling time necessary to reach 150 degrees after landing.

104
Q

ROW - how works and Alerts?

A

ROW
Concerns the airborne phase,
From 500ft AGL until touchdown.
Alerts the flight crew in the case of potential runway excursion at landing.
Warning
IF WET: RWY TOO SHORT -> only FMA
RWY TOO SHORT -> FMA + Voice ( voice is repeated as long as ROW detest an overrun)

105
Q

ROP - How works and Alerts?

A

ROP
Concerns the ground phase of the landing.

Alerts the flight crew in the case of potential runway excursion

Asks the flight crew to use maximum reverser thrust and automatically commands maximum braking, when an auto-brake mode is engaged.

Remains armed
Until 30kt, or
Until the aircraft vacates the runway.

106
Q

Stop Bars - What shows?

A

Appears when plane is on Ground ( dissapair Dry or Wet line)
Stop Bar shows you:
When using BTV -> plane will reach 10 knts
Basic Autobrake -> plane will stop

107
Q

STOP BAR RED

A

Appears when the Stop Bar is after end of runway

Applies Max Braking

Triple Click
Sound -> “MAX REVERSE” until apply max reverse. At 80 knts new announce “KEEP APPLYING MAX REVERSE”

PFD -> “MAX REVERSE” until ROP detects Rwy is enough

108
Q

ROW/ROP -Limitations

A

Only with Conf 3 and Full

You can use for Contaminated Runways, but it doesn’t prevent from Runway Excursion

Also with Overweight Landing

109
Q

ROW/ROP - No AutoBrake

A

Means -> Pedal Braking

FMA -> “MAX BRAKING”( as long as ROP is active) + “MAX REVERSE” ( as long as ROP is active)

Voice -> “MAX BRAKING”. When the flight crew applies maximum pedal braking, the aural alert “SET MAX REVERSE” replaces the aural alert “MAX BRAKING”.“ “SET MAX REVERSE” the voice will repeat until we apply Max Reverse. At 80 kt -> Reminder “KEEP MAX REVERSE”

110
Q

Max Fuel Discrepancy during refueling

A

1900 kilos

FOB before Refueling + Fuel Uplifted = FOB SD

111
Q

Min Oil

A

EA -> 6 + 0,4xh ( min 10 quarters)

RR
- below 0 degrees -> 6 + 0,5 (min 13 quarters)
- 0 or above -> 6 + 0,5 (min 10 quarters)

112
Q

Magnetic vs True?

A

True north is a fixed point on the globe.

Magnetic north is the direction that a compass needle points

If you read the winds -> they’re true; if you hear them -> they’re magnetic

ND
- Wind numbers -> True North
- Arrow
Plane on heading -> Magnetic North
Plane on Track. -> True North

113
Q

ENGINE ANTI-ICE - when On?

A

Icing Conditions
- When OAT is 10 degrees or Below on the ground and for takeoff, or
- TAT in flight is 10°C or below

No need:
- During climb and cruise when the SAT is below –40°C.

114
Q

When you suspect GPS Interference?

A

The POSITION / GPS page displays dashes on GPS positions, and/or

Number of tracked satellites (“NBR OF SAT”) may be lower than 5 or null

115
Q

When we set the Clock to INT, what is its capability?

A

INT mode of the clock maintains the ATC Datalink capabilities for 24 h.

The internal clock deviates from the GPS by a maximum of one second every 24 h.

To reset the drift resulting from the UTC internal time, the crew must switch the UTC selector of the clock to the GPS mode during10 s

The clock is connected to GPS 1

116
Q

When can we return the Clock to GPS?

A

1- Check that the POSITION / GPS page displays GPS1 in NAV (Green) mode and

2- At least 5 satellites tracked.

117
Q

What systems interfere with GPS interference?

A

Cruise Phase

- GPS
- Aircraft Position
- ADS-B 
- ATC Datalink
- SATCOM
- TAWS
- WXR

APP and LAND phase
- FLS
- GLS
- OANS
- ROW/ROP

118
Q

To enter in NAT you need?

A

At least two​ fully serviceable Long Range Navigation Systems (LRNSs).

A LRNS may be one​of the following:​
- one Inertial Navigation System (INS);​
- one Global Navigation Satellite System (GNSS

119
Q

UEA Airspace

A

RNAV 1 navigation specifications and GNSS

Failure before departure ( inbound DXB) -> aircraft is allowed to depart under RNAV 5

Failure airborne -> revised ​ clearance ​ shall ​ be​ obtained from the ATC. ATC may also provide the​aircraft with radar vectors until the aircraft is capable of resuming its own navigation.​

Initial ​ contact ​ on ​ an​ ​ ATC ​ -> ‘EK 321 UNABLE RNAV DUE EQUIPMENT’

120
Q

No GPS - problems

A
  • No enter UAE
  • PBCS Tracks in the NAT FL 350-390
  • Arrivals or SID that says “ GNSS REQUIRED “
  • UAE all START, SID
  • RNAV 1 (initial APP…) when we don’t have RAD NAVS to update position (min req RNAV1)
  • No RNP or RNAV
121
Q

RNP APCH what are they?

A

RNP APCH operations correspond to RNAV(GNSS) or RNAV(GPS) operations.

RNP differs from RNAV that they have a Alert and Monitoring system

Always they need GPS

122
Q

RNP APP - How can you fly them?

A

Always with GPS

  • FLS -> F-LOC F-G/S
    * with LNAV or LNAV/VNAV minimum
    * the only Capability acceptable is F-APP. If we see F-APP+RAW -> we cannot do it
  • NAV/FPA
    • LNAV minima only
    • GPS PRIMARY must be available on at least one FMS.
    • Discontinue the App:
      • GPS PRIMARY LOST
      • NAV FM/GPS POS DISAGREE
      • CrossTrack error exceeds 0.3 NM
123
Q

How much fuel burn for a GA and return?

A

2,5 tones

124
Q

Minima for visual app

A

LIDO 5 km.

125
Q

Can we taxi out with 2 engines?

A

Exceptional​ Circumstances​ would be listed in either CCI,​ or by CoNotam.​

On the day of ops, if required by ​circumstances, the crew​ should contact Management Pilot on Duty (MPOD) or Tech Pilot on Duty (TPOD) via​ VPNC​ for ​guidance​ and approval.​

126
Q

VGSI and FAPA are not coincident - what is VGSI and FAPA?

A

VGSI -> Vertical Guidance Slope Indicator

FAPA -> Final Approach Profile Angle​

127
Q

Oxygen for pilots -half frame (amber) - meaning

A

On ground only

Means -> The pressure is below the minimum necessary to dispatch the aircraft with 4 or 5 flight crewmembers.

However, the pressure may be sufficient to dispatch the aircraft with less than 4 or 5 flight crewmembers

Refer to Cockpit Oxygen Limitations.

128
Q

Contingency procedures

A

30 o más and offset 5nm. Then on the offset:

  • Descend FL290
  • Offset vertical of 500’
129
Q

Contingency Procedure of Wx

A

Deviation less than 5NM -> keep level

+5nm -> vertical offset 500’ ( rule of the rebota)

130
Q

RWYCC

A

Runway Condition Code

Dry is 6

131
Q

How many EXT power units are needed?

A

At least three EXT power units are necessary to supply the aircraft with the APU OFF

If only two EXT power units are available, it is recommended:
- To keep the APU ON or
- Reduce the load demand for a while (e.g. by setting to OFF the CAB FANS pb-sw and COOLG pb-sw )