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A320F > Limitations > Flashcards

Limitations Flashcards

1
Q

Flight Maneuvering Load Acceleration (Clean)

A

-1G to +2.5G

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2
Q

Flight Maneuvering Load Acceleration (Slats+Flaps/Slats Only)

A

0G to 2G

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3
Q

Environmental Envelope (Maximum Operating Altitude)

A

Slats/flaps retracted: 39 800 ft
Slats and/or flaps extended: 20 000 ft

Takeoff and Landing: 9 200 ft

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4
Q

Environmental Envelope (Minimum Temperature)

A
  • 70 ºC
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5
Q

Environmental Envelope (Maximum Temperature)

A

+55 ºC

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6
Q

Runway Slope

A

+/- 2%

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7
Q

Runway Altitude

A

9200 ft

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8
Q

Nominal/Minimum Runway Width

A

Nominal: 45 m
Min: 30 m

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9
Q

Max. Crosswing Takeoff/Landing

A

38 knots demonstrated (gust included)

SFO/FO/SO<500h:
15 knots

10 knots if Ceiling < MDA+200/ RVR +400m

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10
Q

Max. Tailwind Takeoff/Landing

A

10 knots

SFO/FO/SO<500h:

5 knots (dry rwy)

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11
Q

Max. Wind Pax Door Operation

A

65 knots

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12
Q

Max. Wind Cargo Door Opening

A

40 knots (50knots if aircraft nose is into the wind or if the door is on the leeward side)

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13
Q

Max Operating Speed (VMO)

A

350 knots

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14
Q

Max Operating Mach Number (MMO)

A

Mach 0.82

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15
Q

Severe Turbulence Recommended Speed Below FL200

A

250 knots

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16
Q

Severe Turbulence Recommended Speed At or Above FL200

A

275 knots/ Mach.76

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17
Q

Flaps/Slats Configurations and Speeds ( Conf 1)

A

Slats 18º, Flaps 0º, ECAM 1, MAXIMUM SPEED 230 knots

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18
Q

Flaps/Slats Configurations and Speeds ( Conf 1+F)

A

Slats 18º, Flaps 10º, ECAM 1+F, MAXIMUM SPEED 215 knots

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19
Q

Flaps/Slats Configurations and Speeds ( Conf 2)

A

Slats 22º, Flaps 15º, ECAM 2, MAXIMUM SPEED 200 knots

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20
Q

Flaps/Slats Configurations and Speeds ( Conf 3)

A

Slats 22º, Flaps 20º, ECAM 3, MAXIMUM SPEED 185 knots

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21
Q

Flaps/Slats Configurations and Speeds ( Conf FULL)

A

Slats 27º, Flaps 40º(319)/35º(320), ECAM FULL, MAXIMUM SPEED 177 knots

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22
Q

Max Altitude Flaps/Slats Extended

A

20 000 feet

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23
Q

VLE - Max Speed Gear Extended

A

280 knots / M.67

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24
Q

VLOe - Max Speed Gear may be extended

A

250 knots

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25
Q

VLOr - Max Speed Gear may be retracted

A

220 knots

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26
Q

Max speeds L/G doors not closed

A

250 knots

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27
Q

Max Altitude L/G may be extended

A

25 000 feet

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28
Q

Max Tire Speed

A

195 knots

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29
Q

Max Speed Windshield Wipers in use

A

230 knots

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30
Q

Max Speed Cockpit Window Open

A

200 knots

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31
Q

Max Altitude With Cockpit window/windshield cracked

A

FL230

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32
Q

Max Taxi speed (GW > 76T)

A

20 knots in a turn

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33
Q

Max Taxi Speed with 1 tire per gear deflated

A

Turning: 7 knots

(Max 3 tires)

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34
Q

Max Taxi Speed with 2 deflated tires on the same main gear

A

3 knots + Max 30º NWS

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35
Q

Max Taxi Speed with ECAM: “WHELL N/W STRG FAULT”

A

10 knots

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36
Q

Cabin Pressure Maximum Positive Diff. Press.

A

9 PSI

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37
Q

Cabin Pressure Maximum Negative Diff. Press.

A

-1 PSI

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38
Q

Cabin Pressure Maximum Positive Diff. Press. (Safety Relief Valve)

A

+8.6 PSI

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39
Q

Elec: Max Load per Generator

A

100 % (90 kVA)

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40
Q

Elec: Max Continuous Load per TRU

A

200A

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41
Q

Minimum Height to engage AP after TO with SRS mode

A

100 feet AGL (+5 seconds after liftoff)

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42
Q

Minimum Height AP use on ILS CAT 1

A

160 feet AGL

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43
Q

Maximum Fuel Imbalance allowed with full tanks

A

1500 kg

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44
Q

JET A-1 Freezing Temperature

A

-47ºC

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45
Q

JET A-1 Minimum Temperature

A

-43ºC

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46
Q

JET A-1 Maximum Temperature

A

+54ºC

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47
Q

Minimum Fuel for Takeoff

A

1500 kg

(+ no “WING TK LO LVL” ECAM)

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48
Q

Normal Operating Hydraulic Pressure

A

3000 PSI +/- 200

RAT 2500 PSI

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49
Q

Max Takeoff brake temperature with Brake fans ON

50
Q

Max Takeoff brake temperature with Brake fans OFF

51
Q

APU “LOW OIL LEVEL”

A

another 10 hours of operation

52
Q

APU Starter (waiting time after 3 attempts)

A

60 minutes

53
Q

APU Maximum Rotor Speed

54
Q

APU Start Up and Electrical Power use

A

Max FL 390

55
Q

APU Battery Restart limit up to (Elec Emerg)

56
Q

APU Max altitude to assist engine start

A

20 000 feet

57
Q

APU Max altitude for air conditioning and pressurization with 2 packs

58
Q

TOGA

A

5 minutes (10 if OEI)

59
Q

TOGA EGT LIMIT

60
Q

MCT EGT LIMIT

61
Q

Engine: OIL Minimum Starting Temperature

62
Q

Engine: OIL Minimum Takeoff Temperature

63
Q

Minimum Engine Oil Quantity

A

9,5 Qts + 0,5 Qts/h + 15 minutes

64
Q

Engine Start pause between start cycles

A

20 seconds

1 cycle = 3 attempts

65
Q

Engine Start cooling after 4 attempts

A

15 minutes

66
Q

IRS

A

73ºN - 60º S

67
Q

Vmca

A

110 knots IAS at Sea Level, decreasing with increase in altitude

68
Q

Vmcg

A

111 knots IAS at sea level with CONF 1+F, decreasing with increase in altitude and flap setting

69
Q

MAX time without Air Cond Supply with PAX onboard

A

20 minutes

70
Q

Max. APU EGT for START

A

1090°C below 35 000 ft

1120 ºC at or above 35 000 ft

or (MSN):

900°C below 25 000 ft

982 ºC at or above 25 000 ft

71
Q

Max EGT for Engine start

72
Q

Maximum taxi speed to backtrack

73
Q

ROLLING TAKEOFF MIN. RWY LENGTH

74
Q

MTOW (319/320)

A

Voe fleet:

66 000 kg/ 71 500 kg

75
Q

MLW (319/320)

A

61 000 kg or 62 500 kg/ 66 000 kg (NNZ, MBK, NOL: 64500KG)

76
Q

Maximum nosewheel travel during towing

A

85 º (Mechanical stop at 95º)

77
Q

Maximum safety relief differential pressure

78
Q

Maximum negative differential pressure

79
Q

RNP Accuracy with GPS PRIMARY

A

With AP ON in NAV:

  • En Route: 1 NM
  • In Terminal Area: 0.5 NM
  • In Approach: 0.3 NM

With AP OFF and FD ON in NAV:

  • En Route: 1 NM
  • In Terminal Area: 0.51 NM
  • In Approach: 0.3 NM

With AP OFF and FD OFF:

  • En Route: 1.1 NM
  • In Terminal Area: 0.51 NM
  • Not Authorized
80
Q

NON PRECISION APPROACHES WITH OEI

A

If OEI, use of AP is not allowed for NPA in the following flight modes:
‐ FINAL APP
‐ NAV/VS
‐ NAV/FPA.
Note: The use of FD in NAV mode remains authorized.

81
Q

SPEED BRAKES LIMITATION

A

For approach, the use of speed brakes at or below 240 kt is not permitted if:
‐ GWCG is above 35 % or
‐ In overweight landing conditions.

82
Q

AUTOLAND

A

Autoland has been demonstrated:
‐ With CAT II and CAT III ILS beam, with ILS slope angle inside a range of -2.5 ° and -3.15 °
‐ For an airport that has an elevation between -1 000 ft and 9 200 ft.
Performance of ROLL OUT mode has been demonstrated on dry and wet runways.

One autopilot at least must be engaged in APPR mode and CAT 2 or CAT 3 SINGLE or CAT 3 DUAL capability must be displayed on FMA.

83
Q

Minimum Height AP use on FINAL APP, V/S or FPA

A

250 ft AGL

84
Q

Minimum Height AP use on CIRCLING

A

500 ft AGL

85
Q

Minimum Height AP use after manual GO-Around

A

100 ft AGL

86
Q

Use of AP or FD in OPEN DES or DES mode

A

The use of AP or FD in OPEN DES or DES mode is not permitted if FCU altitude is set below MDA/MDH or 500 ft AGL, whichever is higher.

87
Q

Minimum Height AP use on CAT II Approach (No Autoland)

88
Q

Minimum Decision height CAT II APPROACH AUTOLAND

A

100 ft AGL

One autopilot at least must be engaged in APPR mode and CAT 2 or CAT 3 SINGLE or CAT 3 DUAL capability must be displayed on FMA

89
Q

MAX WIND - CAT II OR CAT III APPROACH OR AUTOMATIC LANDING AND AUTOMATIC ROLLOUT

A

With all engines operative (AEO):

CONF FULL with airport elevation at or below 5 750 ft:

  • *Headwind: 20 kt (30 kt for A320)**
  • *Tailwind: 10 kt**

Crosswind: 20 kt

With one engine inoperative (OEI):
CONF FULL with airport elevation at or below 5 750 ft:
Headwind: 15 kt
Tailwind: 10 kt
Crosswind: 10 kt

90
Q

IRS accuracy compliance ( max light time)

91
Q

IRS Ground Alignment latitude limitations

A
  • If all ADIRUs have the same magnetic variation table:
    Flights using the NAV mode are prohibited:
    ‐ North of 73 ° North, and
    ‐ South of 60 ° South.
  • If one ADIRU has a different magnetic variation table:
    Flights using the NAV mode are prohibited:
    ‐ North of 60 ° North, between 30 ° West and 160 ° West, and
    ‐ North of 73 ° North, and
    ‐ South of 55 ° South.
92
Q

Max APU EGT

A

742 ºC/675ºC (MSN)

93
Q

MAX EGT FOR ENGINE START

94
Q

ENG MAX ROTOR SPEEDS (N1/N2)

A

N1: 104% / N2: 105%

95
Q

OIL MINIMUM PRESSURE

96
Q

OIL MAXIMUM TEMPERATURE

A

140ºC for continuous operations

97
Q

Maximum/Min FLEX TEMP

A

The flex temperature must not be:
‐ Higher than ISA + 70
‐ Lower than the flat rating temperature or actual OAT.

98
Q

Engine anti-ice must be ON

A

During all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below -40 °C SAT.

The engine anti-ice must be ON prior to and during descent in icing conditions, including temperatures below -40 °C SAT.

99
Q

Air Cond: Max time without AC

A

With pax on board, it is not recommended to exceed 20 min without air conditioning supply.

100
Q

APU BLEED USE WITH HP 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.

101
Q

Avionics Ventilation: Time limit without electrical power depending on OAT

A

49ºC55ºC - 2 h

55ºC60ºC - 1 h

60ºC64ºC - 0.5 h

102
Q

PACKS USE WITH 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.

103
Q

Use of NAV mode after takeoff

A

NAV mode may be used after takeoff provided that:

‐ GPS PRIMARY is available, or
‐ The flight crew checked the FMGS takeoff updating.

104
Q

Use of NAV mode in terminal area

A

NAV mode may be used in terminal area provided that:
‐ GPS PRIMARY is available, or
‐ the appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed, or
‐ FMS navigation is crosschecked with navaid raw data.

105
Q

APU Max altitude for air conditioning and pressurization with 1 pack

A

20 000 feet

106
Q

DEFINITION OF SEVERE ICE ACCRETION

A

Ice accretion is considered severe when the ice accumulation on the airframe reaches approximately 5 mm (0.2 in) thick or more.

107
Q

RAIN REPELLENT

A

The flight crew should only use the rain repellent in the case of moderate to heavy rain

108
Q

TAXI WITH DEFLATED OR DAMAGED TIRES

A

-Maximum taxi speed during turn: 7 kt (max one tire per gear)
‐ If two tires are deflated on the same main gear (maximum one main gear): Maximum taxi speed: 3 kt
‐ Maximum NWS angle: 30 °

In addition, if tire damage is suspected, the flight crew must ask for an aircraft inspection prior to vacate the runway or taxi. If the ground crew suspects that a tire burst may damage the landing gear, maintenance action is due.

109
Q

Flights over water limitation

A

In order to comply with CAT.IDE.A.285 and since Volotea does not carry life rafts on board, the maximum distance to an adequate aerodrome will be limited to 1h flight time in still air conditions or 400 nm, taking the lower one.

110
Q

Navigation limitations due to SSR navigation performance requirements

A

All A320F fleet has anticolision system (ACAS)
ACAS II type, Mode S EHS (Enhanced Surveillance) ATC Transponders, and ADS-B system. Refer to FCOM DSC-34-SURV

111
Q

Definition of Wet runway

A

A runway whose surface is covered by any visible dampness or water up to and including 3 mm deep within the area intended to be used (OM - B)

112
Q

EFB Battery level

A

1st flight: 50% (90% mount inop)

consecutive flights: 25% (40% mount inop)

During descent the charging must be stopped and the charger and cables stowed before passing FL 100

113
Q

A320F MAXIMUM DEVIATION FROM THE ILS GLIDE PATH AND/OR LOCALISER

A

In accordance with FCOM PRO-NOR-SRP-01-70 the warning of excessive beam deviation is a flashing of the LOC and G/S scales on the PFD and ND ROSE ILS. It shall occur whenever:

  • G/S deviation is greater than 1 dot (above 100 ft RA).
  • LOC deviation is greater than 1/4 dot(above 15 ft RA).
114
Q

REQUIRED VISUAL REFERENCE FOR CAT II APPROACH

A

The visual references must contain:
• a segment of at least 3 consecutive lights being:
• the centre of the approach lights, or
• touchdown zone lights, or
• runway centre line lights, or
• runway edge lights, or
• a combination of these
• a lateral element of the ground pattern:
• an approach lighting crossbar, or
• the landing threshold, or
• a barrette of the touchdown zone lighting

115
Q

Max vertical speed during last 2000ft of climb/descent

A

1500 ft/min (FCOM)

116
Q

What brake temp. Requires maintenance action?

A

-Temp difference between two brakes > 150°C; + 1 brake over 600°C / below 60°C -ONE BRAKE EXCEEDS 900°C

117
Q

G or Y HYD RESERVOIR value turns Amber?

A

When below LOW LEVEL WARNING: 3.5 L

118
Q

Required equipment for RVSM

A

-1 XPDR -1 AP -1 FCU CHANNEL -1 FWC -2 ADRs -2 DMCs -2 PFDs

119
Q

Max EXTRA FUEL (due weather)

A

805kg - 320 775kg - 319 ( Sufficient to 20’ holding at 1500’)

120
Q

When is OETD not allowed?

A
  • cold engine (>6h) -Icing conditions - LVO - Slippery or contaminated rwy -self maneuvering to left - failure affecting HYD, ELEC; APU GEN; STEERING/BRAKING CAPABILITY; BLEED
121
Q

When is OETD not allowed?

A
  • cold engine (>6h) -Icing conditions - LVO - Slippery or contaminated rwy -self maneuvering to left - failure affecting HYD, ELEC; APU GEN; STEERING/BRAKING CAPABILITY; BLEED
122
Q

Max. Taxi speed on contaminated taxiways

A320F (24 decks)

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