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A32x > FCOM LIM > Flashcards

FCOM LIM Flashcards

1
Q

Maximum pax LIM

A

318 / 319 / 320 Airbus 180 / 145 / 136 Avianca 162 / 132 / 120

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2
Q

Kind of operations LIM

A

VFR / IFR Extended overwater Icing conditions

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3
Q

Weights LIM

A

318 / 318 / 319 / 320 / 320s Mtxw +400 = = = = Mtow 63.0 / 68.0 / 75.5 / 77.0 / 78.0 Mlw 57.5 / 57.5 / 62.5 / 66.0 / 66.0 Mzfw = / -3 / -4 / -3,5 / = MinW = / 34.5 / 35.4 / 37.2 / =

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4
Q

Runway slope LIM

A

+- 2 %

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5
Q

RUNWAY ALTITUDE LIM

A

MAX

9200 ft

_______________

MIN

CEO/321 -1000 ft

NEO -2000 ft

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6
Q

NOMINAL RUNWAY WIDTH LIM

A

NEO/321 ……………………………………………45 m

________________________________

CEO 320 Nominal Width………………….45 m

Minimal runway width……..30 m

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7
Q

WIND FOR TAKEOFF AND LANDING DRY LIM

A

A321NEO ………………………… 35kt (JUST TAKE OFF)

CEO/NEO…………………………..38kt

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8
Q

Maximum X wind for TO and LNDG damp LIM

A

20kt

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9
Q

Maximum X wind for TO and LNDG ice LIM

A

15Kt

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10
Q

MAXIMUN TAIL WIND for AUTOMATIC LANDING LIM

A

10Kt

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11
Q

Maximum wind to operate pax door LIM

A

65kt

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12
Q

Maximum wind to operate cargo door LIM

A

40kt or 50kt if nose is into the wind ( and should be closed before 65Kt)

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13
Q

TO is FORBIDDEN if LIM

A

Wet ice Water over compacted snow Dry snow

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14
Q

MAXIMUM OPERATING SPEED VMO/MMO

A

350kt / 0.82 mach

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15
Q

MAXIMUM FLAPS/SLATS SPEEDS A320

A

1 230kt 1+f 215kt 2 200kt 3 185kt Full 177kt

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16
Q

MAXIMUM OPERATING SPEED VMO/MMO

A

Mvle 280kt / 0.67 mach Mvlo ext 250kt / 0.60 mach Mvlo ret 220kt / 0.54 mach

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17
Q

MAXIMUM TIRE SPEED

A

195 G/S

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18
Q

WIPERS MAXIMUM OPERATING SPEED

A

230kt

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19
Q

COCKPIT WINDOW OPEN MAXIMUM SPEED

A

200kt

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20
Q

MAXIMUN SPEED WHEN ABOVE 76000 kg

A

320 CEO……….20kt

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21
Q

RAM Air inlet min pressure LIM

A

1 psi

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22
Q

PACKS USE WITH LOW PRESSURE AIR CONDITIONING UNIT

A

DO NOT USE LP with / PACKS (Max p 1,2kg/s)

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23
Q

APU BLEED USE WITH HIGH PRESSURE AIR START UNIT

A

DO NOT USE ( avoid system damage)

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24
Q

CABIN PRESSURE MAX positive delta pressure LIM

A

9.0 psi

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25
Q

CABIN PRESSURE Max negative delta pressure LIM

A

-1.0 psi

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26
Q

CABIN PRESSURE Safety relief delta pressure LIM

A

8.6 psi (0.1psi tolerance)

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27
Q

AVIONICS VENTILATION LIM

A

49°c No limit

55°c T< 2h

60°c T< 1h

64°c T< 1/2h

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28
Q

Minnimum AP engagement HEIGHT LIM

A

100ft or 5s ( system logic )

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29
Q

Minimum Height WITH AP In approach with FINAL APP, V/S or FPA mode

A

250ft

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30
Q

Minimum Height WITH AP In CIRCLING approach

A

500 ft AGL for aircraft category C

600 ft AGL for aircraft category D

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31
Q

Minimum Height WITH AP ILS/MLS approach when CAT1 is displayed on the FMA

A

160ft

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32
Q

Minimum Height WITH AP ILS/MLS approach when CAT2 OR CAT 3 is displayed on the FMA

A

0 FT AGL if autoland

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33
Q

Minimum Height WITH AP After a manual go-around

A

100ft

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34
Q

Minimum Height WITH AP ( ALL OTHER PHASES ) LIM A320

A

500ft

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35
Q

Minimum Height SET WITH AP in OPEN DES LIM

A

500ft or MDA / MDH ( whichever is higher)

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36
Q

RNP ACCURACY

A

ENR 1.0nm TER 0.5nm APP 0.3nm

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37
Q

TO WITH OUT “GPS PRIMARY” LIM

A

GPS DESELECT until a safe altitude

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38
Q

TO WITH GLS LIM

A

FORBIDDEN

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39
Q

FOR RNAV(GNSS)

A

At least 1 “GPS PRIMARY”

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40
Q

USE OF NAV MODE IN RNAV APPROACH

A

An RNAV(RNP) approach may be performed, with GPS PRIMARY not available, only if the radio navaid coverage supports the RNP value and HIGH accuracy is displayed on the MCDU with the specified RNP, and an operational approval is obtained. An RNAV(GNSS) approach may be performed provided that GPS PRIMARY is available

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41
Q

ILS CAT2 minimum decision height LIM

A

100ft If manual landing disconnect ap bfr 80ft

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42
Q

ILS CAT 3 FAIL PASSIVE (single) minimum decision height LIM

A

50ft A/THR

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43
Q

ILS CAT 3 FAIL OPERATIONAL (dual) minimum decision height and alert height LIM

A

A320 NEO…….. NONE

A320………………. 25ft

A321……………….. 22ft

AH 100ft

MIN RVR 75m

44
Q

ENGINE OUT CAT2/3 FLAP CONFIG LIM

A

A320N/21/21N……….. 3+FULL

A320CEO…………………FULL

45
Q

MINIMUM FUEL QUANTITY FOR TAKE OFF

A

1500kg

46
Q

MAXIMUM TAILWIND for TAKEOFF and LANDING

A

A320/1 NEO………………………… 15kt

CEO………………………………………..10kt

10kt……COMPANY OMA POLICY

* if landing with MORE than 10kt TL use CONF FULL

47
Q

MAXIMUM FLAPS/SLATS SPEEDS A321

A

1 235kt 1+f 225kt 2 215kt 3 195kt Full 190kt

48
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) A320 NEO

A

116kts

49
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) A320

A

114kts

50
Q

Minimum Height WITH AP ILS/MLS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA

A

0 ft AGL if autoland

51
Q

Minimum Height WITH AP ( ALL OTHER PHASES ) LIM A321

A

900ft

52
Q

DEGRADED SITUATION If GPS PRIMARY LOST is displayed on the ND and MCDU

A

the navigation accuracy remains sufficient for RNP operations provided that, the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.

53
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.

54
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.

55
Q

USE OF NAV MODE IN APPROACH BASED ON RADIO NAVAIDS

A

A navaids approach may be performed in NAV, APP NAV or FINAL APP, with AP or FD engaged, provided that: ‐ If GPS PRIMARY is available, the reference navaid may be unserviceable, or the airborne radio equipment may be inoperative, or not installed, provided that an operational approval is obtained ‐ If GPS PRIMARY is not available, the reference navaid and the corresponding airborne radio equipment must be serviceable, tuned and monitored during the approach.

56
Q

MAXIMUM WIND CONDITIONS FOR ILS/MLS CAT II OR CAT III AND FOR CAT I

A

Headwind : 40 kt for CAT II / 30 kt for CAT III

Tailwind : 10 kt

Crosswind: 25 kt for CAT II / 20 kt for CAT III

57
Q

AUTOMATIC LANDING Alt LIMIT

A

A320 CEO…………………………… 6500ft / -1000ft

A320 NEO…………………………… 9200ft / -2000ft

A321 ………………………………………5750ft / -1000ft

58
Q

APU START ATTEMPTS

A

X3 then 60 min

59
Q

APU MAX ROTOR SPEED

A

Maximum N speed ……………….. 107%

60
Q

Maximum EGT for APU start (below 35 000 ft)

A

1 090 °C

61
Q

Maximum EGT for APU start (above 35 000 ft)

A

1 120 °C

62
Q

Maximum EGT for APU running

A

675 °C

63
Q

APU START/SHUTDOWN DURING REFUELING/DEFUELING

A

‐ If the APU failed to start or following an automatic APU shutdown, do not start the APU ‐ If a fuel spill occurs, perform a normal APU shutdown.

64
Q

APU BLEED Max altitude to assist engine start

A

20 000 ft

65
Q

APU BLEED Max altitude for air conditioning and pressurization (single pack operation) ..and elec power supply

A

22 500 ft

66
Q

APU BLEED Max altitude for air conditioning and pressurization (dual pack operation) ..and elec power supply

A

15 000 ft

67
Q

Use of APU bleed air for wing anti-ice is……

A

not permitted.

68
Q

APU START CEILING LIMIT

A

41 000ft

69
Q

APU ELEC POWER ONLY

A

Above 22 500ft

70
Q

APU Battery restart limit (ELEC Emer CONFIG)

A

25 000 ft

71
Q

GSM ONBOARD

A

The use of mobile phones is prohibited in the toilets and the cockpit. It is prohibited to use the GSM Onboard System: ‐ Below 3 000 m AGL (approximately 10 000 ft) ‐ In some geographical areas (refer to the “Regional Operation Data for the Onboard Mobile Telephony System” document for the identification of these geographical areas).

72
Q

THRUST SETTING/EGT LIMITS

A320 NEO

A
73
Q

THRUST SETTING/EGT LIMITS

A320 IAE

A
74
Q

THRUST SETTING/EGT LIMITS

A321 PW

A
75
Q

SHAFT SPEEDS ( N )

A320 NEO

A

Maximum N1 in normal operation……………………………………………………..100 %

Maximum N1 permitted………………………………………………………………………105 %

____________________________________________

Maximum N2 in normal operation…………………………………………………….100 %

Maximum N2 permitted……………………………………………………………………………………………. 105 %

76
Q

SHAFT SPEEDS (N)

A320 CEO

A321

A

Maximum N1…………………………………………………………………………………………100 %

____________________________________________

Maximum N2 ………………………………………………………………………………………100 %

77
Q

OIL TEMPERATURE

A320 CEO

A321

A
78
Q

OIL TEMPERATURE

A320 NEO

A
79
Q

MINIMUM OIL PRESSURE

A320 CEO

A321

A
80
Q

MINIMUM and MAXIMUM OIL PRESSURE

A320 NEO

A
81
Q

MINIMUM OIL QUANTITY

A

A320 NEO - 14 quarts

A320 CEO and A321 - 11 quarts (0.3 qt/h)

82
Q

START attempts

A

A320 NEO …….. 3x /35s/ then 15 min

(The starter must not be run when N2 is above 20 %)

A320 CEO / A321 …… 3x /15s/ then 30 min or 5 min crank

(The starter must not be run when N2 is above 10 % on-ground and 18 % in-flight.

83
Q

REVERSE THRUST

A

Maximum reverse should not be used below 70 kt.

Idle reverse is permitted down to aircraft stop.

84
Q

REDUCED THRUST TAKEOFF

A

TFLEX cannot be:

‐ Higher than TMAXFLEX, equal to ISA + 50 °C.(NEO)

ISA + 55 °C.(CEO)

ISA + 42 °C.(A321)

ISA + 72 °C.(LCH,LCI)

‐ Lower than the flat temperature (TREF).

‐ Lower than the actual OAT.

85
Q

CROSSWIND OPERATION ON GROUND

A

NEO………….. The engine is able to start in crosswind up to 35 kt.

CEO……………..The engine is able to start in crosswind up to 35 kt. (GUST)

321N……………The engine is able to start in crosswind up to 45 kt.

86
Q

MAXIMUM ALTITUDE FLAPS/SLATS EXTENDED

A

Maximum operating altitude with slats and/or flaps extended…………………20 000 ft

87
Q

FUEL TEMPERATURE LIMITS WHEN JP4 AND JET B FUELS ARE USED

A

If the wing fuel temperature exceeds 30 °C at engine start, the altitude must be limited to 35 000 ft until the center tank is empty.

If the wing fuel temperature exceeds 40 °C at engine start, the altitude must be limited to 30 000 ft until the center tank is empty.

If the wing fuel temperature exceeds 49 °C at engine start, the altitude must be limited to 25 000 ft until the center tank is empty.

88
Q

FUEL TEMPERATURE

A320 CEO

A
89
Q

FUEL TEMPERATURE

A320 NEO

A
90
Q

FUEL TEMPERATURE

A321

A
91
Q

MAXIMUM ALLOWED FUEL IMBALANCE

A

500 kgs …. inner tank. CHECK TABLE

92
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.

93
Q

DEFINITION OF ICING CONDITIONS

A

‐ Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is at or

below 10 °C and visible moisture in any form is present (such as clouds, fog with visibility of 1 sm (1 600 m) or less, rain, snow, sleet or ice crystals).

‐ Icing conditions also exist when the OAT on the ground and for takeoff is at or below 10 °C and operating on ramps, taxiways or runways where surface snow, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes.

94
Q

DEFINITION OF THIN HOARFROST

A

Thin hoarfrost is typically a white crystalline deposit which usually develops uniformly on exposed surfaces on cold and cloudless nights.

It is so thin that surface features (lines or markings) can be distinguished beneath it.

95
Q

RAIN REPELLENT usage

A

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

96
Q

BRAKE TEMPERATURE

A

Maximum brake temperature for takeoff (brake fans  off)……………………………………………..300 °C

97
Q

MINIMUM FLIGHT CREW OXYGEN PRESSURE

A

check table

98
Q

NOSEWHEEL STEERING (NWS)

A

Towbarless operation on the nose landing gear (towing and pushback) is approved when using the accepted towbarless towing vehicles listed in the Airbus WISE ISI 09.11.00001, with the following

information:

Maximum NWS angle………………………………………………………………………….. ±85 °

99
Q

INERTIAL REFERENCE SYSTEM (IRS)

IR GROUND ALIGNMENT

A

Ground alignment of the IRS is possible in latitudes between 73 ° North and 73 ° South.

100
Q

TAXI WITH DEFLATED OR DAMAGED TIRES

A

‐ If maximum one tire per gear is deflated (consider three gears)

Maximum taxi speed during turn……………………………………………………………………………………. 7 kt

‐ If two tires are deflated on the same main gear (maximum one main gear)

Maximum taxi speed……………………………………………………………………………………………………. 3 kt

‐ For the nosewheel steering (NWS) angle

Maximum NWS angle………………………………………………………………………………………………….. 30 °

101
Q

GPWS / PREDICTIVE GPWS

A

The predictive GPWS  functions should be inhibited (TERR pushbutton to OFF, on the GPWS panel) when the aircraft position is less than 15 NM from the airfield:

‐ For operations from/to runways not incorporated in the predictive GPWS database.

‐ For specific approach or departure procedures, which have previously been identified as potentially causing expected or spurious terrain alerts.

102
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIM

A

Clean configuration ………-1 g to +2.5 g Other configurations………0 g to +2 g

103
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) OLD A320

A

109kts

104
Q

CAN YOU MAKE AN AUTOLAND IF CAT 2 ON FMA?

A

YES - “At least CAT2 capability is displayed on the FMA and the crew uses CATII / III procedures”

105
Q

GSM ONBOARD

A

FORBIDDEN in the toilets and cockpit

A32x (7 decks)

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