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Airbus 320 GlobalX > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Crosswind

Takeoff

A
  • 38 kts

* Gust included

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2
Q

Max Crosswind

Landing

A
  • 38 kts

* Gust included

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3
Q

Max Tailwind (Takeoff)

A
  • *15 kts

* * For landing with a tailwind greater than 10 knots use FLAPS FULL

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4
Q

Max Tailwind (Landing)

A
  • *15 kts

* * For landing with a tailwind greater than 10 knots use FLAPS FULL

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5
Q

Max Wind for Passenger Door Operations

A

65 kts

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6
Q

Max Wind Cargo Door Operation

A 
40 kts
(50 kts if aircraft is positioned into the wind or door is on the leeward side)
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7
Q

Cargo Doors must be closed before wind exceeds

A

65 kts

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8
Q

VLE

A

280 kts / M 0.67

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9
Q

VLO - Extension

A

250 kts / M 0.60

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10
Q

VLO - Retraction

A

220 kts / M 0.54

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11
Q

Max Tire Ground Speed

A

195 kts

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12
Q

Max Brake Temp for Takeoff

A

300°C (150°C if brake fans in use)

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13
Q

Max Operating Altitude

A

FL 390

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14
Q

Severe Turbulence Penetration Speed

A

275 kts / M0.76

250 kts below FL 200

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15
Q

Max Speed with Windshield Wipers in Use

A

230 kts

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16
Q

Max Speed with the Flight Deck Window Open

A

200 kt

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17
Q

AIR CONDITIONING LIMITATIONS

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

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18
Q

AP At Takeoff

A

100 ft AGL

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19
Q

Min Height for AP Use on approaches with FINAL APP,

V/S, or FPA Mode

A

50 ft AGL

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20
Q

Min Height for AP Use on a Circling Maneuver**

A

1,000 ft AGL or Circling MDA(H), whichever higher

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21
Q

Min Height for AP Use during a CAT I ILS WITHOUT

CAT II or CAT III DUAL/SINGLE Displayed

A

160 ft AGL

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22
Q

Min Height for AP Use during a CAT I ILS WITH CAT II

or CAT III DUAL/SINGLE Displayed

A

80 ft AGL

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23
Q

Min Height for AP Engagement on Go Around

A

500 ft AGL

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24
Q

INSTRUMENT APPROACHES

A

RNAV (RNP) AR or RNAV (RNP) Approaches with “Authorization Required” in the notes, are not authorized.

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25
Q

Max Operating Altitude With Slats and/or Flaps Extended

A

FL 200

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26
Q

Max Fuel Imbalance for Takeoff

A

1000 lbs*

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27
Q

Max Fuel Imbalance Inflight or Landing

A

3000 lbs*

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28
Q

Min Oil Quantity for Departure

A

9.5 Quarts + 0.5 Quarts per

Hour of Flight

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29
Q

Min Oil Temperature for Starting

A

-40°C

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30
Q

Min Oil Temperature for Takeoff

A
  • 10°C
31
Q

Max Number of Consecutive Start Cycles

A

4

32
Q

Min Cooling Period After Max Cycles

A

15min

33
Q

Min Pause Between Start Cycles (Ground Start):

A

20 sec

34
Q

Max N2 for Running Re-Engagement of Starter

A

20%

35
Q

Speed Below Which Max Reverse Thrust

SHOULD Not be Used

A

70 IAS

36
Q

WHEN TO USE ENGINE ANTI-ICE

Ground and takeoff

A

• Outside Air Temperature (OAT) is 10°C or below and
• visible moisture in any form is present (i.e., clouds, fog with visibility of 1 mile or less, rain, snow, sleet, or ice crystals), or
• when 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.

37
Q

WHEN TO USE ENGINE ANTI-ICE

In flight

A
  • Total Air Temperature (TAT) is 10°C or below and
  • visible moisture in any form is present (i.e., clouds, fog with visibility of 1 mile or less, rain, snow, sleet, or ice crystals).
38
Q

WHEN TO USE ENGINE ANTI-ICE

Engine anti-ice operation

A

• Engine anti-ice must be ON 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).
• Engine anti-ice must be ON prior to and during descent in icing conditions (including temps below -40° SAT).

39
Q

APU Max Altitude for Dual Pack Operations

A

15,000 ft

40
Q

APU Max Altitude for Single Pack Operations

A

22,500 ft

41
Q

After 3 Starter Motor Duty

Cycles

A

Wait 60 min before attempting another

start

42
Q

Max Altitude to Start the APU during EMER ELEC

CONFIG

A

FL 250

43
Q

EGPWS ALERTS

A

AP……………………………………………………OFF
PTICH…………………………………………….. PULL UP
THRUS LEVERS……………………………… TOGA
SPEEDBRAKES……………………………….. CHECK RETRACTED
BANK……………………………………………….. WINGS LEVEL OR ADJUST
Do not change configuration (slats/flaps, gear) until clear obstacle.

44
Q

EMER DESCENT

A

CREW OXYGEN MASK…………………………. ON
CREW COMMUNICATIONS…………………. ESTABLISH
SIGNS……………………………………………………. ON
ALT ……………………………………………………….. SET and PULL
HDG ……………………………………………………… SET and PULL
SPD/MACH …………………………………………… ADJUST
THRUST LEVERS (if A/THR off) …………… IDLE
SPD BRK ……………………………………………….. FULL (RESPECTING VLS)

45
Q

LOSS OF BRAKING

A

IF AUTOBRAKE IS SELECTED:
BRAKE PEDALS ……………………………………. PRESS

IF NO BREAKING AVAILABLE:
REV ……………………………………………………….. MAX
BRAKE PEDALS ……………………………………. RELEASE
A/SKID & N/W STRG ……………………………. OFF
BRAKE PEDALS ……………………………………. PRESS
MAX BRK PR ………………………………………… 1000 PSI

IF STILL NO BREAKING
PARKING BRAKE …………………………………SHORT AND
SUCCESIVE APPLICATIONS

46
Q

STALL RECOVERY

A

NOSE DOWN PITCH CONTROL …………. APPLY
BANK ……………………………………………………… WING LEVEL

When out of stall(no longer stall indications):
THRUST …………………. INCREASE SMOOTHLY AS NEEDED
SPEEDBRAKES ………………………….. CHECHK RETRACTRED
FLIGHT PATH …………………………….. RECOVERY SMOOTHLY

If clean configuration and below 20,000’ :
FLAP 1 …………………………………………. SELECT

47
Q

STALL WARNING AT LITOFF

A

THRUST ………………………………….. TOGA
PITCH ……………………………………… 15 o
BANK ………………………………………. WINGS LEVEL

48
Q

TCAS WARNINGS

A

AP(If engaged) ………………………… OFF
BOTH FDs ……………………………….. OFF
V/S ……………………….. ADJUST PITCH, MAINTAIN GREEN, AVOID RED
ATC ………………………………………….. NOTIFY

49
Q

UNABLE TO MAINTAIN ALTITUDE

ENGINE FAILURE DRIFTDOWN

A

THRUST LEVERS ………………………. MCT
A/THR ………………………………………… OFF
SPD/MACH ………………………………… SET M.78 AND PULL

  • Consider setting Green Dot ( obstacle strategy) if
    flying over high terrain

HDG …………………………………………… SET and PULL
ALT ………………… SET EO REC MAX from MCDU PROG PAGE and PULL

50
Q

UNRELIABLE SPEED INDICATION

A

• If the safe conduct of the flight is impacted:
AP……………………………………………………………………………………………………………….OFF
A/THR ……………………………………………………………………………………………………….OFF
FD …………………………………………………………………………………………………………….OFF
PITCH/THRUST………………………………………………………………………………………….SET
Below THRUST RED ALT…………………………………………………………………………15o/TOGA
Above THRUST RED ALT andBelow FL100………………………………………….10o/CLB
Above THRUST RED ALT andAbove FL100 …………………………………………. 5o/CLB
FLAPS (if CONF 0 (1) (2) (3)) …………………………………….MAINTAIN CURRENT CONF
FLAPS (if CONF FULL)…………………………………….. SELECT CONF 3 AND MAINTAIN
SPEEDBRAKES ………………………………………………………………..CHECK RETRACTED
L/G …………………………………………………………………………………………………………….. UP

When at or above MSA or Circuit Altitude. Level off for troubleshooting

51
Q

WINDSHEAR

A

At Takeoff
If before V1:
TAKEOFF……………………………………………………………………………………………………REJECT
If there are significant variations in airspeed, and in airspeed trend below the indicated V1, reject
the takeoff.
If After V1:
THR LEVERS…………………………………………………………………………………………. TOGA
REACHING VR……………………………………………………………………………………..ROTATE
SRS ORDERS……………………………………………………………………………………. FOLLOW
Airborne, initial climb or landing:
THRUST LEVERS AT TOGA……………………………………………………. SET or CONFIRM
AP (if engaged)………………………………………………………………………………….. KEEP ON
SRS ORDERS……………………………………………………………………………………. FOLLOW
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF
WINDSHEAR
CLOSELY MONITOR FLIGHT PATH AND SPEED
RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF WINDSHEAR

52
Q

WINDSHEAR AHEAD (RED)

A

During the takeoff run:
TAKEOFF …………………………………………………………………………………………….REJECT
When Airborne:
THR LEVERS……………………………………………………………………………………… TOGA
AP (If engaged)…………………………………………………………………………………..KEEP ON
SRS ORDERS ……………………………………………………………………………………. FOLLOW
Landing:
GO AROUND ……………………………………………………………………………………PERFORM
AP (If engaged)…………………………………………………………………………………..KEEP ON

53
Q

Runway altitude

A

9200 ft

54
Q

VMO

A

350 kt

55
Q

MMO

A

M 0.82

56
Q

Taxi speed

A

20 kt

higher 76000 kg

57
Q

Max taxi weight

A

77 400 kg

58
Q

Max take off weight

A

77 000 kg

59
Q

Max landing weight

A

64 500 kg

60
Q

Max zero fuel weight

A

61 000 kg

61
Q

Minimum weight

A

37 230 kg

62
Q

Max positive differential pressure

A

9.0 PSI

63
Q

Max negative differential pressure

A

-1.0 PSI

64
Q

Safety relief valve setting

A

8.6 PSI

65
Q

APU Max altitude to assist engine start

A

20 000 ft

66
Q

EGT Limit Takeoff/Go-around 2 eng.

A

950*C (5min)

67
Q

EGT Limit takeoff/Go-around 1 eng.

A

950*C (10min)

68
Q

EGT Max Continuous Thrust (MCT)

A

915*C (Not Limited)

69
Q

EGT Starting

A

725*C (On ground/In flight)

70
Q

Max N1

A

104%

71
Q

Max N2

A

105%

72
Q

Max Continuous oil temperature

A

140*C

73
Q

Max transient temperature

A

155*C (15 min)

Airbus 320 GlobalX (1 decks)

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