Airbus A320 Limitations Flashcards

1
Q

MIN T/O & Landing Altitude

A

-1000 MSL

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2
Q

MAX T/O & Landing Altitude

A

9,200 MSL

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3
Q

MAX Operating Altitude

A

FL 39800

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4
Q

MAX Runway Slope

A

+ / - 2 %

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5
Q

MAX Crosswind Takeoff

A

29 G 38 Knots

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6
Q

MAX Crosswind Landing

A

33 G 38 Knots

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7
Q

MAX Tailwind

A

10 KTS

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8
Q

NOMINAL RUNWAY WIDTH

A

148’ (45 M)

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9
Q

VMO / MMO

A

350 KIAS / .82M

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10
Q

VTURB BELOW FL200

A

250 KIAS

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11
Q

VTURB FL200-FL320

A

275

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12
Q

VTURB ABOVE FL320

A

n.a. / .76M

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13
Q

Vfe 1

A

230 KIAS

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14
Q

Vfe 1 + F

A

215 KIAS

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15
Q

Vfe 2

A

200 KIAS

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16
Q

Vfe 3

A

185 KIAS

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17
Q

Vfe 4

A

177 KIAS

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18
Q

Vlo (EXTEND)

A

250 KIAS

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19
Q

Vlo (RETRACT)

A

220 KIAS

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20
Q

Vle

A

280 KIAS / .67M

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21
Q

VWW (Windshield Wiper)

A

230 KIAS

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22
Q

Vtls (Tire)

A

195 KIAS

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23
Q

Max Window Speed

A

200 KIAS

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24
Q

Max Taxi Weight

A

162,900 lbs

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25
Q

Max Takeoff Weight

A

162,000 lbs

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26
Q

Max Landing Weight

A

142,200 lbs

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27
Q

Max ZFW

A

134,500 lbs

28
Q

Minimum Flight Weight

A

82,080 lbs

29
Q

Min Alt. Autopilot on after T/O with SRS

A

100’ AGL

30
Q

Min Alt. Autopilot on-Non-Precision Approach

A

MDA

31
Q

Min Alt. Autopilot on-Circling Approach

A

MDA-100’

32
Q

Min Alt. Autopilot on ILS with CAT I on FMA

A

160’ AGL

33
Q

Min Alt. Autopilot on after Go Around with A/P or F/D

A

100’ AGL

34
Q

Min Alt. Autopilot on All other Phases

A

500’ AGL

35
Q

Autothrust On

A

With or without AP/FD in selected or managed

36
Q

AP/FD in DES or OP DES

A

Not applicable unless FCU ALT at or above MDA or 500’ AGL

37
Q

MIN FUEL TEMP

A

-36 C

38
Q

MAX FUEL IMBALANCE

A

3300 lbs. Inner

1500 lbs. Outer

39
Q

MIN FUEL FOR TAKEOFF

A

3300 lbs. No Low Level Warning

40
Q

Oxygen MIN Crew

A

Refer to FCOM below 1500’

41
Q

Oxygen REF Temp, Ground

A

(OAT + Cockpit Temp) / 2

42
Q

Oxygen REF Temp, Flight

A

Cabin Temp C - 10 C

43
Q

EGPWS Use for Navigation

A

NO

44
Q

EGPWS Man-Made objects

A

NO

45
Q

EGPWS Runway not in database

A

Turn off

46
Q

Engine Start Cycles CFM

A

4 Cycles of 2 minutes ON and 20 seconds OFF followed by 15 minutes of Cooling.

47
Q

Engine Start Cycles IAE

A

2 Cycles of 2 minutes ON and 15 seconds OFF followed by 3rd cycle of 1 minute ON and then 30 minutes of Cooling.

48
Q

G Limits

A

Clean Config. -1.0 - +2.5 G

Flaps/Slats 0 - +2.0 G

49
Q

Doors - Max Wind

A

Cargo Opening - 40 knots
Cargo Open - 65 knots
PAX Open - 65 knots

50
Q

Pressurization - MAX Positive DPSI

A

8.6 psid

51
Q

Pressurization - MAX Negative DPSI

A

-1.0 psid

52
Q

Pressurization - MAX PSID Ram Air

A

<1 psid

53
Q

Air Conditioning - LP Ground Use

A

No Packs ON

54
Q

Air Conditioning - HP Ground Use

A

No APU BLEED

55
Q

Reverse Thrust

A

IN Flight - Not permitted
Power Back - Not permitted
Max Reverse - until 70 knots
Idle Reverse - To a Stop

56
Q

MAX Altitude Gear Extension

A

FL 250

57
Q

MAX Altitude Flaps/Slats Extension

A

FL 200

58
Q

MAX Brake Temp for T/O

A

300 C - fans off

59
Q

Park Brake Engage

A

MAX N1 75%

60
Q

Taxi after Tire Damage

A

1 Tire - Max 7 knots in turn

2 Tires - Max 3 knots in turn & 30 degrees steering

61
Q

Max Hydraulic Pressure

A

3000 -/+ 200 PSI

62
Q

Hydraulics - Single Engine Taxi

A

No brake input on second start.

63
Q

IRU area of operation

A

73 degrees North

60 degrees South

64
Q

CFM-56-5B Engine Thrust

A

26,500 lbs

65
Q

IAE V2527-A5 Engine Thrust

A

27,000 lbs

66
Q

CFM-56-5B Engine Temps Limits

A

Start 725 C
MCT 915 C
TOGA 1 Engine 950 C/ 10 minutes
TOGA 2 Engine 950 C/ 5 minutes

67
Q

IAE V2527-A5 Engine Temp Limits

A

Start 635 C
MCT 610 C
TOGA 1 Engine 635 C/ 10 minutes
TOGA 2 Engine 635 C/ 5 minutes