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Airbus 320 Family > Limitations - 03/17 > Flashcards

Limitations - 03/17 Flashcards

1
Q

Kind of Operations

A

VFR and IFR
Extended Overwater flight
Flight in Icing Conditions

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2
Q

Minimun Flight Crew

A

The minimum Flight Crew consists of 2 pilots

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3
Q

Flight Maneuvering Load Accelerations Limits

A

Clean Configuration……………………….-1.0g to +2.5g
Other Configuration………………………. 0g to +2.0g

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4
Q

Aircraft Wingspans

A

A319, A320, A321 ——————- 111’ 10”

A320, A321 ( Sharklet ) ———— 117’ 5”

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5
Q

Maximum Certified Altitude

A

FL 398

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6
Q

Runway Slope ( mean )

A

+/- 2%

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7
Q

Runway Altitude

N502NK-N694NK / N901NK-N905NK

A

9,200 ft

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8
Q

Nominal Runway Width

A

45m ( 148 Ft ) - Can be reduced to 98 Ft in accordance with “Operations on Narrow Runways” COM procedure.

Note: The A321 without sharklets is NOT authorized to operate on runways less than 148 Ft wide.

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9
Q

Maximum demonstrated crosswind at landing

A

N502NK-N536NK / N587NK-N683NK / N901NK-N905NK

38 kt ( Gust Included )

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10
Q

Maximum tailwind for takeoff

A

15 kt

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11
Q

Maximum tailwind for landing

A

10 Kt

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12
Q

Maximum wind for passenger door operation

A

65 kt

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13
Q

Gear Speeds

A

Landing gear extended ( VLe ) - 280 kt/M.67
Landing gear extension( VLo ) - 250 kt/M.60
Landing gear retraction( VLo ) - 220 kt/M.54

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14
Q

Max altitude landing gear may be extended

A

25,000 Ft

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15
Q

Maximum Tire Speed

A

195 Kt

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16
Q

Taxi Speed

N601NK-N696NK

A
  • When the taxi weight is higher than 167,550 LBS, (76,000 KG) do not exceed a taxi speed of 20 Kt during a turn.
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17
Q

MLW A319

A

137,788 LBS

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18
Q

Windshield Wipers in Use

A

Max speed….. 230 kt

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19
Q

Maximum speed cockpit window open

A

200 Kt

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20
Q

MLW A320CEO

A

145,505 LBS

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21
Q

MLW A320NEO

A

148,591 LBS

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22
Q

MLW A321

A

171,519 LBS

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23
Q

APU with HP Ground Unit

A

Do not use HP ground unit when the APU supplies bleed air to avoid bleed system damage.

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24
Q

Cabin Pressure - Max positive differential pressure

A

9.0 Psi

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25
Q

Cabin Pressure - Max negative differential pressure

A

-1.0 Psi

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26
Q

Cabin Pressure - Safety relief valve setting

A

8.6 Psi

27
Q

Air Conditioning with LP Ground Unit

A

Do not use conditioned air simultaneously from the packs and LP ground unit ( to avoid chattering of the non-return valves).

28
Q

Auto Flight Function

Minimum height for use of Autopilot

A

Takeoff with SRS mode…………………………..100 Ft AGL
Straight-in non precision approach………… Applicable Minimum
Circling Approach……………………Applicable Circling Minimums - 100 Ft
ILS Approach CAT II / CAT III is not displayed on FMA………..160 Ft AGL
Go-Around ( AP or FD engagement ) ……… 100 Ft AGL
All other Phases …………………………………… 500 Ft AGL (A319/A320)
…………………………………… 900 Ft AGL ( A321 )
Use of AP or FD in Open DES or DES mode is not permitted in approach, unless FCU altitude is set at or above:
Highest of
-Minimum or 500 Ft AGL (A319/A320)
-Minimum or 900 Ft AGL ( A321 )

29
Q

Flight Management Function

A

NAV mode may be used in the terminal area, provided:

  • GPS PRIMARY is available or,
  • HIGH accuracy is displayed, and the appropiate RNP is checked or entered on the MCDU, or
  • FMS navigation is cross-checked with NAVAID raw data
30
Q

Non-Precision Approaches with Engine-Out

A319 & A321

A

If one engine is inoperative, it is NOT permitted to use the autopilot to perform NPAs in the following modes:

FINAL APP, NAV V/S, NAV/FPA

Only FD use is permitted

31
Q

Go Around

  • Applicable to A320NEO
A

When operating the aircraft on airports with a pressure altitude between 6,000 Ft and 9,200 Ft, the flight crew shall use:

  • Flaps 3, or
  • Flaps Full with approach speed of at least VLS + 5 Kt
32
Q

Automatic Approach, Landing and Roll Out

A

ILS CAT III Fail Passive ( Single )

Minimum decision height ……….. 50 Ft

ILS CAT III Fail Operational ( Dual )

Alert Height ……………………………100 Ft

Minimum RVR …………………………300 RVR

Note: A/THR must be used in selected or managed speed.

33
Q

All Engines Operative (AEO), Maximum wind conditions for CAT II or CAT III Automatic Approach, Landing and Roll out

N502NK - N536NK

A

Headwind - 20 Kt
Tailwind - 5 Kt
Crosswind - 15 Kt

34
Q

Maximum wind conditions for ILS CAT II or ILS CAT III

A319

A

CONF Full with airport Elevation at or below 5,750’:
Headwind - 20kt ( 15 Kt - OEI )
Tailwind - 10 Kt
Crosswind - 15 Kt ( 10kt - OEI )

CONF Full with airport elevation above 5,750’ or CONF 3:
Headwind - 20kt ( 15 Kt - OEI )
Tailwind - 5 Kt
Crosswind - 15 Kt ( 10kt - OEI )

35
Q

Maximum wind conditions for ILS CAT II or ILS CAT III

A320

A

Headwind - 30 Kt
Tailwind - 10 Kt
Crosswind - 15 Kt

36
Q

Maximum wind conditions for ILS CAT II or ILS CAT III

A320NEO

A

Headwind - 20 Kt
Tailwind - 5 Kt
Crosswind -15 Kt

37
Q

Maximum wind conditions for ILS CAT II or ILS CAT III

A321

A

Headwind: 40 kt CAT II / 30 kt CAT III
Tailwind: 10 kt
Crosswind:15 kt

38
Q

APU

APU Starter

A

After 3 starter motor duty cycles, wait 60 min before attempting 3 more cycles.

39
Q

Air Bleed Extraction

APS 3200 Hamilton Standards APU

A

Max altitude to assist engine start - 20,000’

One Pack up to 20,000’ ( 22,500’ Honeywell 131-9 = N535-36 / N640-94NK )

Two Packs up to 15,000’

Use of APU bleed air for wing A/I is not permitted

40
Q

Power Plant - Thrust Setting/ EGT Limits

A320

A

Starting: 635c
Takeoff & Go-Around: 5 minutes @ 635c
10 minutes @ 635c - OEI
MCT: Unlimited @ 610c

41
Q

Power Plant - Thrust Setting/ EGT Limits

A321

A

Starting: 635c
Takeoff and Go-Around: 5 minutes @ 650c
10 minutes@ 650c - OEI
MCT: Unlimited @ 610c

42
Q

Oil

V2500

A

Minimum starting temperature: -40c
Minimum prior to exceeding Idle: -10c
Minimum prior to Takeoff: 50c
Minimum Oil Pressure: 60 Psi

43
Q

Oil

PW1100G

A

Minimum starting temperature: -40c
Minimum prior to Takeoff: 52c
Minimum Oil Pressure: 65 Psi

44
Q

Starter Duty - V2500

A
  • A standard automatic start that includes only one attempt is considered one cycle
  • For ground starts ( automatic or manual ), a 15s pause is required between successive cycles
  • A 30 min cooling period is required, subsequent to 3 failed cycles or 5 min of continuous crank
  • For manual start, observe a 2 minutes maximum cycle time.
  • For crank, observe a 5 min maximum cycle time
  • The starter must not be run when N2 is above 10% on the ground and 18% in-flight.
45
Q

Starter Duty - PW1100G

A
  • A standard automatic start that includes up to 3 start attempts, is considered one cycle
  • For ground starts ( automatic or manual ), a 35s pause is required between successive cycles
  • A 15 min cooling period is required, subsequent to three failed cycles, or 15 min of continuous or accumulated crank
  • The starter must not be run when N2 is above 20%
46
Q

Reverse Thrust

A

Maximum reverse should not be used below 70 knots. Idle reverse is permitted down to aircraft stop.

47
Q

Reduced Thrust Takeoff

A319

A

Must not exceed 25% of full rated takeoff thrust.

ISA + 65c ( Total Max Flex )
ISA + 60c ( Engine A/I On )

Not permitted on contaminated runways.

48
Q

Reduced Thrust Takeoff

A320

A

Must not exceed 25% of full rated takeoff thrust.

ISA + 55c ( Total Max Flex )

Not permitted on contaminated runways.

49
Q

Reduced Thrust Takeoff

A321

A

Must not exceed 25% of full rated takeoff thrust.

ISA + 42c ( Total Max Flex )

Not permitted on contaminated runways.

50
Q

Reduced Thrust Takeoff

A320NEO

A

Must not exceed 25% of full rated takeoff thrust.

ISA + 50c ( Total Max Flex )

Not permitted on contaminated runways.

51
Q

Power Plant - Thrust Setting/ EGT Limits

A320NEO

A

Starting: 1,083c
Takeoff & Go-Around: 5 minutes @ 1,083c
10 minutes @ 1,083c - OEI
MCT: Unlimited @ 1,043c

54
Q

Flight Controls - Flaps & Slats

Max operating altitude with slats and/or flaps extended

A

20,000 feet

56
Q

Maximum Allowed Fuel Imbalance

A319, A320 & A320NEO

At Landing

A

Inner Tank: 3,306 LB - Max Allowed Imbalance

57
Q

Oil

Minimum Oil Quantity - PW1100G

A

14 quarts

If the OAT is colder than -30c

16.5 quarts

58
Q

Oil

Minimum Oil Quantity - V2500

A

11.0 quarts + estimated consumption (average estimated consumption } 0.3 quarts./ hour )

59
Q

Landing Gear - Nosewheel Steering

Nosewheel Steering Angle Limits

A

Handwheel - 75

Towing & Pushback - 95

Towbarless - 85

60
Q

Crosswind Operation

A

This engine is capable of starting in crosswinds of up to 35 knots.

61
Q

Ground Clearance Chart

A

A 319 Ext 15.5 Compressed 13.9

A 320 Ext 13.5 Compressed 11.7

A 320N Ext 13.7 Compressed 11.7

A 321 Ext 11.2 Compressed 9.7

62
Q

Landing Gear - Brakes

Maximum brake temperature for takeoff

A

300c. - Brake fans off, if installed

63
Q

Maximum Allowed Fuel Imbalance

A319, A320 & A320NEO

At Takeoff

A

Inner Tank: 1,102 LB - Maximum Allowed Imbalance

63
Q

Maximum Allowed Fuel Imbalance

A321

At Takeoff

A

882 LB

63
Q

Maximum Allowed Fuel Imbalance

A321

At Landing

A

2,910 LB

63
Q

Fuel Temperature

A

For Jet A only, if TAT reaches -34c, monitor on Fuel SD page that fuel temperature remains higher than -36c.

Airbus 320 Family (3 decks)

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