- •Technical appendices - Contents
- •A318 Key data
- •A319 Key data
- •A320 Key data
- •A321 Key data
- •A320 Family standard cabin layouts
- •A320 Family standard cabin layouts
- •A320 Family standard cabin layouts
- •Standard containers
- •Additional fuel capacity
- •Additional fuel capacity
- •A320 Family flight deck
- •Main instrument panel
- •Main instrument panel
- •Primary Flight Display
- •Navigation Display
- •Electronic Centralised Aircraft Monitor (ECAM)
- •Centralised Fault Display System (CFDS)
- •AIRMAN
- •Maintenance optimisation
- •Fly-by-wire flight controls
- •Fly-by-wire flight controls
- •Wing movable surfaces
- •Competitive choice of engines on A320 Family
- •Advanced engine control
- •A320 Family APU
- •A318 range capability
- •A318 range capability
- •A319 range capability
- •A319 range capability
- •A320 range capability
- •A320 range capability
- •A321 range capability
- •A321 range capability
- •A318 Take-off performance
- •A318 Take-off performance
- •A319 Take-off performance
- •A319 Take-off performance
- •A320 Take-off performance
- •A320 Take-off performance
- •A321 Take-off performance
- •A321 Take-off performance
- •A318 Landing performance
- •A319 Landing performance
- •A320 Landing performance
- •A321 Landing performance
- •Assumptions
A320 Landing performance
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
JAR3% flight profile Typ. 2-class pass. payload 200nm alternate
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2000 |
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6,500 |
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1750 |
CFM56-5B |
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V2500-A5 |
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MLW |
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5,500 |
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(m) |
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(ft) |
distance |
1500 |
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Typical landing weight |
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distance |
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2000 ft |
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4,500 |
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Landing |
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Landing |
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1250 |
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Sea level |
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3,500 |
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1000 |
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750 |
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2,500 |
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50 |
52 |
54 |
56 |
58 |
60 |
62 |
64 |
66 |
68 |
70 |
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Landing weight (t) |
Page 49 |
May 2009 |
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A321 Landing performance
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
JAR3% flight profile Typ. 2-class pass. payload 200nm alternate
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2000 |
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6500 |
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1750 |
CFM56-5B |
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MLW |
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V2500-A5 |
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5500 |
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Typical landing weight |
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(m) |
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(ft) |
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2000 ft |
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distance |
1500 |
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distance |
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Sea level |
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4500 |
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Landing |
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Landing |
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1250 |
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3500 |
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1000 |
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750 |
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2500 |
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60 |
62 |
64 |
66 |
68 |
70 |
72 |
74 |
76 |
78 |
80 |
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Landing weight (t) |
Page 50 |
May 2009 |
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Assumptions
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Performance assumptions (“typical airline” rules)
Weight standards: |
OWEs are to “typical airline” assumptions including an allowance for |
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cabin changes and option selection. Cabin layouts are as shown in |
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the cabin section. |
Flight profile: |
En-route profile includes engine start and taxi-out, take-off, climb, |
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cruise, descent, approach, landing and taxi-in. Sector distance |
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comprises the climb, cruise and descent phases. |
Payloads: |
Passenger + baggage weights are 90.7kg / 200lb. Volumetric |
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payloads assume an average baggage volume of 3.0ft3 per |
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passenger, a bulk and ULD loadability of 85% and cargo with an |
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average density of 10ft3. |
Page 51 |
May 2009 |
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
This document and all information contained herein is the sole property of AIRBUS S.A.S.. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied.
The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof.
AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.
AIRBUS S.A.S.
31707 BLAGNAC CEDEX, FRANCE
REFERENCE CSMS_PR0907198_V1
May 2009
PRINTED IN FRANCE
© AIRBUS S.A.S. 2009
ALL RIGHTS RESERVED
Page 52 |
May 2009 |