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TitleA320 Review Book
File Size5.0 MB
Total Pages134
Document Text Contents
Page 1

A319, AA320, AA321
Oral SSystem RReview©

trs-digital-presentation™
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legal statement . . . . . . . . . . . . . . .p 2
review book . . . . . . . . . . . .p’s 3 - 128
index . . . . . . . . . . . . . . . p’s 129 - 132
other products . . . . . . . . . . .133 - 134

Page 2

trs-digital-presentation
A319, A320, A321 System Review©

TM

Aug 2004page 2

COPYRIGHT NOTICE
Copyright 2004 Tom Sceurman d/b/a trs-digital-presentation™. All rights reserved.
Permission to use, duplicate or copy and distribute this document and/or any includ-
ed text or graphics or Compact Disc content contained in this publication is forbid-
den without the express written permission of the author.

TRADEMARKS
trs-digital-presentation and digitial-presentation.net are trademarks owned by Tom
Sceurman. All rights reserved.

DISCLAIMER
This guide is for familiarization purposes ONLY. This guide is not approved
by the aircraft manufacturer or the FAA/CAA/JAA or Transport Canada and does
not supercede, replace, or overrule the aircraft manufacturer's AOM or FCOM.
Tom Sceurman d/b/a trs-digital-presentation™ makes NO WARRANTY or REPRE-
SENTATIONS about the suitability of the information contained in the documents or
attached Compact Discs and related graphics/text published in this guide.

All such documents and related graphics are provided "AS IS" without warranty of
any kind. Tom Sceurman d/b/a trs-digital-presentation™ hereby disclaims all war-
ranties and conditions with regard to this information including all implied warranties
and conditions of merchantability, fitness for a particular purpose and non- infringe-
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any special, indirect or consequential damages or any damages what so ever result-
ing from loss of use, data or profits, whether in an action of contract, negligence or
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information available from this Documents contents.

The documents and related graphics published in this guide could include technical
inaccuracies or typographical errors. Changes are periodically added to the informa-
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any time.

Page 67

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A319, A320, A321 System Review©

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Aug 2004 page 67

PFD SPEED DATA

VMAXVMAX

VLSVLS
ALPHAALPHA PROT SPEEDPROT SPEED

ALPHAALPHA MAX SPEEDMAX SPEED

VFE NEXTVFE NEXT - VFE corresponding to next flap
lever position when aircraft below FL150 or
FL200.

NOTE: see next page for Symbology & Definitions.

ECON SPEED RANGEECON SPEED RANGE

ENG OUT OPERAENG OUT OPERATING SPEED INTING SPEED IN
CLEAN CONFIGURACLEAN CONFIGURATIONTION
AIRSPEED REF AIRSPEED REF AND SCALEAND SCALE

MIN SLAMIN SLAT RETRACT SPEEDT RETRACT SPEED
MIN FLAPMIN FLAP RETRACT SPEEDRETRACT SPEED

TTARGET ARGET AIRSPEEDAIRSPEED
DECISION SPEED (V1)DECISION SPEED (V1)

MACH NUMBERMACH NUMBER

Page 68

trs-digital-presentation
A319, A320, A321 System Review©

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Aug 2004page 68

SYMBOLOGY & DEFINITIONS:
Vs - reference stalling speed (Equal to Vs1g).

VMCG - minimum control speed on ground from which a sudden failure of
the critical engine can be controlled by use of primary flight con-
trols only, the other engine remaining at TO power.

V1 - represented by “1” on airspeed scale (or (V1 value when out of
range). Manually inserted by the crew through the MCDU.

Vr - manually inserted by the crew through the
MCDU.

V2 - represented by the SPEED SELECT symbol on airspeed scale.
- minimum value for V2 is equal to 1.13 Vs of the corresponding

configuration.
- manually inserted by the crew through the MCDU.

VMCA - minimum controls speed in flight at which aircraft can be control-
led with 5° max bank, in case of failure of one engine, the other
engine remaining at TO power (TO flaps setting, gear retracted).

F - is the minimum speed at which the flaps may be retracted to
CONF 1. Represented by “F” on airspeed scale. It is equal to
about 1.23 Vs of CONFIGURATION 1+F.

S - is the minimum speed at which the slats may be retracted to
CONF 0. Representated by “S” on airspeed scale. It is equal to
about 1.29 Vs of CLEAN CONFIGURATION.

O - ENGINE OUT OPERATING (Green Dot) speed (Best lift to drag
ration speed or DRIFT DOWN SPEED) in clean configuration. It
corresponds also the the FINAL TAKEOFF SPEED. It is calcul-
ated by FACs and represents:
• below 20,000 ft:

Green dot = 2 x weight (t) +80
• above 20,000 ft. add 1 kt per 1,000 ft.

VFE - max speed for each flaps and/or slats configuration.

VREF - reference speed used for a normal final approach, it is equal to
1.23 Vs of configuration “FULL”

- represented on the MCDU APP page.

Page 133

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A319, A320, A321 System Review©

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Aug 2004 page 133

Page 134

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A319, A320, A321 System Review©

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Aug 2004page 134

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