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WG44-SC217 Subgroup Content
Airbus Supplemental Needs
Presented by
André Bourdais
AIRBUS
Navigation R&T Leader
Content - Airbus Supplemental Needs 19/05/2009 Page 15
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Content –
Airbus Supplemental Needs
• In addition to Honeywell proposals and outcomes of “content” subgroup,
Airbus identifies the potential following needs:
Runway vertical profile
Surface type after shoulders
Identification of rubber presence on runway parts (to cover some
NOTAMs)
Turnpads suitability for limiting aircraft (such as A340-600)
Culverts with max allowed aircraft weight
ILS interferences areas
• All these needs are not certain but Airbus would like to know if it
could be captured in an Airport Database, as it might be useful for
some applications.
Content - Airbus Supplemental Needs 19/05/2009 Page 16
© 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.
10-11-12-13 September 2002-Morocco ARAB INSTRUMENT PROCEDURE DESIGN SEMINAR
Navigation & flight planning
by FMS-equipped aircraft
AI/EE-A 441.0144/01
Table of contents
P.3 Navigation & flight management
P.4An overview of aircraft avionics
P.5GPS PRIMARY navigation
P.8RNP navigation
P.10 Flight management
P.11 Flight planning
P.12 Vertical navigation
P.13 Navigation database : ARINC 424 format
P.14 Path terminator concept
P.15 IF leg type
P.16 TF leg type
P.17 RF leg type (new leg type)
P.18 CF leg type
P.19 DF leg type
P.20 FA leg type
P.21 FC leg type
P.22 FD leg type
P.23 FM leg type
P.24 CA leg type
P.25 CD leg type
P.26 CI leg type
P.27 CR leg type
P.28 AF leg type
P.29 VA leg type
P.30 VD leg type
P.31 VI leg type
P.32 VM leg type
P.33 VR leg type
P.34 PI leg type
P.35 HA, HF, HM leg types
P.36 ARINC 424 leg transitions
P.37 Navigation database related issues
P.38 Compatibility...
P.39 Production process
P.40 Some top level issues
P.44 Recommendations
P.45 Issues summary
P.46 Short term
P.52 Medium term
P.54 Longer term
10-11-12-13 September 2002-Morocco ARAB INSTRUMENT PROCEDURE DESIGN SEMINAR
Navigation & flight management
An overview of aircraft avionics ...
Modern avionics have considerably improved flight
safety on non-precision approaches :
accurate position (RNP 0.3)
flight plan display on EFIS
reference approach path
automated lateral guidance
automated vertical guidance
ground proximity warning system (GPWS)
terrain display on EFIS (EGPWS)
terrain clearance floor warnings (EGPWS)
An overview of aircraft avionics ...
700’
500’ AGL AGL
5 NM 12 NM15 NM
3 degrees
GPS PRIMARY navigation
AIRBUS is promoting GPS PRIMARY navigation
All new A318/A319/A320/A321/A330/A340 production
aircraft are fitted with GPS PRIMARY capable equipment
Ground navaids are only used as a backup
VOR, DME
ADF is not used for navigation
only for procedural navigation check
Hybrid (A320 family & A340 family)
AIRBUS system GPS architecture
MMR
or
GPSSU
ADIRS FMS
IRS position
GPIRS position
GPS raw data
GPS position FMS position
EGPWS
Autonomous (A300-600/A310 family, retrofit solution
for A320 family with older ADIRS)
AIRBUS system GPS architecture
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