EUROPEAN ORGANISATION
FOR THE SAFETY OF AIR NAVIGATION
EUROCONTROL
EUROCONTROL EXPERIMENTAL CENTRE
MODE-S SPECIFIC SERVICES
INSTALLATION ON A300/600ST
BELUGA AIRCRAFT
EEC NoteNo. 20/98
EEC Task C07
EATCHIP Task SUR-3-E1
Issued: September 1998
The information contained in this document is the property of the EUROCONTROL Agency and no part should be reproduced
in any form without the Agency’s permission.
The views expressed herein do not necessarily reflect the official views or policy of the Agency.
REPORT DOCUMENTATION PAGE
Reference:
EEC Note No. 20/98
Security Classification:
Unclassified
Originator:
EEC - COM
(Communications)
Originator (Corporate Author) Name/Location:
EUROCONTROL Experimental Centre
B.P.15
F - 91222 Brétigny-sur-Orge CEDEX
FRANCE
Telephone : +33 (0)1 69 88 75 00
Sponsor:
EATCHIP Development Directorate
DED.3
Sponsor (Contract Authority) Name/Location:
EUROCONTROL Agency
Rue de la Fusée, 96
B -1130 BRUXELLES
Telephone : +32 2 729 9011
TITLE:
MODE-S SPECIFIC SERVICES INSTALLATION ON A300/600ST BELUGA
Author
P.Hunt
EATCHIP Task
Specification
SUR-3-E1
Date
Pages
Figures
Tables
Appendix
09/98
iv + 77
5
-
6
EEC Task No.
References
Task No. Sponsor
Period
SUR-3-E1
04/97 to 01/98
CNS-C07
Distribution Statement:
(a) Controlled by:
Head of COM
(b) Special Limitations: None
(c) Copy to NTIS:
YES / NO
Descriptors (keywords):
“Mode-S Specific Services” IIMSES DAP “Data Link” ModeS
Abstract:
This note describes the Mode-S Specific Services Installation on the Airbus Inter Transport A300/600ST
Beluga aircraft. This installation enables the enhanced surveillance ModeS functionality to be validated.
This document has been collated by mechanical means. Should there be missing pages, please report to:
EUROCONTROL Experimental Centre
Publications Office
B.P. 15
91222 - BRETIGNY-SUR-ORGE CEDEX
France
EEC Note No. 20/98
EEC Task No. C07
Issued : September 1998
MODE-S SPECIFIC SERVICES
INSTALLATION ON A300/600ST
BELUGA AIRCRAFT
by
Patrick HUNT
Summary
This note describes the Mode-S Specific Services Installation on the Airbus Inter Transport A300/600ST
Beluga aircraft. This installation enables the enhanced surveillance ModeS functionality to be validated.
iii
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
TABLE OF CONTENTS
1.
INTRODUCTION.............................................................................................................................................. 1
2.
HARDWARE...................................................................................................................................................... 2
3.
SOFTWARE....................................................................................................................................................... 3
4.
SYSTEM TESTING........................................................................................................................................... 4
4.1.
4.2.
5.
INITIAL GROUND TESTS ................................................................................................................................. 4
FLIGHT TEST ................................................................................................................................................. 4
CONCLUSIONS ................................................................................................................................................ 5
FIGURE 1 : SCHEMATIC DIAGRAM - PRINCIPLE MODES INSTALLATION.......................................... 6
FIGURE 2 : SCHEMATIC DIAGRAM - SHEET 2 .............................................................................................. 7
FIGURE 3 : BELUGA UNDER TEST..................................................................................................................... 8
FIGURE 4 : BELUGA UNDER TEST..................................................................................................................... 9
FIGURE 5 : GICB CONTENTS AVAILABLE ON BELUGA ( EXAMPLE) .................................................. 10
APPENDIX A - GROUND TEST REPORT .................................................................................................... 12
APPENDIX B - FLIGHT TEST RESULTS ..................................................................................................... 19
APPENDIX C - BASIC SYSTEM TEST FOR GROUND CREW ................................................................ 29
APPENDIX D - FLIGHT TEST SCENARIO .................................................................................................. 31
APPENDIX E - DETAILS OF GICB CONTENTS......................................................................................... 37
APPENDIX F - BDS ALLOCATION TABLE FOR A300 BELUGA ........................................................... 66
iv
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
1.
INTRODUCTION
In the context of the Eurocontrol (Initial Implementation of Mode S in Europe) IIMSES
programme, Eurocontrol is equipping several aircraft with Mode S Specific Services
(MSS) capabilities. This will assist in the validation of the enhanced surveillance
capability of the (Pre-Operational Experimental ModeS) POEMS radars during the preoperational phase.
This note describes the Mode S installation on the Airbus Inter Transport A300/600ST
Beluga aircraft registration F-GSTA. This aircraft was chosen because it flies mainly in
or near the core area of Europe and also has less installation constraints than a
commercial passenger carrying aircraft.
The installation conforms as far as is possible to the “Mode S Specific Services Manual”
ICAO Document 9688-AN/952.
As no commercially certified ADLP is yet available, the aircraft is fitted with the
Eurocontrol DLPU which has been programmed to provide the MSS defined data
formats for GICB protocols where possible. The previous Eurocontrol defined data
formats have also been used where there is no conflict with the new MSS definitions.
At the present time this installation enables only the enhanced surveillance capability of
the MSS, the downlink aircraft parameters (DAP) may be extracted by the POEMS
ground stations.
At a later date an ADLP could be fitted in place of the DLPU giving full MSS and ATN
services.
1
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
2.
HARDWARE
Eurocontrol (EEC) provided the following hardware for installation in the aircraft :
1 ADLP Type NLR Model C/1/3
1 Transponder Type Rockwell Collins TPR900 Level 3
1 Cockpit Printer Type Bendix PTR 45B
1 DLT Type EEC
plus avionic equipment support trays and connectors.
The aircraft cabling was made by Airbus Inter Transport under a Eurocontrol contract.
A schematic diagram shows the essential parts of the Beluga data link wiring.
2
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
3.
SOFTWARE
The DLPU software provided by NLR enables aircraft data processing for enhanced
surveillance and is the same in each DLPU but because different aircraft types may
have different data bus configurations, a data allocation table is defined for each
different aircraft type. The aircraft type is hard wired on the aircraft so the correct
allocation table is selected automatically by the DLPU.
The allocation table for the Beluga is shown in appendix F.
3
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
4.
SYSTEM TESTING
The Mode S data link and MSS system were tested using the Mode S Test Bench [1]
and this was made in two stages.
4.1.
Initial Ground Tests
The initial ground test was made at Toulouse Blagnac in July 1997 in the Airbus Inter
Transport hangar. Using the Test Bench, messages were sent to and received from the
aircraft. All possible aircraft parameters were extracted and checked and recordings
made for reference and further investigation when necessary. See appendix Appendix A
for details.
4.2.
Flight Test
A flight test was made in December 1997 at Toulouse Blagnac. During this test aircraft
parameters which could not be checked on the ground were verified and also non
interference tests with other aircraft systems were carried out.
For this purpose the aircraft was interrogated by the Mode S test bench sited on the
ground at Toulouse Airport during different flight phases.
Mode S data link messages were sent to the ground throughout the flight by the
onboard operator.
The rate of Mode S uplink data link messages was augmented by sending bursts of
messages that would be rejected by the onboard system, as well as some valid data
link messages that would be processed by the system.
In this way the flow of 1090/1030 MHz data was greatly increased in an attempt to
perturb the other aircraft systems but on the other hand the Mode S data link system
was not overloaded with to many valid messages.
These tests are described in more detail in Appendices A and B.
4
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
5.
CONCLUSIONS
The installed system is now ready for operational use.
As soon as the agreement between Eurocontrol and Airbus Inter Transport concerning
the confidentiality and the range of aircraft parameters to be exploited during the
foreseen trials is signed. The system may be used operationally.
5
Aircraft Ident
from FMS (Beluga)
TP-6A
TP-2A
TP-6B
TP-2B
A
B
DATA LINK IN
A
Screen
B
DATA LINK OUT
MP-5E
MP-5F
Screen
TP-2C
TP-2D
A
COMMC/D DATA IN
B
TP-2F
A
COMMC/D DATA OUT
B
Screen
BP-8
BP-11
Signal Ground
115v hot
115v cold
Chassis Ground
B
A
G15
B
E6
E15
Screen
CHANNEL 1
-
IRS 1
High Speed
F7
G7
F9
A
E7
G9
B
J6
E9
Screen
CHANNEL 2
- NC
High Speed
H6
F1
F10
G10
G1
E10
A
CHANNEL 3 - FCU
B
AIRCRAFT
Low Speed
Screen
E1
DATA
INPUTS
Signal Ground
Chassis Ground
ARINC 429
XPDR
A
Aircraft Ident
F15
G6
K6
Screen
TP-2E
F6
L
P
A
M
R
B
A
J9
K9
Screen
H9
C
D
H
A
V
J11
B
W
A
B
E2
Screen
J10
A
K10
B
H10
Screen
CHANNEL 4 - NC
High Speed
K11
Screen
DLT
F2
G2
H11
Connector SOURIAU
CHANNEL 5 - ADC 1I
Low Speed
851 06RC 16-26
E
A
J15
J13
B
A
F
K15
K13
B
H15
H13
Screen
Screen
115v hot
R
115v cold
N
T
A
L
U
B
Chassis Ground
CHANNEL 6
J14
J7
A
K14
K7
B
H14
H7
Screen
Connector ITT CANNON
J1
A
KPSE 06F20-415
K1
B
H1
Screen
Screen
- FMC 1
Low Speed
CHANNEL 7 - EFIS 1 - SGU
Low Speed
PRINTER
File Transfer Input
A
F5
J2
A
B
G5
E5
K2
B
H2
Screen
A
F3
B
J5
K5
A
G3
E3
H5
Screen
Screen
File Transfer Output
CHANNEL 8 - NC
Screen
Low Speed
CHANNEL 9 - NC
CHANNEL
B
10 - NC
Low Speed
Low Speed
EUROCONTROL Experimental Centre
BP 15
Title:
F91222 Br‚tigny - Cedex
DLPU-C2 CABLING DIAGRAM
for BELUGA
BLOCK A
Diagram 1 Sheet 1 file beluga.ds4
SIZE
CODE
A4
DLPU
Figure 1 : Schematic diagram - principle ModeS installation
6
Date:
NUMBER
REV
D
PH-001
15/12/97
Sheet
1
of
2
Bit 0 - lsb
Bit 1
SYSTEM
Bit 2
ADDRESS
Bit 3
LABEL 05
Bit4
Bit 5
A6
A11
B6
B11
K6
K11
J6
J11
A7
A13
B7
B13
K7
K13
J7
J13
Bit 0 - lsb
Bit 1
AIRCRAFT TYPE 6
Bit 2
Bit 3
- msb
A9
B9
K9
A14
J9
B14
No BDS20 Generation
A10
Bit 6
Bit 7 - msb
B10
K14
K10
J14
Dual Channel Transponder
J10
STRAPS
Connected = 0
BLOCK B
Open
=1
To be programmed according to aircraft
configuration
115v hot
4
6
115v cold
10
Chassis Ground
BLOCK C
DLPU
EUROCONTROL Experimental Centre
BP 15
F91222 Br‚tigny - Cedex
Title:
DLPU-C2 CABLING DIAGRAM
SIZE
CODE
A4
Diagram 1 Sheet 2 file beluga.ds4
Date:
Figure 2 : Schematic diagram - Sheet 2
7
NUMBER
REV
PH-001
15/12/97
Sheet
D
2
of
2
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
Figure 3 : BELUGA under Test
8
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
Figure 4 : BELUGA under Test
9
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
Figure 5 : GICB CONTENTS AVAILABLE ON BELUGA ( Example)
GICB
Contents
10
20
30
Capability
Fight ID
TCAS
10
20
GICB
40
Parameter
Sel.alt
992
Bearing to
-1.03
Windspd
20 kt
SAT
25
Roll angl
0
Lat.
Parameter
Sel.alt.rate
100 ft/min
Time to go
10 min
Wind dir.
55 deg
Av. press
29.79 hp
True track
24.69
Long.
43°37.4377N
1°22.8506E
70
Contents
Aircraft
Intention
Next wypt
details
Meteo.
report
Met.hazrd
report
Track &
turn rpt.
Position
rpt.
Air ref.
state vec.
Heading
& spd rpt
Intent 1
80
Intent 2
90
Intent 3
A0
Deviation
report
Speeds
report
Altitudes
report
Meteo.
report
Air ref.
state vect.
Waypoint
info.
Mag.hd
27.422
Mag.head
27.422
Sel.alt.
992
Sel.Air spd
ncd
Sel.mach
ncd
X-trk error
ncd
CAS
ncd
Radio ht.
2
Roll angl
0
Mag.head
27.42
Bear. wpt.
-136.99
IAS
ncd
IAS
ncd
Sel.head
61.875
Sel.alt.rt
ncd
Sel.alt.rt
ncd
Vert.dev
ncd
TAS
ncd
Stat.press
950.75
Inert.VV
-132
TAS
100 kt
Time to go
10 min
43
44
45
50
51
53
60
B0
C0
71
21
31
Data
04
T
AE
30
82
G
B
9
not implemented on this aircraft
Parameter
sel.mag.hd
61.875(62)
Dist.to go
2.3
SAT
26
Radio ht
2
Gr’nd spd.
0
Altitude
192
Mach
ncd
Mach
ncd
Discretes
0000
Sel.alt
992
Sel.alt
992
Accel.nrm
-0.0169
Mach
ncd
Altitude
188
Wind spd
ncd
Inertial v.v.
0
Dist.to go
2.3 nm
10
Parameter
sel airspd
100
05
4
Parameter
06
0
Parameter
Av. press.
1014 hp
Trk ang. rt
-0.03
TAS
100 kt
TAS
ncd
Baro.alt
-3.2
Discretes
0040
Nav.dscrt1
0000
Nav.dscrt1
0000
Alt.rate
-132
Inert. VV
-32
Nav.dscrt2
0000
Nav.dscrt2
0000
Mag.head
27.422
Wind angl.
ncd
SAT
26
SAT
26
Accel.nrm
0
Accel.nrm
0
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
61
24
17
27
2A
D0
D1
D2
GMT
report
Weights
report
Engine 1
report
Engine 2
report
Radio
frequency
Turn
report 1
Turn
UTC
NA
C of G
ncd
N1
NA
N1
NA
VHF 1
NA
Sel.course
ncd
Roll angle
Flight Nr
ncd
Weight
ncd
Fuel flow
NA
Fuel flow
NA
VHF 2
NA
Sel.head
61.6
Roll rate
GMT
NA
TAT
25
TAT
25
SAT
25
SAT
25
Sel.alt.
992
Trk.ang.rt.
Desrd.trk
NA
Mag.head
Inert.VV
-32
X-trk.accel
X-head ac.
report 2
Turn
report 3
0
Roll angle
0
0
Roll rate
0
-0.25
Trk.angl.rt.
-0.25
27.42
Trk.angl.
25.05
0.5g
X-trk.accel
0.5g
NA
X-head ac.
NA
Note: NA = Data not available on this aircraft
ncd = No computed data on this test
11
APPENDIX A - GROUND TEST REPORT
MODE-S DATA LINK & SPECIFIC SERVICES INSTALLATION
ON
A300/600 BELUGA
AT
TOULOUSE BLAGNAC
15 JULY 1997
Made by P.Hunt / P.Brun
12
Mode S Airborne Equipment details
Equipment
Manufacturer
Type
Transponder
DLPU
DLT
Printer
Collins
NLR
EEC
Bendix
TPR 900
C/1/3
Serial Nr.
617
001
002
PTR 45B
Mode S Test Equipment
Dassault Electronique Mode S Test Bench + PC driver
PC terminal emulator for DLPU programming and control
Aircraft details
Type: A300/608ST Beluga
Wing Nr.
F-GSTA
Operator: Airbus Inter Transport
General Remarks
These tests were carried out on the ground with the aircraft
All test results are recorded on the PC hard disk whenever possible.
13
1. Data Link Equipment Initial Installation Tests
Equipment
Test
Pass
Transponder
Panel Test
√
DLPU
Front panel lights
Log file
√
√
DLT
Lighting
Dim
Initial message on screen
Printer
Panel Test
Channel 1 active
Paper full
Fail
√
not tested *
√
√
√
√
* due to cabling work on aircraft, the dim function was not able to be tested
2. Mode S address
From squitter or DF 11 reply
3
Correct :
9
Address hexedecimal
4
A
6
0
F
YES
14
-
Decoded Tail number
G
S
T
A
3. DLPU Arinc Channels and labels
Check presence of labels on each channel with PC plugged into DLPU.
Channel 1
Channel 3
Channel 5
Channel 6
Channel 7
IRS 1
FCU
ADC 1
FMC 1
SGU EFIS 1
Label
OK
Label
OK
Label
OK
Label
OK
Label
OK
150
310
311
312
313
314
315
316
317
320
321
322
323
324
325
333
335
362
363
364
365
366
367
NCD
√
√
√
√
√
NCD
NCD
√
√
√
√
√
√
√
√
√
√
√
√
√
√
√
103
106
102
101
104
270
271
272
273
274
275
√
NCD
√
√
NCD
NCD
NCD
X
X
NCD
NCD
203
204
220
212
206
241
221
205
213
211
242
210
217
√
√
√
√
NCD
NCD
NCD
NCD
√
√
√
NCD
√
001
002
012
066
075
103
106
115
116
117
233
234
235
236
261
310
311
343
NCD
NCD
NCD
NCD
NCD
NCD
√
NCD
NCD
NCD
NCD
NCD
NCD
NCD
NCD
√
√
NCD
312
320
164
325
317
313
314
270
271
206
203
221
205
211
√
√
√
√
√
√
√
NCD
NCD
NCD
√
√
√
√
Notes:
NCD = No Computed Data ( which means the label is present on the bus
but because the aircraft is not in the correct flight phase the data cannot be computed.
Labels 272, 273 were not present, these are discrete data not used in this application
Label 150 (UTC) is not available on this aircraft, as no GPS fitted.
Labels 315,316 are NCD until TAS > 100 kts
Labels 321,322 = 0 until ground speed > 50 kts.
labels 206,241,221,205,210 are NCD until CAS > 30 or 60 kts
15
4. Downlink Tests
4.1 GICB Extract and verify the contents
GICB
Contents
10
20
30
Capability
Fight ID
TCAS
10
20
GICB
40
Parameter
Sel.alt
992 (1000)
Bearing to
-1.03
Windspd
ncd
SAT
25
Roll angl
0
Lat.
Parameter
Sel.alt.rate
ncd
Time to go
ncd
Wind dir.
ncd
Av. press
29.79 hp
True track
24.69
Long.
43°37.4377N
1°22.8506E
70
Contents
Aircraft
Intention
Next wypt
details
Meteo.
report
Met.hazrd
report
Track &
turn rpt.
Position
rpt.
Air ref.
state vec.
Heading
& spd rpt
Intent 1
80
Intent 2
90
Intent 3
A0
Deviation
report
Speeds
report
Altitudes
report
Meteo.
report
Air ref.
state vect.
Waypoint
info.
Waypoint
Identifier
Mag.hd
27.422
Mag.head
27.422
Sel.alt.
992
Sel.Air spd
ncd
Sel.mach
ncd
X-trk error
ncd
CAS
ncd
Radio ht.
2
Roll angl
0
Mag.head
27.42
Bear. wpt.
-136.99
Act.wpt1
NA
IAS
ncd
IAS
ncd
Sel.head
61.875
Sel.alt.rt
ncd
Sel.alt.rt
ncd
Vert.dev
ncd
TAS
ncd
Stat.press
950.75
Inert.VV
-132
TAS
ncd
Time to go
ncd
Act.wpt2
NA
43
44
45
50
51
53
60
B0
C0
71
21
31
41
Data
04
T
AE
30
82
G
B
9
not implemented on this aircraft
Parameter
sel.mag.hd
61.875(62)
Dist.to go
2.3
SAT
26
Radio ht
2
Gr’nd spd.
0
Altitude
192
Mach
ncd
Mach
ncd
Discretes
0000
Sel.alt
992
Sel.alt
992
Accel.nrm
-0.0169
Mach
ncd
Altitude
188
Wind spd
ncd
Inert.VV
0
Dist.to go
2.3 nm
Des.track
NA
16
Parameter
sel airspd
100
00
4
Parameter
00
0
Parameter
Av. press.
29.79 hp
Trk ang. rt
-0.03
TAS
ncd
TAS
ncd
Baro.alt
-3.2
Discretes
0040
Nav.dscrt1
0000
Nav.dscrt1
0000
Alt.rate
-132
Inert. VV
-32
Nav.dscrt2
0000
Nav.dscrt2
0000
Mag.head
27.422
Wind angl.
ncd
SAT
26
SAT
26
Accel.nrm
0
Accel.nrm
0
61
24
17
27
2A
D0
D1
D2
GMT
report
Weights
report
Engine 1
report
Engine 2
report
Radio
frequency
Turn
report 1
Turn
report 2
Turn
report 3
UTC
NA
C of G
ncd
N1
NA
N1
NA
VHF 1
NA
Sel.course
ncd
Roll angle
0
Roll angle
0
Flight Nr
ncd
Weight
ncd
Fuel flow
NA
Fuel flow
NA
VHF 2
NA
Sel.head
61.6
Roll rate
0
Roll rate
0
GMT
NA
TAT
25
TAT
25
SAT
25
SAT
25
Sel.alt.
992
Trk.ang.rt.
-0.25
Trk.angl.rt.
-0.25
Desrd.trk
NA
Mag.head
27.42
Trk.angl.
25.05
Inert.VV
-32
X-trk.accel
0.5g
X-trk.accel
0.5g
X-head ac.
NA
X-head ac.
NA
Note : NA = Not Available ( On this installation )
ncd = no computed data ( Under ground test conditions )
Values in brackets i.e.(1000) were the actual values set on the aeroplane. Note that the values
extracted maybe slightly different due to the precision defined in the parameter tables of the DLPU.
Example: If 1000 ft is set on the aircraft’s selected altitude as the resolution of this parameter is in
16 ft units when transferred to the transponder, the extracted value will be 992 ft.
4.2 Broadcast Messages
Change of Flight ID
Change of Capability Report
- PASS
- FAIL*
* The change of capability was broadcast permamently. This appears to be a Collins
transponder problem. The transponder thinks that there is a change in the capability report
each time the DLPU sends a capability report ( set at 5 seconds in this test).
Action to be taken : Contact Collins about this function.
Solutions for this installation:
Either : Inhibit DLPU update of Capability report ( present situation)
Or
: The DLPU updates the capability report once evry 15 minutes (say) so that the
broadcast only occurs once evry 15 minutes during 18 seconds.
Note: Capability report when only Collins updates ( No DLPU update ) is as follows
10 00 00 00 80 00 00 (Hex) The bit set indicates Aircraft Identification capability.
4.3 Comm-D Messages
Not applicable on this installation
17
4.4 Aquisition Squitter
Diversity fitted
- YES
Top antenna
Bottom antenna
-NOT TESTED*
-PASS
RATE:
RATE: 0.5 Hz
In the hangar the top antenna was not visible, this test could be done outside with the bottom
antenna masked.
4.5 Send Comm-B message with DLT
Read with bench
-PASS
4.6 Send Comm-D message with DLT
Not applicable on this installation
5. Data Link Uplink Tests
5.1 Send Comm-A test messages with bench
Messages received on printer
PASS
5.2 Send Comm-C messages with bench
Messages received on printer
FAIL*
The transfer of Comm C messages was not possible.
This was probably due to the aircraft being in the hangar. The 16 segment Comm C message
is the most demanding test in these conditions because it is a series of 16 long contiguous
segments of 112 bits with only 50 µsec between each segment, the chances of this getting
through to the transponder without reflections and/or saturation are quite small under these
conditions.
Action to be taken:
1) Test this function in the laboratory with a TPR 900.
2) Test this function outside or in flight at a later date.
6.0 Conclusions:
1) The electrical installation was correct.
2) The On-Board Mode S equipment initialised correctly.
3) The aircraft parameters that could be extracted were correct.
4) The parameters flagged by the aircraft systems as “no computed data” will have to be
verified during roll or flight tests.
5) Short Mode S data link messages were exchanged in uplink and downlink.
6) Long Mode S data link messages will have to be verified during roll or flight tests.
Attachment: Printout showing Printer Test Report and Uplink short messages.
18
APPENDIX B - FLIGHT TEST RESULTS
MODE-S DATA LINK & SPECIFIC SERVICES INSTALLATION
ON
A300/600 BELUGA
AT
TOULOUSE BLAGNAC
Monday, 08 December, 1997
19
Mode S Airborne Equipment details
Equipment
Manufacturer
Type
Serial Nr.
Transponder
DLPU
DLT
Printer
Collins
NLR
EEC
Bendix
TPR 900
C/1/3
617
001
002
PTR 45B
Mode S Test Equipment
Dassault Electronique Mode S Test Bench + PC driver
PC terminal emulator for DLPU programming and control
Aircraft details
Type: A300/608ST Beluga
Wing Nr.
F-GSTA
Operator: Airbus Transport International
General Remarks
All test results are recorded on the PC hard disk whenever possible.
20
1. Data Link Equipment Initial Installation Tests
Equipment
Test
Pass
Transponder
Panel Test
YES
DLPU
Front panel lights
Log file
YES
YES
DLT
Lighting
Dim
Initial message on screen
YES
YES
Panel Test
Channel 1 active
Paper full
YES
YES
80%
Printer
Fail
2. Mode S address
From squitter or DF 11 reply
3
Correct :
Address hexedecimal
9
4
A
6
0
F
YES
21
Decoded Tail number
G
S
T
A
3. DLPU Arinc Channels and labels
Check presence of labels on each channel with PC plugged into DLPU.
Channel 1
Channel 3
Channel 5
Channel 6
Channel 7
IRS 1
FCU
ADC 1
FMC 1
SGU EFIS 1
Label
150
310
311
312
313
314
315
316
317
320
321
322
323
324
325
333
335
362
363
364
365
366
367
OK
Label
103
106
102
101
104
270
271
272
273
274
275
OK
Label
OK
Label
203
204
220
212
206
241
221
205
213
211
242
210
217
001
002
012
066
075
103
106
115
116
117
233
234
235
236
261
310
311
343
Not enough time during flight to make this test.
22
OK
Label
312
320
164
325
317
313
314
270
271
206
203
221
205
211
OK
4. Downlink Tests
4.1 GICB Extract and verify the contents
GICB
Contents
10*
Capability
10
00
00
00
80
10
Capability
10
04
AE
30
80
20
Fight ID
20
B
G
A
9
1
30
TCAS
not implemented on this aircraft
* capability initially inserted by TPR 900 ( overwritten later by DLPU )
GICB
40
43
44
45
50
51
53
Contents
Aircraft
Intention
Next wypt
details
Meteo.
report
Met.hazrd
report
Track &
turn rpt.
Position
rpt.
70
Air ref.
state vec.
Heading
& spd rpt
Intent 1
80
Intent 2
90
Intent 3
A0
Deviation
report
Speeds
report
Altitudes
report
GMT
report
Meteo.
report
Air ref.
state vect.
60
B0
C0
61
71
21
Parameter
Sel.alt
26000
Bearing to
-36.21
Windspd
34
SAT
Roll angl
-0.35
Lat.
43N16.503
1
Parameter
Sel.alt.rate
Time to go
06.30
Wind dir.
-104
Av. press
339 hPa
True track
-91.4
Long.
1E29.9778
Mag.hd
-90.176
Mag.head
-90.176
Sel.alt.
26000
Sel.Air spd
IAS
256
CAS
256
Sel.head
-90.00
Sel.alt.rt
Sel.mach
0.600
X-trk error
0.008
CAS
244
Radio ht.
Sel.alt.rt
UTC
Roll angl
0
Mag.head
-90.18
Vert.dev
158
TAS
358
Stat.press
339.5
Flight Nr.
9194
Inert.V.V.
-132
TAS
358
Parameter
sel.mag.hd
-90.00
Dist.to go
35.8
SAT
Parameter
sel airspd
242.5
00
00
9
Parameter
00
00
4
Parameter
Av. press.
339 hPa
Radio ht
Gr’nd spd.
338
Altitude
24248
Trk ang. rt
0
TAS
372
Mach
0.632
Mach
0.624
Discretes
001E
Sel.alt
26000
Sel.alt
26000
Accel.nrm
0.094
Mach
0.603
Altitude
26029
GMT
NA
Wind spd
35
Inert.VV
-64
TAS
372
Baro.alt
-384
Discretes
0040
Discretes
1100
Discretes
1100
Alt.rate
924
Inert. v.v.
32
23
Discretes
000
Discretes
000
Mag.head
-90.176
Wind angl.
-104
SAT
-40.5
SAT
-40
Accel.nrm
0.1g
Accel.nrm
31
41
51
Waypoint
info.
Waypoint
Identifier
Position
report
Bear. wpt.
-80.33
Act.wpt1
NA
Lat.
43N29.954
5
Time to go
5.9
Act.wpt2
NA
Long.
1E34.4891
Dist.to go
31.60
Des.track
NA
Altitude
4040
24
Weights
C of G
Weight
report
25.3%
236800 lbs
17
Engine 1
N1 Target
Fuel flow
TAT
report
NA
-3
27
Engine 2
N1 Target
Fuel flow
TAT
6eport
NA
-3
2A
Radio
VHF 1
VHF 2
frequency
NA
NA
D0
Turn
Sel.course
Sel.head
Sel.alt.
report 1
NA
-89.60
26000
D1
Turn
Roll angle
Roll rate
Trk.ang.rt.
report 2
-0.70
-1.0
-0.25
D2
Turn
Roll angle
Roll rate
Trk.angl.rt.
report 3
-0.70
-1.0
-0.25
NA = Parameter Not Available on this installation
SAT
-16
SAT
-16
Desrd.trk
NA
Mag.head
-90.0
Trk.angl.
-90.0
Inert.V.V.
-32
X-trk.accel
0.492
X-trk.accel
0.492
X-head ac.
NA
X-head ac.
NA
The following parameters were not seen or not valid:
ARINC Label 021 N1 Target ( FMC bus )
ARINC Label 150 GMT/UTC ( IRS bus ) - Does this have to be input by the pilot via the FMS ?
ARINC Label 103 Selected Air Speed (FCU bus) - Was this selected during the flight ?
ARINC Label 104 Selected vertical speed (FCU bus) - ditto ?
ARINC Label 164 Radio Altitude ( SGU EFIS bus)- Is this only valid in certain flight phases?
ARINC Label 213 SAT Static Air Temperature - due to a too short timeout in DLPU for this
parameter, now corrected.
4.2 Broadcast Messages
Change of Flight ID
Change of Capability Report
- PASS
- PASS
4.3 Comm-D Messages
Not applicable on this installation
4.4 Aquisition Squitter
Diversity fitted
- YES
Top antenna
Bottom antenna
-PASS
-PASS
24
RATE:0.5 Hz
RATE:0.5 Hz
4.5 Send Comm-B message with DLT
Read with bench
-PASS
4.6 Send Comm-D message with DLT
Not applicable on this installation
25
5. Data Link Uplink Tests
5.1 Send Comm-A test messages with bench
Messages received on printer
PASS
5.2 Send Comm-C messages with bench
Messages received on printer
FAIL
Due to a wiring error on the CommC/D transponder channel. This will be corrected as soon
as possible.
Note:
As a verification the DLPU and transponder from the aircraft were tested at EEC Bretigny and
the CommC messages functionned correctly.
After a wiring change on the aircraft this was retested and the CommC messages were then
correctly received by the aircraft system.
26
6.0 Flight Test
6.1 Test programme
Interference tests will be made during various flight phases.
For this purpose ModeS Data Link messages will be exchanged with the ground station.
The ground station can transmit data link messages at a high rate (bursts) during any interference
test.
The airborne data link equipment ( DLT ) can transmit messages to the ground during the flight
tests but at a low rate only, as this is dependant on a human operator and keyboard.
The exact nature and sequence of the flight test is described in a paper by S. Le Gall entitled
A300-600ST ENHANCED MODE S EMI FLIGHT TEST dated 4/12/97.
6.2 Mode S test setup
During the flight, Mode S data link messages were sent down-link from the DLT installed in the
cockpit and uplink messages were transmitted to the aircraft by the mobile Mode S ground station
installed on the taxi-way at Blagnac airport.
The ground station also extracted and validated the various aircraft parameters loaded into the
transponder by the DLPU.
Data link activity was high during the flight test.
Bursts of data link messages were also sent on request from the aircraft during some flight phases.
6.3 Mode S activity during Flight
During the flight 118 valid ATC type messages were received on the flight deck printer and 25
messages were sent from the flight deck (DLT) and correctly received on the ground. The GICB
registers were extracted many times during the flight. Recordings were made of all this Mode S
activity.
Many hundreds of messages were sent to the aircraft during the bursts of messages sent during
some flight phases. These messages, although processed by the Mode S system, were not
recorded or output on the printer as they would have overloaded the Mode S data link system.
27
7.0 Conclusions
No interference or perturbances were observed during the flight test due to Mode S Data Link
activity, STNA will certify the ModeS Data-Link Enhanced Surveillance Installation.
A wiring change is necessary to correct the delivery of CommC ( long messages) on the second
transponder channel. This will be done as soon as possible and the delivery of CommC messages
to the aircraft will be further tested when the aircraft flies within range of the Orly Mode S radar.
Note: This is now done and the CommC functions correctly.
A few parameters were not available during the flight ( see Section 4.1 ). These may be verified at
a later date and are not considered essential for the present trials.
The installed system is now ready for operational use.
28
APPENDIX C - BASIC SYSTEM TEST FOR GROUND CREW
29
Basic system test for Mode S data link system
PRINTER, DLT check power ON.
TRANSPONDER, check position 2 selected on control unit and transponder power ON.
DLPU check power ON.
PRINTER:
Check paper.
Press Test button and verify printer output correct :
1) All characters printed OK
2) Port 1 active
3) All other ports ( 2 -12 ) inactive.
DLT
Verify display shows : DLPU DLT DRIVER
Press ‘Shift’ key to verify all keyboard keys light up correctly
DLPU ( Check only if above tests fail )
Check GREEN light on front panel is ON. ( You must wait 20 seconds after switch on )
TRANSPONDER ( Check only if above tests fail )
Press TEST button on control unit ( or front panel ) to verify transponder self test.
SYSTEM RESET:
In case of any malfunction make a sytem reset by pulling the DLPU breaker OFF and then push ON
again.
If the malfunction persists inform EUROCONTROL.
30
APPENDIX D - FLIGHT TEST SCENARIO
31
NOTE:
The enhanced Mode S system under certification shall be in operation (in transmit
mode) during all the measures
and tests described herebelow.
The flight interphone shall be used and checked during all the flight test.
1.
PREPARATION FOR FLIGHT
1.1 RADIO ALTIMETER ACCURACY
The PFD 1/2 radio height indications are 0.
• Annotate RAD ALT1 - 2
Perform the current TAXI procedure and check that radio height is 0 during taxing.
2.
AFTER LIFT OFF - CLIMBTO FL310
2.1 RADIO ALTIMETER ACCURACY
Above 2500 ft the radio height indications are removed from the PFD 1/2
• Annotate RAD ALT1 - 2
3.
CRUISE AT FL 310
3.1 NAVIGATION SYSTEM ACCURACY
3.1.1 VHF NAV
The VOR - DME - ATC minimum range is 175Nm at FL 310.
• Add 5 Nm forevery 2000 ft above FL 310,
• Substract 5 Nm for every 2000 ft below FL 310.
VOR stations within range are obtained from the EFIS VOR option key.
• Annotate VOR 1 - 2
• Annotate DME 1 - 2
• Annotate ATC 1 - 2 including IDENT I - 2
3.1.2 WEATHER RADAR
The WX/RX are verified on all available operating modes.
• Annotate WX/RX I - 2.
32
3.2 COMMUNICATION SYSTEM ACCURACY
3.2.1 VHF COM
The VHF COM minimum range is 175Nm at FL 310.
• Add 5 Nm for every 2000 ft above FL 310,
• Subtract 5 Nm for every 2000 ft below FL 310.
• Annotate VHF 1-2-3 including SELCAL 1-2-3.
33
3.2.2 HF COM
The HF COM minimum range is dependant on meteo conditions and wave propagation.
The most common HF frequencies for in-flight use are listed herebelow:
• TOULOUSE
• STOCKHOLM
• LUFTHANSA
6543
5 541 - 8 930 - 11 345 - 13 342
10 078 - 13 296
• Annotate HF 1-2 including SELCAL 1-2
4.
DESCENT TO FL 100 - CRUISE AT FL 100
4.1
ADF
The ADF range is dependant on the ground station quality and is expected to be 50 Nm minimum.
ADF stations within range are obtained from the EFIS NDB option key.
• Annotate ADF 1 - 2.
4.2 WEATHER RADAR
The WX/RX are verified on all available operating modes.
• Annotate WX/RX 1 - 2
5.
APPROACH 1 GO AROUND
5.1 NDB BALANCE
At FL 40 the balance time of the ADF indication shall be measure vertically to an NDB station.
• Annotate ADF 1 - 2
5.2 WEATHER RADAR
The WX/RX are verified on all available operating modes.
• Annotate WX/RX I - 2
5.3 A/C GENERAL
DH :
AFS:
100ft
CAT 2
5.4 RADIO ALTIMETER ACCURACY
Below 2500 ft the radio height indications are restored on both PFD 1/2
• Annotate RAD ALT1 - 2
5.5 VOR MARKER VALIDITY AND ACCURACY
34
The time between Markers illumination is to be verified.
The VOR MKR 1/2 shall be checked.
• Annotate VOR MKR 1 - 2
35
5.6 ILS ACCURACY
The linearity of Localizer and Glide Slope is to be verified.
The LOC and GS indications shall be checked.
• Annotate ILS I - 2
5.7 AUTO CALL OUT (1)
When 100 ft above DH : Specific Auto Call Out for 100 ft above DH may be generated.
5.8 AUTO FLIGHT
When at DH initiate the go around.
6.
APPROACH 2 - AUTO - LAND
6.1 ILS ACCURACY
The linearity of Localizer and Glide Slope is to be verified.
The LOC and GS indications shall be checked.
• Annotate ILS I - 2
6.2 A/C GENERAL
AUTO BRK MED
DH
: ON (if necessary)
: 100 ft
6.3 AUTOMATIC LANDING
Perform standard Automatic Landing procedure.
6.4 AUTO CALL OUT (2)
• Record the Auto Call Out sequence as generated.
6.5 ENGINE REVERSE
• Apply idle engine reverse.
36
APPENDIX E - DETAILS OF GICB CONTENTS
Page No.
Eurocontrol Format
BDS 1.0 - Capability Report
BDS 1.7 - Engine No. 1 Report
BDS 2.1 - Aircraft Referenced State Vector Report
BDS 2.4 - Weight and Balance Report
BDS 2.7 - Engine No. 2 Report
BDS 3.1 - Waypoint Information
BDS 4.1 - Waypoint Identifier
BDS 5.1 - Position Report
BDS 6.1 - G.M.T. Report
BDS 7.0 - Aircraft Intention 1 Report
BDS 7.1 - Meteorological Report
BDS 8.0 - Aircraft Intention 2 Report
BDS 9.0 - Aircraft Intention 3 Report
BDS A.0 - Deviation Report
BDS B.0 - Airspeeds Report
BDS C.0 - Altitude Report
BDS D.0 - Intention Report 1
BDS D.1 - Turn Indication Report 1
BDS D.2 - Turn Indication Report 2
Mode S Specific Services Format
BDS 2.0 - Aircraft Identity
BDS 4.0 - Aircraft Intention
BDS 4.3 - Aircraft Intention
BDS 4.4 - Meteorological Routine Report
BDS 4.5 - Meteorological Hazard Report
BDS 5.0 - Track and Turn Report
BDS 5.1 - Position Report Coarse
BDS 5.3 - Air-referenced State Vector
BDS 6.0 - Heading and Speed Report
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 1,0
Capability Report
Eurocontrol Format
Purpose: To provide the DLPU status.
Notes:
1) Bite test bit B definition
1 = Bite test successful.
0 = Bite test failure.
2) DLPU status LED bit definition
1 = LED on.
0 = LED off
3) BDS 20 output
1 = active
0 = not active
4) ADI channels active bits c1 to c10. ( 10 channels )
1 = channel active.
5) DLT ( cockpit Data Link Terminal ) bit d definition
1 = DLT present and on-line
6) MICP ( cockpit printer ) bit m definition
1 = printer present and on-line
7) GPFT ( General Purpose File Transfer ) g bit definition
1 = GPFT initialised and available
0 = GPFT not initialised.
8) Control unit bit u definition
1 = control unit connected
9) Aircraft type field tttt definition
Indicates type of aircaft field 0 to 15 which is hard wired on
aircraft. This enables DLPU to process data from 15
different types of aircraft installations.
10) SAL Sytem Address Label field ssssssss definition.
The SAL can be hard wired on the aircraft. Value from 00 to
FF hexadecimal. This is used by the file transfer facility.
38
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Data
bit no.
Description
Bit.
BDS 1,0
( Not used )
Bite test
Status LED
BDS 20 o/p
ADI
Channels
Active
DLT
MICP
GPFT
Not used
Control unit
msb
Aircraft type
lsb
msb
System
Address
Label
lsb
Not used
0
0
0
1
0
0
0
0
x
x
x
x
x
B
S
T
c1
c2
c3
c4
c5
c6
c7
c8
c9
c 10
d
m
g
x
x
x
x
x
x
u
t
t
t
t
s
s
s
s
s
s
s
s
x
x
x
x
x
x
x
x
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 1, 7 Engine No. 1
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Report
Eurocontrol Format
Status bit = 0 also if data too old.
39
Data
bit no.
Status
Description
1 = valid data
msb = 128 %
N1 ACTUAL
Label 346
Range = [0,256 %]
Status
lsb = 128/1024 %
1 = Valid data
msb = 16384 lb/hr
FUEL FLOW
Label 347
Range = 0, 32768 lb/hr
Status
Sign
lsb = 8 lb/hr
1 = Valid data
1 = -ve
msb = 256 C
TOTAL AIR
TEMPERATURE
Label 211
Range = +-512 deg C
Status
Sign
msb = 0.5 C
1 = Valid data
1 = -ve
msb = 256 C
STATIC AIR
TEMPERATURE
Label 213
Range = +- 512 C
lsb = 0.5 C
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
29
28
27
26
25
24
23
22
21
20
19
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 2,1
Aircraft Referenced State Vector Report
Eurocontrol Format
Status bit = 0 also if data too old.
40
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
Data
bit no.
Status
Sign
49
50
51
52
53
54
55
56
Status
Sign
Description
1 = valid data
MAGNETIC
HEADING
Label 320
Range = [+-180 deg]
lsb = 0.18 deg
Status
TRUE AIR SPEED
Label 210
Range = [0,2048 kt]
lsb = 0.5 kt]
Status
Sign
ALTITUDE RATE
Label 212 or 365
Range =[+-16384 ft/min]
lsb = 64 ft/min
Status
Sign
STATIC AIR
TEMPERATURE
Label 213
Range = [+-512 °C]
lsb = 0.5 °C
NORMAL BODY
ACCELERATION
Label 333
Range = [+-1g]
lsb = 0.16g
ARINC
bit no.
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30&31
29
27
26
25
24
23
22
21
20
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
29
26
25
24
23
22
21
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 2,4
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Weight and Balance Report
Eurocontrol Format
Status bit = 0 also if data too old.
41
Data
bit no.
Status
Description
1 = valid data
CENTRE OF GRAVITY
Label 066 ( BCD )
Range = 0, 99.9 %
Status
1 = valid data
msb = 65536 lbs
GROSS WEIGHT
Label 075
Range = 0, 131072 lbs
msb = 16 lbs
ARINC
bit no.
30&31
27
26
25
24
23
22
21
20
19
18
17
16
15
30&31
28
27
26
25
24
23
22
21
20
19
18
17
16
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 2, 7 Engine No. 2
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Report
Eurocontrol Format
Status bit = 0 also if data too old.
42
Data
bit no.
Status
Description
1 = valid data
msb = 128 %
N1 ACTUAL
Label 346
Range = [0,256 %]
Status
lsb = 128/1024 %
1 = Valid data
msb = 16384 lb/hr
FUEL FLOW
Label 347
Range = 0, 32768 lb/hr
Status
Sign
lsb = 8 lb/hr
1 = Valid data
1 = -ve
msb = 256 C
TOTAL AIR
TEMPERATURE
Label 211
Range = +-512 deg C
Status
Sign
msb = 0.5 C
1 = Valid data
1 = -ve
msb = 256 C
STATIC AIR
TEMPERATURE
Label 213
Range = +- 512 C
lsb = 0.5 C
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
29
28
27
26
25
24
23
22
21
20
19
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 3,1
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Waypoint Information
Eurocontrol Format
Status bit = 0 also if data too old.
43
Data
bit no.
Status
Sign
Description
1 = valid data
BEARING TO WAYPOINT
Label 115
Range =[ +-180 deg ]
lsb = 0.18 deg ]
Status
TIME TO GO
Label 002
BCD
Range = [0,399.9 min]
ARINC
bit no.
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
Status
DISTANCE TO GO
BCD
Label 001
Range = [0,3999.9 nm]
SPARE
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 4,1
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Waypoint Identifier
Eurocontrol Format
Status bit = 0 also if data too old.
44
Data
bit no.
Status
Description
1 = valid data
char 3
ACTIVE WAYPOINT 1
Label 356
ISO 5 Characters
char 2
Status
char 1
1 = valid data
char 6
ACTIVE WAYPOINT 2
Label 357
ISO 5 Characters
char 5
Status
Sign
char4
1 = valid
1 = west
msb = 90 deg
DESIRED TRACK
Label 114
Range = +- 180 deg
lsb = 90/512 deg
ARINC
bit no.
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
10
9
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
10
9
30&31
29
28
27
26
25
24
23
22
21
20
19
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
BDS 5,1 Position Report
Eurocontrol Format
Status bit = 0 also if data too old.
45
Data
bit no.
Status
Sign
Description
1 = valid data
msb = 90 deg
LATITUDE
Label 310
Range =[ +-180 deg ]
Status
Sign
lsb = 90/131072 deg
1 = valid data
msb = 90 deg
LONGITUDE
Label 311
Range =[ +-180 deg ]
Status
Sign
lsb = 90/131072 deg
1 = valid data
msb = 65536 ft
ALTITUDE
Label 203
Range = -1000,131072 ft
lsb = 8 ft
ARINC
bit no.
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 6,1
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
G.M.T. Report
Eurocontrol Format
Status bit = 0 also if data too old.
46
Data
bit no.
Status
Description
1 = valid data
Hrs 0 -23
GMT Binary Word
Label 150
Minutes 0 - 59
Seconds 0 - 59
Status
1 = valid data
FLIGHT NUMBER (BCD)
Label 261
Status
1 = valid data
GMT BCD Word
Label 125
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 7,0
Aircraft Intention 1
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Report
Eurocontrol Format
Status bit = 0 also if data too old.
47
Data
bit no.
Status
Description
1 = valid data
SELECTED ALTITUDE
Label 102
Range = [0,65536 ft]
Status
Sign
lsb = 16 ft
1 = Valid data
SELECTED HEADING
Label 101
Range = [+-180 deg]
lsb = 0.8 deg
Status
STATUS WORD 1
Label 270
Discrete data
Status
STATUS WORD 2
Label 271
Discrete data
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30&31
29
28
27
26
25
24
23
22
21
30&31
25
24
23
22
21
20
19
18
17
16
15
14
13
12
11
30&31
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 7,1
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Meteorological Report
Eurocontrol Format
Status bit = 0 also if data too old.
48
Data
bit no.
Status
Sign
Description
1 = valid data
1 = left wing down
msb = 45 deg
ROLL ANGLE
Label 325
Range =[ +-90 deg ]
Status
Sign
Status
lsb = 45/128 deg
1 = valid data
1 = down
msb = 4096 ft/min
ALTITUDE RATE or
INERTIAL VERTICAL VEL.
Label 212 or 365
Range +-8192 ft/min
lsb = 128 ft/min
1 = valid data
msb = 128 kt
WIND SPEED
Label 315
Range = 0,256 kt
Status
Sign
lsb = 1 kt
1 = valid data
1 = west
msb = 90 deg
WIND ANGLE
Label 316
Range = +-180 deg
Status
Sign
lsb = 90/1218 deg
1 = valid data
1 = -ve
msb = 256 C
STATIC AIR
TEMPERATURE
Label 213
Range +- 512 deg C
Status
Sign
lsb = 0.5 C
1 = valid data
1 = -ve
msb = 0.5 g
ACCELERATION
Label 333
lsb = 1/16 g
ARINC
bit no.
30&31
29
27
26
25
24
23
22
21
20
30&31
29
26
25
24
23
22
21
30&31
29
28
27
26
25
24
23
22
21
30&31
29
28
27
26
25
24
23
22
21
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
29
26
25
24
23
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 8,0
Aircraft Intention 2
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Report
Eurocontrol Format
Status bit = 0 also if data too old.
49
Data
bit no.
Status
Description
1 = valid data
msb = 256 kt
SELECTED AIR SPEED
Label 103
Range = [0,512 kt]
Status
Sign
lsb = 0.25 kt
1 = Valid data
1 = down
msb = 8192
SELECTED ALTITUDE
RATE
Label 104
Range = [+-16384 ft/min]
lsb = 16 ft/min
Status
msb = 32768 ft
SELECTED ALTITUDE
Label 102
Range = 0, 65536 ft
msb = 16 ft
Status
STATUS WORD 1
Label 270
Discrete data
Status
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30 & 31
25
24
23
22
20
15
14
13
30 & 31
STATUS WORD 2
Label 271
Discrete data
27
22
21
20
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 9, 0
Aircraft Intention 3
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Report
Eurocontrol Format
Status bit = 0 also if data too old.
50
Data
bit no.
Status
Description
1 = valid data
msb = 2048 mM
SELECTED MACH
Label 106
Range = [0,4096 mM]
Status
Sign
lsb = 2 mM
1 = Valid data
1 = down
msb = 8192
SELECTED ALTITUDE
RATE
Label 104
Range = [+-16384 ft/min]
lsb = 16 ft/min
Status
msb = 32768 ft
SELECTED ALTITUDE
Label 102
Range = 0, 65536 ft
msb = 16 ft
Status
STATUS WORD 1
Label 270
Discrete data
Status
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30 & 31
25
24
23
22
20
15
14
13
30 & 31
STATUS WORD 2
Label 271
Discrete data
27
22
21
20
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS A,0
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Deviation Report
Eurocontrol Format
Status bit = 0 also if data too old.
51
Data
bit no.
Status
Sign
Description
1 = valid data
msb = 64 nm
CROSS TRACK ERROR
Label 116
Range =[ 0, 128 mn] ]
Status
Sign
lsb =0.004 nm
1 = valid data
1 = low
msb = 1024 ft
VERTICAL DEVIATION
Label 117
Range = 0, 2048 ft
Status
Sign
lsb = 1 ft
1 = valid data
1 = -ve
msb = 0.5 g
BODY NORMAL
ACCELERATION
Label 333
Range = +- 1g
lsb = 1/64 g
ARINC
bit no.
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
30&31
29
28
27
26
25
24
23
22
21
20
19
18
30&31
29
26
25
24
23
22
21
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS B,0
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Airspeeds Report
Eurocontrol Format
Status bit = 0 also if data too old.
52
Data
bit no.
Status
Description
1 = valid data
msb = 512 kt
COMPUTED AIR SPEED
Label 206
Range =[ 0, 1024 kt ]
Status
lsb = 0.25 kt
1 = valid data
msb = 1024 kt
TRUE AIR SPEED
Label 210
Range =[ 0, 2048 kt ]
Status
lsb = 0.5 kt
1 = valid data
msb = 2048 mM
MACH
Label 205
Range =[ 0, 4.096 ]
Status
Sign
lsb = 0.00025
1 = valid data
1 = west
msb = 90 deg
MAGNETIC HEADING
Label 320
Range =[+-180 deg ]
lsb = 90/512 deg
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30&31
28
27
26
25
24
23
22
21
20
19
18
17
16
15
30&31
29
28
27
26
25
24
23
22
21
20
19
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS C,0
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Altitude Report
Eurocontrol Format
Status bit = 0 also if data too old.
53
Data
bit no.
Status
Description
1 = valid data
msb = 4096 ft
RADIO HEIGHT
Label 164
Range = 0, 8192 ft
Status
lsb = 1 ft
1 = valid data
msb = 512 mb
AVERAGE STATIC
PRESSURE
Label 246
Range 0,1024 mb
Status
lsb = 0.25 mb
1 = valid data
msb = 65536 ft
ALTITUDE
Label 203
Range = 0, 131072 ft
lsb = 1 ft
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
17
16
30&31
27
26
25
24
23
22
21
20
19
18
17
16
30&31
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
13
12
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS D,0 Intention Report 1
Eurocontrol Format
Status bit = 0 also if data too old.
54
BDS
1
2
3
4
5
6
7
8
9
10
Data
Status
Sign
11
12
13
14
15
16
17
18
19
20
Status
Sign
21
22
23
24
25
26
27
28
29
30
31
32
33
34
Status
Sign
35
36
37
38
39
40
41
42
43
44
Status
Sign
45
46
47
48
49
50
51
52
53
54
55
56
Status
Sign
Description
1 = valid data
msb 90 deg
SELECTED COURSE
Label 100
Range [+-180 deg ]
lsb 0.7 deg
1 = valid data
msb 90 deg
SELECTED HEADING
Label 101
Range [+-180 deg ]
lsb 0.7 deg
1 = valid data
msb 32 768 ft
SELECTED ALTITUDE
Label 102
Range [0,65 536 ft]
lsb 16 ft
1 = valid data
msb 90 deg
DESIRED TRACK
Label 114
Range [+-180 deg ]
lsb 0.7 deg
1 = valid data
msb 16339 ft/min
INERTIAL VERTICAL
VELOCITY
Label 365
Range [0,32678 ft/min]
lsb = 32 ft/min
ARINC
30&31
29
28
27
26
25
24
23
22
21
30&31
29
28
27
26
25
24
23
22
21
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
30&31
29
28
27
26
25
24
23
22
21
30&31
29
28
27
26
25
24
23
22
21
20
19
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS D,1 Turn Indication Report 1
Eurocontrol Format
Status bit = 0 also if data too old.
55
BDS
bit no.
1
2
3
4
5
6
7
8
Data
bit no.
Status
Sign
9
10
11
12
13
14
15
16
17
Status
Sign
18
19
20
21
22
23
24
25
26
Status
Sign
27
28
29
30
31
32
33
34
35
36
37
38
39
40
Status
Sign
41
42
43
44
45
46
47
48
Status
49
50
51
52
53
54
55
56
Status
Description
1 = valid data
msb 22.5 deg
ROLL ANGLE
Label 325
Range [+- 45 deg ]
lsb 0.7 deg
1 = valid data
msb 56 deg/sec
ROLL RATE
Label 327
Range [0,128 deg/sec]
lsb 1 deg/sec
1 = valid data
msb 16 deg/sec
TRACK ANGLE RATE
Label 335
Range [ +- 32 deg/sec
lsb 0.25 deg/sec
1 = valid data
msb 90 deg
MAGNETIC HEADING
Label 320
Range [+-180 deg]
lsb 0.044 deg
1 = valid data
msb 0.25 g
CROSS TRACK ACCEL
Label 363
Range [0,0.5g]
lsb 0.004g
1 = valid data
msb 0.25 g
CROSS HEAD. ACCEL
Label 376
Range [0,0.5g]
lsb 0.004g
ARINC
bit no.
30&31
29
26
25
24
23
22
21
30&31
29
28
27
26
25
24
23
22
30&31
29
28
27
26
25
24
23
22
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
30&31
25
24
23
22
21
20
19
30&31
25
24
23
22
21
20
19
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS
1
2
3
4
5
6
7
8
BDS D,2 Turn Indication Report 2
Eurocontrol Format
Status bit = 0 also if data too old.
Data
Status
Sign
msb 22.5 deg
ROLL ANGLE
Label 325
Range [+- 45 deg ]
lsb 0.7 deg
9
10
11
12
13
14
15
16
17
56
Description
1 = valid data
msb 56 deg/sec
ROLL RATE
Label 327 or 337
Range [128 deg/sec]
lsb 1 deg/sec
18
19
20
21
22
23
24
25
26
Status
Sign
27
28
29
30
31
32
33
34
35
36
37
38
39
40
Status
Sign
41
42
43
44
45
46
47
48
Status
49
50
51
52
53
54
55
56
Status
1 = valid data
TRACK ANGLE RATE
Label 335
Range [ 0,32 deg/sec]
1 = valid data
msb 90 deg
TRACK ANGLE TRUE
Label 313
Range [+-180 deg]
lsb 0.044 deg
1 = valid data
msb 0.25 g
CROSS TRACK ACCEL
Label 363
Range [0,0.5g]
lsb 0.004 g
1 = valid data
msb 0.25 g
CROSS HEAD. ACCEL
Label 376
Range [0,0.5g]
lsb 0.004 g
ARINC
30&31
29
26
25
24
23
22
21
30&31
29
28
27
26
25
24
23
22
30&31
29
28
27
26
25
24
23
22
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
30&31
25
24
23
22
21
20
19
30&31
25
24
23
22
21
20
19
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
BDS 2,0 Aircraft Identity
ModeS Specific Service Format
Purpose: To report aircraft identification to the ground in
accordance with Annex.10 Volume IV, section 3.1.2.9
Notes:
1) Annex 10, Volume IV, section 3.1.2.9 provides a full
definition of BDS 2,0
2) The character coding to be used is identical to taht
defined in Table 3-6 of Chapter 3, Annex 10, Volume IV.
3) This data may be input to ther transponder from sources
other than the Mode S ADLP.
4) This format is used by the extended squitter application.
Description
BDS
Label 2,0
Bit
0
0
1
0
0
0
0
0
Character 1
see Note
2
12
13
14
15
16
17
Character 2
see Note
2
18
19
20
21
22
23
Character 3
see Note
2
24
25
26
27
28
29
Character 4
see Note
2
30
31
32
33
34
35
Character 5
see Note
2
36
37
38
39
40
41
Character 6
see Note
2
42
43
44
45
46
47
Character 7
see Note
2
48
49
50
51
52
53
Character 8
see Note
2
54
55
56
57
Data
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
BDS 4,0 Aircraft intention
Purpose: To provide ready access to information about an
aircraft’s short-term intentions, in order to improve the
effectiveness of conflict probes and to provide additional
tactical information to controllers.
Notes:
1) The data entered into this register should be derived from
the sources that are controlling the aircraft.
2) Selected course/heading and selected airspeed/mach are
switchable, with an extra switch bit to indicate which
parameter is in use. It is defined as follows:
SWITCH bit
Course/heading
Airspeed/Mach
0
Course
Airspeed
1
Heading
Mach
58
Data
Status
Sign
Description
1 = valid data
msb = 32768 ft
SELECTED ALTITUDE
Label 102
Range =[ 0, 65520 ft ]
lsb = 16 ft
1 = valid data
Sign 1 = minus
msb = 8192 ft/min
SELECTED ALTITUDE
RATE
Label 104
Range = [+- 16352 ft/min ]
lsb = 32 ft/min
SWITCH
STATUS
SIGN
msb = 90 deg
SELECTED MAGNETIC
COURSE / HEADING
Label 100 / 101
Range = [+-180 deg]
lsb = 360/512 deg
SWITCH
STATUS
msb = 256 kt/Mach 2048
SELECTED
AIRSPEED/MACH
Label 103 / 106
Range = [ 0,512 kt]
or [0,4.096 Mach]
lsb = 0.5 kt/Mach 0.004
STATUS of MODE Fields
MODE
SELECTED ALTITUDE
MODE
SELECTED ALTITUDE RATE
MODE
SELECT. COURSE/HEADING
MODE
SELECTED AIRSPEED/MACH
ARINC
bit no.
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30&31
29
27
26
25
24
23
22
21
20
19
30&31
29
28
27
26
25
24
23
22
21
30&31
27
26
25
24
23
22
21
20
19
18
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
BDS 4,3 Aircraft intention
ModeS Specific Service Format
Purpose: To provide ready access to details about the next
waypoint on an aircraft’s route, without the need to establish
a data link dialogue with the flight management system. This
will assist with short and medium term tactical control.
Note:
Time to go and Distance to go are Binary Coded Decimal
values, where each decimal digit requires 4 bits of data.
59
Data
Status
Sign
Description
1 = valid data
Msb=90 deg.
BEARING TO WAYPOINT
Label 115
Range=[+-180 deg.]
Status
Lsb= 360/2048 degs.
1 = valid data
10 min. digit
TIME TO GO
Label 002 (BCD)
1 min.
Range=[0, 99.9 min]
0.1 min
Status
1 = valid data
100 nm. digit
DISTANCE TO GO
10 nm.
Label 001 (BCD)
Range=[0,999.9 nm]
1 nm.
0.1 nm.
UNASSIGNED
ARINC
bit no.
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
29
28
27
26
25
24
23
22
21
20
19
18
30&31
29
28
27
26
25
24
23
22
21
20
19
18
17
16
15
14
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 4,4 Meteorological Routine Report
Purpose: To allow meteorological data to be collected by
ground systems.
The decimal value of the binary coded ( figure of merit )
FOM/SOURCE parameter must be interpreted as follows:
0
1
2
3
4
5-15
= Invalid
= INS
= GNSS
= DME/DME
= VOR/DME
= Unassigned
Notes:
1) ARINC 429 label 315 only supplies data with an MSB of
128. When using this data source, bit 6 in the MB field is
not used and must be set to 0.
2) The interpretation of the two bits assigned to
TURBULENCE is as shown in the table for BDS 4,5.
3) The average static pressure is not a requirement of Annex
3.
60
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Data
Description
ARINC
bit no.
FOM/SOURCE
Status
Wind parameters
MSB = 256 kt
WINDSPEED
Label 315
Range = [0,512 kt ]
lsb = 1 kt
Sign
msb = 90 deg.
WIND DIRECTION
Label 316
Range = [+-180 deg]
lsb = 180/256 deg
Status
Sign
msb = 64 deg C
STATIC AIR TEMPERATURE
Label 213
Range = [+-128 C ]
lsb = 0.25 C
Status
msb = 1024 hPa
AVERAGE STATIC
PRESSURE
Label 217
Range = [2048 hPa]
lsb = 1 hPa
Status
TURBULENCE
Status
msb = 100%
HUMIDITY
lsb = 100/64%
28
27
26
25
24
23
22
21
20
29
28
27
26
25
24
23
22
21
30&31
29
26
25
24
23
22
21
20
19
18
30&31
28
27
26
25
24
23
22
21
20
19
18
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
BDS 4,5 Meteorological Hazard Report
ModeS Specific Service Format
Purpose: To provide reports on the severity of
meteorological hazards, in particular for low flight.
The interpretation of the two bits assigned to each hazard is
defined in the table below:
Bit 1
0
0
1
1
Bit 2
0
1
0
1
Nil
Light
Moderate
Severe
Note : The definition of the terms Light, Moderate, and
Severe are those defined in the PANS-RAC ( Doc.4444)
where applicable.
61
Data
Status
Description
ARINC
bit no.
1 = valid data
TURBULENCE
Status
WIND SHEAR
Status
MICROBURST
Status
ICING
Status
WAKE VORTEX
Status
Sign
Msb = 64 deg c
STATIC AIR TEMPERATURE
Label 213
Range = [ +- 128 deg C]
Lsb = 0.25 deg C
Status
Msb = 1024 hPa
AVERAGE STATIC
PRESSURE
Label 217
Range = 0, 2048 hPa
Lsb = 1 hPa
Status
Msb = 32 768 ft
RADIO HEIGHT
Label 164
Range = 0, 65 528 ft
Lsb = 16 ft
30&31
29
28
27
26
25
24
23
22
21
20
30&31
28
27
26
25
24
23
22
21
20
19
18
30&31
28
27
26
25
24
23
22
21
20
19
18
17
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 5,0
Track and turn report
Mode S Specific Services Format
1. All references to ARINC assume that the ARINC 429
standard is used.
2. The BDS servicing process will make a logical AND of
bits 30 & 31 of each ARINC parameter and insert the result
into the status bit for the corresponding parameter.
3. The maximum acceptable data age at time of transmission
to the ground is 1 s for all parameters.
4. The BDS update rate will be sufficient to ensure that the
maximum acceptable data age of all parameters is not
exceeded in normal operation.
5. If maximum acceptable data age is exceeded for any
parameter, then the status bit for that parameter should
actively be set to 0 by the BDS processing service.
6. If the value of a parameter from the data source exceeds
the range allowable in the BDS definition, the maximum
allowable value in the correct positive or negative sense will
be used instead.
Notes:
1) The data entered into this register should, whenever
possible, be derived from the sources that are controlling
the aircraft.
2) This requires active intervention by the BDS servicing
process.
3) Where ARINC 429 is used, this only relates to parameters
where the most significant bit or bits have been omitted
from the BDS format.
7. If any parameter is not available on the aircraft, all bits
corresponding to that parameter must be actively set to 0 by
the BDS servicing process.
Note : If any parameter becomes unavailable due
to abnormal operation, then item 5 above applies.
62
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Data
bit no.
Status
Sign
Description
1 = valid data
1 = left (left wing down )
msb = 45 deg
ROLL ANGLE
Label 325
Range =[ +- 90deg ]
Status
Sign
lsb = 45/256 deg
1 = valid data
1 = west ( e.g. 315 = -45 deg)
msb = 90 deg
TRUE TRACK ANGLE
Label 313
Range =[ +- 180 deg ]
Status
lsb = 90/512 deg
1 = valid data
msb = 1024 kts
GROUND SPEED
Label 312
Range = [0,2046 ]
lsb = 2 kt
1 = valid data
1 = minus
msb = 8 deg/sec
TRACK ANGLE RATE
Label 335
Range = [-16,+16]
lsb = 8/256
1 = valid data
msb = 1024 kt
TRUE AIR SPEED
Label 210
Range =[0,2046]
lsb = 2 kt
ARINC
bit no.
30&31
29
27
26
25
24
23
22
21
20
19
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
27
26
25
24
23
22
21
20
19
18
30&31
29
27
26
25
24
23
22
21
20
19
30&31
28
27
26
25
24
23
22
21
20
19
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
BDS 5, 1 Position Report Coarse
ModeS Specific Service Format
PURPOSE: To provide a three-dimensional report on
aircraft position.
Notes :
1) The single status bit ( bit 1 ) is to be set to 0 if any of the
three parameters are invalid and are identical to the status
bit in BDS 5,2.
2) The required valid range for latitude is +90 degrees to 90 degrees, but the parameter is coded with an msb of 90
degrees to allow the use of the same coding algorithm as
for longitude.
3) The source of the information in this buffer is the same as
that indicated in the FOM/SOURCE field of BDS 5,2.
63
Data
Status
Sign
Description
1 = valid data
msb = 90 deg
LATITUDE
Range =[ +-180 deg ]
lsb = 360/1048576 deg
Sign
msb = 90 deg
LONGITUDE
Range =[ +-180 deg ]
lsb = 360/1048576 deg
Sign
msb = 65536 ft
PRESSURE
ALTITUDE
Range = 131068 ft
lsb = 8 ft
ARINC
bit no.
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
BDS 5,3 Air-referenced State Vector
ModeS Specific Service Format
PURPOSE: To provide the ATC system with the current
measured values of magnetic heading, IAS/Mach, altitude
rate and TAS.
64
Data
bit no.
Status
Sign
Description
1 = valid data
msb = 90 deg
MAGNETIC HEADING
Label 320
Range =[ +-180 deg ]
Status
lsb = 360/2048 deg
1 = valid data
msb = 512 kt
INDICATED AIRSPEED (IAS)
Label 206
Range = 0, 1024 kt
Status
lsb = 1 kt
1 = valid data
msb = 2.048
MACH NUMBER
Label 205
Range = 0, 4.096
Status
lsb = 0.008
1 = valid data
msb = 1024 kt
TRUE AIRSPEED (TAS)
Range = 0,2048 kt
Status
Sign
lsb = 0.5 kt
1 = valid data
msb = 8192 ft/min
ALTITUDE RATE
Label 212
Range = +- 16384 ft/min
msb = 64 ft/min
ARINC
bit no.
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
28
27
26
25
24
23
22
21
20
19
30&31
28
27
26
25
24
23
22
21
20
30&31
28
27
26
25
24
23
22
21
20
19
18
17
30&31
29
28
27
26
25
24
23
22
21
Mode-S Specific Services Installation on A300/600ST Beluga aircraft
EUROCONTROL
BDS 6,0 Heading and speed report
ModeS Specific Service Format
1. All references to ARINC assume that the ARINC 429
standard is used.
2. The BDS servicing process will make a logical AND of
bits 30 & 31 of each ARINC parameter and insert the result
into the status bit for the corresponding parameter.
3. The maximum acceptable data age at time of transmission
to the ground is 1 s for all parameters.
4. The BDS update rate will be sufficient to ensure that the
maximum acceptable data age of all parameters is not
exceeded in normal operation.
5. If maximum acceptable data age is exceeded for any
parameter, then the status bit for that parameter should
actively be set to 0 by the BDS processing service.
6. If the value of a parameter from the data source exceeds
the range allowable in the BDS definition, the maximum
allowable value in the correct positive or negative sense will
be used instead.
Notes:
1) The data entered into this register should, whenever
possible, be derived from the sources that are controlling
the aircraft.
2) This requires active intervention by the BDS servicing
process.
3) Where ARINC 429 is used, this only relates to parameters
where the most significant bit or bits have been omitted
from the BDS format.
7. All parameters are required except for Inertial Vertical
Velocity which will be supplied only by aircraft with a
suitable inertial source. If Inertial Vertical Velocity is not
available bits 46 to 56 inclusive must be actively set to 0 by
the BDS servicing process.
65
BDS
bit no.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
Data
bit no.
Status
Sign
Description
1 = valid data
1 = west
msb = 90 deg
MAGNETIC HEADING
Label 320
Range =[ +-180 deg ]
Status
lsb = 90/512 deg
1 = valid data
msb = 512 kt
INDICATED AIRSPEED
Label 206
Range = [0, 1023]
Status
lsb = 1kt
1 = valid data
msb = 2.048 mach
MACH NUMBER
Label 205
Range = [0, 4.096 ]
Status
Sign
lsb = 2.048/512
1 = valid data
1 = below
msb = 8192 ft/min
BAROMETRIC ALTITUDE
RATE
Label 212
Range = [-16384, +16352 ]
Status
Sign
lsb = 32 ft/min
1 = valid data
1 = below
msb = 8192 ft/min
INERTIAL VERTICAL
VELOCITY
Label 365
Range = [-16384, +16352 ]
lsb = 32 ft/min
ARINC
bit no.
30&31
29
28
27
26
25
24
23
22
21
20
19
30&31
28
27
26
25
24
23
22
21
20
19
30&31
28
27
26
25
24
23
22
21
20
19
30&31
29
27
26
25
24
23
22
21
20
19
30&31
29
27
26
25
24
23
22
21
20
19
APPENDIX F - BDS ALLOCATION TABLE FOR A300 BELUGA
66
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
;
; BELUGA A300/600 TABLE
;
; MODES SPECIFIC SERVICE MANUAL BDS DEFINITIONS
;
DB
26
;number of update reports
;
; BDS 40 AIRCRAFT INTENTION
;
DB
040H ;BDS register
DW
1000 ;update interval
DB
4
;number of ARINC words
;ARINC WORD 1
DB
102Q ;label SELECTED ALTITUDE
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB UNSIGNED ;unsigned value
;ARINC WORD 2
DB
104Q ;label SELECTED ALTITUDE RATE
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
14
;status bit pos in MB field
DB
15
;start data pos in MB field
DB
SIGNED ;signed value
;SWITCH BIT Bit 25 should be 1
;ARINC WORD 3
DB
101Q ;label SELECTED MAGNETIC HEADING
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
26
;status bit pos in MB field
DB
27
;start data pos in MB field
DB
SIGNED ;signed value
;SWITCH BIT Bit 36=0
;ARINC WORD 4
DB
103Q ;label SELECTED AIRSPEED
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
37
;status bit pos in MB field
DB
38
;start data pos in MB field
DB UNSIGNED ;unsigned value
; SPACE HERE FOR SELECTED MODES - 9 BITS
;
; BDS 41 NEXT WAYPOINT DETAILS
;
; Waypoint name - 9 chars in 6 bit character form
; BDS 42 NEXT WAYPOINT DETAILS
; Waypoint Lat. Long. Crossing Altitude
; Information not available
; BDS 43 NEXT WAYPOINT DETAILS
DB
043H ;BDS register
DW
1000 ;update interval
DB
3
;number of ARINC words
;ARINC WORD 1
DB
115Q ;label BEARING TO WAYPOINT
DB
6
;channel
DB
BNR ;format
EUROCONTROL
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
002Q ;label TIME TO GO
DB
6
;channel
DB
BCD ;format
DW
400 ;max age ms
DB
26
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
13
;status bit pos in MB field
DB
14
;start data pos in MB field
DB UNSIGNED ;unsigned value
;ARINC WORD 3
DB
001Q ;label DISTANCE TO GO
DB
6
;channel
DB
BCD ;format
DW
400 ;max age ms
DB
26
;start bit ARINC word
DB
16
;number of bits to copy
DB
0
;number of discretes
DB
26
;status bit pos in MB field
DB
27
;start data pos in MB field
DB UNSIGNED ;unsigned value
;
; BDS 44 METEREOLOGICAL ROUTINE AIR REPORT
;
; Bits 1 to 4 should be Figure of Merit (FOM)
DB
044H ;BDS register
DW
1000 ;update interval
DB
4
;number of ARINC words
;ARINC WORD 1
DB
315Q ;label WINDSPEED
DB
1
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
5
;status bit pos in MB field
DB
6
;start data pos in MB field
DB UNSIGNED ;sign
;ARINC WORD 2
DB
316Q ;label WIND DIRECTION (TRUE )
DB
1
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
5
;status bit pos in MB field
DB
15
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 3
DB
213Q ;label STATIC AIR TEMPERATURE
DB
5
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
26
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
24
;status bit pos in MB field
DB
25
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 4
DB
217Q ;label AVERAGE STATIC PRESSURE
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
67
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DB
DB
DB
DB
DB
DB
28
;start bit ARINC word
11
;number of bits to copy
0
;number of discretes
35
;status bit pos in MB field
36
;start data pos in MB field
UNSIGNED ;sign
EUROCONTROL
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
313Q ;label TRUE TRACK ANGLE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
12
;status bit pos in MB field
DB
13
;start data pos in MB field
DB
SIGNED ;signed
;ARINC WORD 3
DB
312Q ;label GROUND SPEED
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
27
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
24
;status bit pos in MB field
DB
25
;start data pos in MB field
DB UNSIGNED ;sign
;ARINC WORD 4
DB
335Q ;label TRACK ANGLE RATE
DB
1
;channel IRS bus
DB
BNR ;format
DW
100 ;max age ms
DB
27
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
35
;status bit pos in MB field
DB
36
;start data pos in MB field
DB
SIGNED ;sign
;ARINC WORD 5
DB
210Q ;label TRUE AIR SPEED
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
46
;status bit pos in MB field
DB
47
;start data pos in MB field
DB UNSIGNED ;sign
;
; BDS 51 POSITION REPORT - COARSE
;
DB
51H ;BDS register
DW
1000 ;update interval
DB
3
;number of ARINC words
;ARINC WORD 1
DB
310Q ;label LATITUDE
DB
6
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
19
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
311Q ;label LONGITUDE
DB
6
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
19
;number of bits to copy
DB
0
;number of discretes
;
; Turbulence Field ( 3 bits 47-49 )
;
; Humidity Field ( 7 bits 50 - 56 )
;
;
; BDS 45 METEREOLOGICAL HAZARD REPORT
;
; Bits 1 to 15 should be indicators of
;
Turbulence
;
Wind shear
;
Microburst
;
Icing
;
Wake vortex
;
DB
045H ;BDS register
DW
1000 ;update interval
DB
3
;number of ARINC words
;ARINC WORD 1
DB
213Q ;label STATIC AIR TEMPERATURE
DB
5
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
16
;status bit pos in MB field
DB
17
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
217Q ;label AVERAGE STATIC PRESSURE
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
DB
28
;start bit ARINC word
DB
11
;number of bits to copy
DB
0
;number of discretes
DB
27
;status bit pos in MB field
DB
28
;start data pos in MB field
DB UNSIGNED ;sign
;ARINC WORD 3
DB
164Q ;label RADIO HEIGHT
DB
7
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
39
;status bit pos in MB field
DB
40
;start data pos in MB field
DB UNSIGNED ;sign
;
; BDS 48 VHF FREQUENCY REPORT
;
Not Available on Beluga
;
;
; BDS 50 TRACK AND TURN REPORT
;
;
DB
50H ;BDS register
DW
1000 ;update interval
DB
5
;number of ARINC words
;ARINC WORD 1
DB
325Q ;label ROLL ANGLE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
27
;start bit ARINC word
68
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DB
1
;status bit pos in MB field
DB
22
;start data pos in MB field
DB
SIGNED ;signed
;ARINC WORD 3
DB
203Q ;label ALTITUDE ( 1013.25 mb )
DB
5
;channel
DB
BNR ;format
DW
125 ;max age ms
DB
28
;start bit ARINC word
DB
14
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
43
;start data pos in MB field
DB UNSIGNED ;sign
;
; BDS 52 POSITION REPORT FINE
;
Not available Beluga
;
; BDS 53 AIR REFERENCED STATE VECTOR
;
DB
53H ;BDS register
DW
1000 ;update interval
DB
5
;number of ARINC words
;ARINC WORD 1
DB
320Q ;label MAGNETIC HEADING
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
206Q ;label COMPUTED AIR SPEED
DB
7
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
13
;status bit pos in MB field
DB
14
;start data pos in MB field
DB
SIGNED ;signed
;ARINC WORD 3
DB
205Q ;label MACH NUMBER
DB
7
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
25
;status bit pos in MB field
DB
26
;start data pos in MB field
DB UNSIGNED ;sign
;ARINC WORD 4
DB
210Q ;label TRUE AIR SPEED
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
34
;status bit pos in MB field
DB
35
;start data pos in MB field
DB UNSIGNED ;sign
;ARINC WORD 5
DB
212Q ;label ALTITUDE RATE
DB
5
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
DB
DB
DB
DB
;
;
;
;
;
;
;
;
;
;
;
;
;
;
EUROCONTROL
0
;number of discretes
47
;status bit pos in MB field
48
;start data pos in MB field
SIGNED ;sign
BDS 54 TACTICAL WAYPOINT REPORTS
BDS 55 TACTICAL WAYPOINT REPORTS
BDS 56 TACTICAL WAYPOINT REPORTS
BDS 5F QUASI STATIC PARAMETER MONITORING
Not available on Beluga
BDS 60 HEADING AND SPEED REPORT
DB
60H ;BDS register
DW
1000 ;update interval
DB
5
;number of ARINC words
;ARINC WORD 1
DB
320Q ;label MAGNETIC HEADING
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
206Q ;label COMPUTED AIR SPEED
DB
7
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
13
;status bit pos in MB field
DB
14
;start data pos in MB field
DB
UNSIGNED ;signed
;ARINC WORD 3
DB
205Q ;label MACH NUMBER
DB
7
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
24
;status bit pos in MB field
DB
25
;start data pos in MB field
DB UNSIGNED ;sign
;ARINC WORD 4
DB
212Q ;label BARO.ALTITUDE RATE
DB
5
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
27
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
35
;status bit pos in MB field
DB
36
;start data pos in MB field
DB
SIGNED ;sign
;ARINC WORD 5
DB
365Q ;label INERTIAL VERTICAL VELOCITY
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
27
;start bit ARINC word
DB
9
;number of bits to copy
DB
0
;number of discretes
DB
46
;status bit pos in MB field
69
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DB
DB
47
;start data pos in MB field
SIGNED ;sign
EUROCONTROL
;
DB
9
;channel
;
DB
BNR ;format
;
DW
250 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
11
;number of bits to copy
;
DB
0
;number of discretes
;
DB
15
;status bit pos in MB field
;
DB
17
;start data pos in MB field
;
DB UNSIGNED ;signed value
;ARINC WORD 3
;
DB
313Q ;label TRACK ANGLE TRUE
;
DB
1
;channel
;
DB
BNR ;format
;
DW
100 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
12
;number of bits to copy
;
DB
0
;number of discretes
;
DB
28
;status bit pos in MB field
;
DB
29
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 4
;
DB
317Q ;label TRACK ANGLE MAGNETIC
;
DB
1
;channel
;
DB
BNR ;format
;
DW
100 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
12
;number of bits to copy
;
DB
0
;number of discretes
;
DB
42
;status bit pos in MB field
;
DB
43
;start data pos in MB field
;
DB
SIGNED ;signed value
;
; Conficts with MSSS
;
;
DB
060H ;BDS register
;
DW
1000 ;update interval
;
DB
5
;number of ARINC words
;ARINC WORD 1
;
DB
317Q ;label TRACK ANGLE MAGNETIC
;
DB
1
;channel
;
DB
BNR ;format
;
DW
100 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
10
;number of bits to copy
;
DB
0
;number of discretes
;
DB
1
;status bit pos in MB field
;
DB
2
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 2
;
DB
312Q ;label GROUND SPEED
;
DB
1
;channel
;
DB
BNR ;format
;
DW
100 ;max age ms
;
DB
27
;start bit ARINC word
;
DB
12
;number of bits to copy
;
DB
0
;number of discretes
;
DB
13
;status bit pos in MB field
;
DB
15
;start data pos in MB field
;
DB UNSIGNED ;signed value
;ARINC WORD 3
;
DB
365Q ;label INERTIAL VERTICAL VELOCITY
;
DB
4
;channel
;
DB
BNR ;format
;
DW
125 ;max age ms
;
DB
27
;start bit ARINC word
;
DB
8
;number of bits to copy
;
DB
0
;number of discretes
;
DB
27
;status bit pos in MB field
;
DB
28
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 4
;
DB
213Q ;label STATIC AIR TEMP.
;
DB
9
;channel
;
DB
BNR ;format
;
; EUROCONTROL DLPU C2 BDS REPORTS
;
; Conficts with MSSS
;
DB
040H ;BDS register
;
DW
1000 ;update interval
;
DB
4
;number of ARINC words
;ARINC WORD 1
;
DB
322Q ;label FLIGHT PATH ANGLE
;
DB
1
;channel
;
DB
BNR ;format
;
DW
100 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
10
;number of bits to copy
;
DB
0
;number of discretes
;
DB
1
;status bit pos in MB field
;
DB
2
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 2
;
DB
323Q ;label FLIGHT PATH ACCELERATION
;
DB
1
;channel
;
DB
BNR ;format
;
DW
100 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
12
;number of bits to copy
;
DB
0
;number of discretes
;
DB
13
;status bit pos in MB field
;
DB
14
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 3
;
DB
241Q ;label CORRECTED ANGLE OF
ATTACK
;
DB
9
;channel
;
DB
BNR ;format
;
DW
125 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
12
;number of bits to copy
;
DB
0
;number of discretes
;
DB
27
;status bit pos in MB field
;
DB
28
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 4
;
DB
204Q ;label BARO.CORRECTED ALTITUDE
#1
;
DB
9
;channel
;
DB
BNR ;format
;
DW
125 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
14
;number of bits to copy
;
DB
0
;number of discretes
;
DB
41
;status bit pos in MB field
;
DB
42
;start data pos in MB field
;
DB
SIGNED ;signed value
;
; Conficts with MSSS
;
;
DB
050H ;BDS register
;
DW
1000 ;update interval
;
DB
4
;number of ARINC words
;ARINC WORD 1
;
DB
205Q ;label MACH NUMBER
;
DB
9
;channel
;
DB
BNR ;format
;
DW
250 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
12
;number of bits to copy
;
DB
0
;number of discretes
;
DB
1
;status bit pos in MB field
;
DB
3
;start data pos in MB field
;
DB UNSIGNED ;signed value
;ARINC WORD 2
;
DB
206Q ;label COMPUTED AIR SPEED
70
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
;
DW
1000 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
10
;number of bits to copy
;
DB
0
;number of discretes
;
DB
37
;status bit pos in MB field
;
DB
38
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 5
;
DB
333Q ;label NORMAL ACCEL.
;
DB
4
;channel
;
DB
BNR ;format
;
DW
100 ;max age ms
;
DB
26
;start bit ARINC word
;
DB
6
;number of bits to copy
;
DB
0
;number of discretes
;
DB
49
;status bit pos in MB field
;
DB
50
;start data pos in MB field
;
DB
SIGNED ;signed value
;
;
;
BDS 70
;
;
DB
070H ;BDS register
DW
1000 ;update interval
DB
4
;number of ARINC words
;ARINC WORD 1
DB
102Q ;label SELECTED ALTITUDE
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
101Q ;label SELECTED HEADING
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
15
;status bit pos in MB field
DB
16
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 3
DB
270Q ;label
ADC BUS DISCRETES
DB
5
;channel
DB
BCD ;format
DW
1000 ;max age ms
DB
26
;start bit ARINC word
DB
14
;number of bits to copy
DB
0
;number of discretes
DB
25
;status bit pos in MB field
DB
26
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 4
DB
271Q ;label
ADC BUS DISCRETES
DB
5
;channel
DB
BCD ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
16
;number of bits to copy
DB
0
;number of discretes
DB
40
;status bit pos in MB field
DB
41
;start data pos in MB field
DB UNSIGNED ;signed value
;
;
DB
080H ;BDS register
DW
1000 ;update interval
EUROCONTROL
DB
5
;number of ARINC words
;ARINC WORD 1
DB
103Q ;label SELECTED AIR SPEED
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
11
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
104Q ;label SELECTED ALTITUDE RATE
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
14
;status bit pos in MB field
DB
15
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 3
DB
102Q ;label SELECTED ALTITUDE
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
26
;status bit pos in MB field
DB
28
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 4
DB
270Q ;label
FMC BUS DISCRETES
DB
6
;channel
DB
BCD ;format
DW
1000 ;max age ms
DB
25
;start bit ARINC word
DB
4
;number of bits to copy
DB
4
;number of discretes
DB
20
;discrete bit n1
DB
15
;discrete bit i
DB
14
;discrete bit r
DB
13
;discrete bit n
DB
40
;status bit pos in MB field
DB
42
;start data pos in MB field
DB UNSIGNED ;signed value
DB
46
;start discrete in MB field
;ARINC WORD 5
DB
271Q ;label
FMC DISCRETES
DB
6
;channel
DB
DISCR ;format
DB
4
;number of discretes
DB
27
;discrete bit
atc
DB
22
;discrete bit
mct
DB
21
;discrete bit
crz
DB
20
;discrete bit
clb
DB
51
;status bit pos in MB field
DB
53
;start data pos in MB field
;
;
DB
090H ;BDS register
DW
1000 ;update interval
DB
5
;number of ARINC words
;ARINC WORD 1
DB
106Q ;label SELECTED MACH NUMBER
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
11
;number of bits to copy
DB
0
;number of discretes
71
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
104Q ;label SELECTED ALTITUDE RATE
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
14
;status bit pos in MB field
DB
15
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 3
DB
102Q ;label
DB
3
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
26
;status bit pos in MB field
DB
28
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 4
DB
270Q ;label
IRS BUS DISCRETES
DB
1
;channel
DB
BCD ;format
DW
1000 ;max age ms
DB
25
;start bit ARINC word
DB
4
;number of bits to copy
DB
4
;number of discretes
DB
20
;discrete bit n1
DB
15
;discrete bit i
DB
14
;discrete bit r
DB
13
;discrete bit n
DB
40
;status bit pos in MB field
DB
42
;start data pos in MB field
DB UNSIGNED ;signed value
DB
46
;start discrete in MB field
;ARINC WORD 5
DB
271Q ;label
IRS BUS DISCRETES
DB
1
;channel
DB
DISCR ;format
DB
4
;number of discretes
DB
27
;discrete bit
atc
DB
22
;discrete bit
mct
DB
21
;discrete bit
crz
DB
20
;discrete bit
clb
DB
51
;status bit pos in MB field
DB
53
;start data pos in MB field
;
;
DB
0A0H ;BDS register
DW
1000 ;update interval
DB
3
;number of ARINC words
;ARINC WORD 1
DB
116Q ;label CROSS TRACK ERROR
DB
6
;channel
DB
BNR ;format
DW
125 ;max age ms
DB
28
;start bit ARINC word
DB
15
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
117Q ;label VERTICAL DEVIATION
DB
6
;channel
DB
BNR ;format
DW
125 ;max age ms
DB
28
;start bit ARINC word
EUROCONTROL
DB
11
;number of bits to copy
DB
0
;number of discretes
DB
18
;status bit pos in MB field
DB
19
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 3
DB
333Q ;label NORMAL ACCELERATION
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
26
;start bit ARINC word
DB
6
;number of bits to copy
DB
0
;number of discretes
DB
31
;status bit pos in MB field
DB
32
;start data pos in MB field
DB
SIGNED ;signed value
;
;
DB
0B0H ;BDS register
DW
1000 ;update interval
DB
4
;number of ARINC words
;ARINC WORD 1
DB
206Q ;label COMPUTED AIR SPEED
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
210Q ;label TRUE AIRSPEED
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
15
;status bit pos in MB field
DB
17
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 3
DB
205Q ;label MACH NUMBER
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
DB
28
;start bit ARINC word
DB
14
;number of bits to copy
DB
0
;number of discretes
DB
29
;status bit pos in MB field
DB
31
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 4
DB
320Q ;label MAGNETIC HEADING
DB
1
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
45
;status bit pos in MB field
DB
46
;start data pos in MB field
DB
SIGNED ;signed value
;
;
DB
0C0H ;BDS register
DW
1000 ;update interval
DB
3
;number of ARINC words
;ARINC WORD 1
DB
164Q ;label RADIO HEIGHT
DB
7
;channel
DB
BNR ;format
72
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
13
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
217Q ;label
STATIC PRESSURE
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
DB
27
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
16
;status bit pos in MB field
DB
18
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 3
DB
203Q ;label ALTITUDE 1013.25mb
DB
5
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
17
;number of bits to copy
DB
0
;number of discretes
DB
30
;status bit pos in MB field
DB
32
;start data pos in MB field
DB UNSIGNED ;signed value
;
;
DB
071H ;BDS register
DW
1000 ;update interval
DB
6
;number of ARINC words
;ARINC WORD 1
DB
325Q ;label ROLL ANGLE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
27
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
365Q ;label INERTIAL VERTICAL VELOCITY
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
26
;start bit ARINC word
DB
6
;number of bits to copy
DB
0
;number of discretes
DB
11
;status bit pos in MB field
DB
12
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 3
DB
315Q ;label WIND SPEED
DB
1
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
19
;status bit pos in MB field
DB
21
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 4
DB
316Q ;label WIND ANGLE
DB
1
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
EUROCONTROL
DB
0
;number of discretes
DB
29
;status bit pos in MB field
DB
30
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 5
DB
213Q ;label STATIC AIR TEMP.
DB
5
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
39
;status bit pos in MB field
DB
40
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 6
DB
333Q ;label NORMAL ACCELERATION
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
26
;start bit ARINC word
DB
4
;number of bits to copy
DB
0
;number of discretes
DB
51
;status bit pos in MB field
DB
52
;start data pos in MB field
DB
SIGNED ;signed value
;
;
DB
021H ;BDS register
DW
1000 ;update interval
DB
5
;number of ARINC words
;ARINC WORD 1
DB
320Q ;label MAGNETIC HEADING
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
210Q ;label TRUE AIR SPEED
DB
5
;channel
DB
BNR ;format
DW
250 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
13
;status bit pos in MB field
DB
15
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 3
DB
365Q ;label INERTIAL VERTICAL VELOCITY
DB
1
;channel
DB
BNR ;format
DW
125 ;max age ms
DB
27
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
27
;status bit pos in MB field
DB
28
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 4
DB
213Q ;label STATIC AIR TEMP.
DB
5
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
37
;status bit pos in MB field
DB
38
;start data pos in MB field
73
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DB
SIGNED ;signed value
;ARINC WORD 5
DB
333Q ;label NORMAL ACCELERATION
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
26
;start bit ARINC word
DB
6
;number of bits to copy
DB
0
;number of discretes
DB
49
;status bit pos in MB field
DB
50
;start data pos in MB field
DB
SIGNED ;signed value
;
;
DB
031H ;BDS register
DW
1000 ;update interval
DB
3
;number of ARINC words
;ARINC WORD 1
DB
115Q ;label BEARING TO WAYPOINT
DB
6
;channel
DB
BNR ;format
DW
125 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
002Q ;label TIME TO GO
DB
6
;channel
DB
BCD ;format
DW
1000 ;max age ms
DB
29
;start bit ARINC word
DB
15
;number of bits to copy
DB
0
;number of discretes
DB
13
;status bit pos in MB field
DB
14
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 3
DB
001Q ;label DISTANCE TO GO
DB
6
;channel
DB
BCD ;format
DW
1000 ;max age ms
DB
29
;start bit ARINC word
DB
19
;number of bits to copy
DB
0
;number of discretes
DB
29
;status bit pos in MB field
DB
30
;start data pos in MB field
DB
SIGNED ;signed value
;
;
DB
041H ;BDS register
DW
1000 ;update interval
DB
3
;number of ARINC words
;ARINC WORD 1
DB
356Q ;label ACTIVE WAYPOINT 1
DB
6
;channel
DB
TRANS ;format
DW
1000 ;max age ms
DB
29
;start bit ARINC word
DB
21
;number of bits to copy
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
;ARINC WORD 2
DB
357Q ;label ACTIVE WAYPOINT 2
DB
6
;channel
DB
TRANS ;format
DW
1000 ;max age ms
DB
29
;start bit ARINC word
DB
21
;number of bits to copy
DB
23
;status bit pos in MB field
DB
24
;start data pos in MB field
;ARINC WORD 3
DB
DB
DB
DW
DB
DB
DB
DB
DB
DB
EUROCONTROL
114Q ;label DESIRED TRACK
6
;channel
BNR ;format
400 ;max age ms
28
;start bit ARINC word
10
;number of bits to copy
0
;number of discretes
45
;status bit pos in MB field
46
;start data pos in MB field
SIGNED ;signed value
;
;
;
DB
051H ;BDS register
;
DW
1000 ;update interval
;
DB
3
;number of ARINC words
;ARINC WORD 1
;
DB
310Q ;label LATITUDE
;
DB
6
;channel
;
DB
BNR ;format
;
DW
400 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
18
;number of bits to copy
;
DB
0
;number of discretes
;
DB
1
;status bit pos in MB field
;
DB
2
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 2
;
DB
311Q ;label LONGITUDE
;
DB
6
;channel
;
DB
BNR ;format
;
DW
400 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
18
;number of bits to copy
;
DB
0
;number of discretes
;
DB
21
;status bit pos in MB field
;
DB
22
;start data pos in MB field
;
DB
SIGNED ;signed value
;ARINC WORD 3
;
DB
203Q ;label ALTITUDE
;
DB
5
;channel
;
DB
BNR ;format
;
DW
125 ;max age ms
;
DB
28
;start bit ARINC word
;
DB
14
;number of bits to copy
;
DB
0
;number of discretes
;
DB
41
;status bit pos in MB field
;
DB
42
;start data pos in MB field
;
DB
SIGNED ;signed value
;
;
DB
061H ;BDS register
DW
1000 ;update interval
DB
2
;number of ARINC words
;ARINC WORD 1
DB
150Q ;label GMT
DB
1
;channel
DB
BNR ;format
DW
2000 ;max age ms
DB
28
;start bit ARINC word
DB
17
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
261Q ;label FLIGHT NUMBER
DB
6
;channel
DB
BCD ;format
DW
2000 ;max age ms
DB
29
;start bit ARINC word
DB
16
;number of bits to copy
DB
0
;number of discretes
DB
20
;status bit pos in MB field
DB
21
;start data pos in MB field
74
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DB
UNSIGNED ;signed value
DB
DB
DB
;
;
DB
024H ;BDS register
DW
5000 ;update interval
DB
2
;number of ARINC words
;ARINC WORD 1
DB
066Q ;label CENTRE OF GRAVITY
DB
6
;channel
DB
BCD ;format
DW
2000 ;max age ms
DB
27
;start bit ARINC word
DB
13
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
075Q ;label GROSS WEIGHT
DB
6
;channel
DB
BNR ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
13
;number of bits to copy
DB
0
;number of discretes
DB
16
;status bit pos in MB field
DB
18
;start data pos in MB field
DB UNSIGNED ;signed value
;
;
DB
017H ;BDS register
DW
1000 ;update interval
DB
4
;number of ARINC words
;ARINC WORD 1
DB
021Q ;label
N1 TARGET ENGINE 1
DB
6
;channel
DB
BCD ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
11
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
347Q ;label FUEL FLOW ENGINE 1
DB
6
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
14
;status bit pos in MB field
DB
16
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 3
DB
211Q ;label TOTAL AIR TEMP.
DB
5
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
28
;status bit pos in MB field
DB
29
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 4
DB
213Q ;label STATIC AIR TEMP.
DB
5
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
EUROCONTROL
40
;status bit pos in MB field
41
;start data pos in MB field
SIGNED ;signed value
;
;
DB
027H ;BDS register
DW
1000 ;update interval
DB
4
;number of ARINC words
;ARINC WORD 1
DB
021Q ;label N1 TARGET ENGINE 2
DB
6
;channel
DB
BCD+SDI2 ;format
DW
400 ;max age ms
DB
28
;start bit ARINC word
DB
11
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
3
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
347Q ;label FUEL FLOW ENGINE 2
DB
6
;channel
DB
BNR+SDI2 ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
14
;status bit pos in MB field
DB
16
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 3
DB
211Q ;label TOTAL AIR TEMP.
DB
5
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
28
;status bit pos in MB field
DB
29
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 4
DB
213Q ;label STATIC AIR TEMP.
DB
5
;channel
DB
BNR ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
40
;status bit pos in MB field
DB
41
;start data pos in MB field
DB
SIGNED ;signed value
;
;
DB
02AH ;BDS register
DW
10000 ;update interval
DB
2
;number of ARINC words
;ARINC WORD 1
DB
030Q ;label VHF FREQUENCY COM 1
DB
6
;channel
DB
BNR+SDI1 ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
DB
14
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 2
DB
030Q ;label VHF FREQUENCY COM 2
DB
6
;channel
DB
BNR+SDI2 ;format
DW
1000 ;max age ms
DB
28
;start bit ARINC word
75
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DB
DB
DB
DB
DB
14
;number of bits to copy
0
;number of discretes
16
;status bit pos in MB field
17
;start data pos in MB field
UNSIGNED ;signed value
EUROCONTROL
DB
325Q ;label ROLL ANGLE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
26
;start bit ARINC word
DB
6
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
327Q ;label ROLL RATE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
7
;number of bits to copy
DB
0
;number of discretes
DB
9
;status bit pos in MB field
DB
10
;start data pos in MB field
DB
SIGNED ;sign
;ARINC WORD 3
DB
335Q ;label TRACK ANGLE RATE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
7
;number of bits to copy
DB
0
;number of discretes
DB
18
;status bit pos in MB field
DB
19
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 4
DB
320Q ;label MAGNETIC HEADING
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
27
;status bit pos in MB field
DB
28
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 5
DB
363Q ;label CROSS TRACK ACCELERATION
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
25
;start bit ARINC word
DB
7
;number of bits to copy
DB
0
;number of discretes
DB
41
;status bit pos in MB field
DB
42
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 6
DB
376Q ;label CROSS HEADING
ACCELERATION (not beluga)
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
25
;start bit ARINC word
DB
7
;number of bits to copy
DB
0
;number of discretes
DB
49
;status bit pos in MB field
DB
50
;start data pos in MB field
DB UNSIGNED ;signed value
;
; D2 START of TURN INDICATION REPORT
;
DB
0D2H ;BDS register
DW
1000 ;update interval
DB
6
;number of ARINC words
;ARINC WORD 1
DB
325Q ;label ROLL ANGLE
;
; D0 START of TURN INDICATION REPORT
;
DB
0D0H ;BDS register
DW
1000 ;update interval
DB
5
;number of ARINC words
;ARINC WORD 1
DB
100Q ;label SELECTED COURSE ( NOT
BELUGA)
DB
3
;channel
DB
BNR ;format
DW
300 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
101Q ;label SELECTED HEADING
DB
3
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
11
;status bit pos in MB field
DB
12
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 3
DB
102Q ;label SELECTED ALTITUDE
DB
3
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
21
;status bit pos in MB field
DB
22
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 4
DB
114Q ;label DESIRED TRACK (NOT BELUGA)
DB
6
;channel
DB
BNR ;format
DW
200 ;max age ms
DB
28
;start bit ARINC word
DB
8
;number of bits to copy
DB
0
;number of discretes
DB
35
;status bit pos in MB field
DB
36
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 5
DB
365Q ;label INERTIAL VERTICAL VELOCITY
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
10
;number of bits to copy
DB
0
;number of discretes
DB
45
;status bit pos in MB field
DB
46
;start data pos in MB field
DB
SIGNED ;signed value
;
; D1 START of TURN INDICATION REPORT
;
DB
0D1H ;BDS register
DW
1000 ;update interval
DB
6
;number of ARINC words
;ARINC WORD 1
76
BDS Allocation Table for A300 Beluga
This ADLP table defines the position and range of each available aircraft parameter in the
transponder GICB registers
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
26
;start bit ARINC word
DB
6
;number of bits to copy
DB
0
;number of discretes
DB
1
;status bit pos in MB field
DB
2
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 2
DB
327Q ;label ROLL RATE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
7
;number of bits to copy
DB
0
;number of discretes
DB
9
;status bit pos in MB field
DB
10
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 3
DB
335Q ;label TRACK ANGLE RATE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
7
;number of bits to copy
DB
0
;number of discretes
DB
18
;status bit pos in MB field
DB
19
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 4
DB
313Q ;label TRACK ANGLE TRUE
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
28
;start bit ARINC word
DB
12
;number of bits to copy
DB
0
;number of discretes
DB
27
;status bit pos in MB field
DB
28
;start data pos in MB field
DB
SIGNED ;signed value
;ARINC WORD 5
DB
363Q ;label CROSS TRACK ACCELERATION
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
25
;start bit ARINC word
DB
7
;number of bits to copy
DB
0
;number of discretes
DB
41
;status bit pos in MB field
DB
42
;start data pos in MB field
DB UNSIGNED ;signed value
;ARINC WORD 6
DB
376Q ;label CROSS HEADING
ACCELERATION (NOT BELUGA)
DB
1
;channel
DB
BNR ;format
DW
100 ;max age ms
DB
25
;start bit ARINC word
DB
7
;number of bits to copy
DB
0
;number of discretes
DB
49
;status bit pos in MB field
DB
50
;start data pos in MB field
DB UNSIGNED ;signed value
_
77
EUROCONTROL