getting to grips with surveillance(122)

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12.4.3.1. & 12.4.3.2. To request the capability of the SSR or ADS-B equipment  ADVISE TRANSPONDER CAPABILITY  ADVISE ADS-B CAPABILITY 
To advise the capability of the SSR or ADS-B equipment  TRANSPONDER (ALPHA, CHARLIE or SIERRA as shown in the flight plan) NEGATIVE TRANSPONDER  ADS-B TRANSMITTER (data link*); ADS-B RECEIVER (data link*) * As AIRBUS aircraft use the 1090 ES data link, TEN NINETY DATA LINK should be announced. NEGATIVE ADS-B 
12.4.3.4. & 12.4.3.5. To  RESET SQUAWK  RE-ENTER [ADS-B or 
request the pilot to  [(mode)] (code)  MODE S] AIRCRAFT 
reselect the assigned  IDENTIFICATION 
mode and code or the  Note: Not able to comply 
aircraft identification  with some FMS standards (see note in 2.5.2.2 – For the Flight Crew). Refer to AIP for alternative 
- B-1 -

 

Circumstances
Radar
ADS-B
procedures.
Read back
RESETTING (mode)
Not defined
(code)
12.4.3.7. To request the operation of the IDENT feature
SQUAWK [(code)]
TRANSMIT ADS-B [AND] IDENT
IDENT
Note: Transponder and ADS-B transmitter are coupled on AIRBUS aircraft. Activate the IDENT function as in radar coverage.
12.4.3.10. To request the
STOP SQUAWK
STOP ADS-B

termination of [TRANSMIT ADS-B TRANSMISSION
transponder or ADS-B
ONLY]
[SQUAWK (code)

transmitter operation ONLY]
Note: Not able to comply with on AIRBUS aircraft. Refer to AIP for alternative procedures.
12.4.3.11. To request SQUAWK CHARLIE TRANSMIT ADS-B
transmission of pressure-ALTITUDE
altitude Note: Transponder and ADS-B transmitter are coupled on AIRBUS aircraft. Activate the altitude reporting as in radar coverage.
12.4.3.13. To request termination of pressure-
altitude  transmission 
because  of  faulty 
operation 

STOP  SQUAWK 
CHARLIE  WRONG 
INDICATION 

STOP ADS-B ALTITUDE

TRANSMISSION 
[(WRONG 
INDICATION,  or 
reason)] 
Note:  Transponder  and 
ADS-B  transmitter  are 

coupled on AIRBUS aircraft. Refer to 2.5.2.2
– For the Flight Crew.

APPENDIX C – ATSAW IN TRAIL PROCEDURE (ITP)
This appendix provides details on ITP with the use of ATSAW. This appendix:
- Gives the definitions of terms commonly used for ITP
- Describes the ITP procedure in details
- Gives a practical example with cockpit interfaces.
The ITP description is compliant with standards published at the time of writing the brochure. The readers must ensure to take into account any updates of ITP standards.
C.1. DEFINITIONS
Ground Speed Difference of ground speed between the ITP aircraft and the Differential Reference Aircraft. The ground speed differential is positive
　
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