Garmin G5000 Airplane Flight Manual Supplement page 128

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Model 560XL
If high speed buffet is encountered when initially responding to an RA, relax
pitch force as necessary to reduce buffet, but still continue to maneuver to
the TCAS pitch command.
If stall warning occurs during an RA maneuver, immediately abandon the
RA and execute stall recovery procedures. TCAS II will continue to provide
RAs during stall warning and recovery procedure.
Exaggerated responses to TCAS RAs are not desirable or appropriate
because of the other potential traffic conflicts and ATC consequences.
From level flight, proper response to TCAS RA typically results in an overall
altitude deviation of 300 to 500 feet in order to successfully resolve a traffic
conflict.
If a CLIMB RA is issued with the airplane in the landing configuration, a
normal go-around should be initiated including the appropriate thrust
increase and configuration change.
Maneuvering should be made with the autopilot disengaged, and limited to
the minimum required to comply with RA.
The pilot should not initiate evasive maneuvers using information from the
traffic display only or on a Traffic Advisory only, without visually acquiring
the traffic.
Compliance with TCAS resolution advisories is required unless the pilot
considers it unsafe to do so.
The pilot should promptly return to the previous ATC clearance after the
TCAS voice message "Clear of Conflict" is announced.
An immediate, smooth response to an RA is required to obtain maximum
separation. While TCAS II algorithms are based upon the pilot initiating the
initial maneuver within 5 seconds of the RA, and within 2 1/2 seconds for
additional corrective RAs (increases or reversals), any delay in responding
to RAs will reduce the separation provided.
3. TCAS II range selection:
a. A 12 NM (or lower) range may be selected for takeoff, low altitude climb, approach and
landing, and below 10,000 feet.
b. A 12 NM (or greater) range may be selected for high altitude cruise.
c. The range selected has no effect on the TCAS II logic giving TAs and RAs.
4. TA only mode:
a. TA only mode can be selected via the GTC. This should be used to preclude unnecessary
RAs when operating near closely spaced parallel runways.
b. All resolution advisories (RAs) are inhibited when TA only mode is selected.
c. The TA only mode should be selected following an in-flight engine shutdown.
Textron Aviation Citation 560XL
3-86
Section III – Operating Procedures
Operating Information
190-02313-03 Rev. 8
FAA Approved

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