Model 560XL Section III – Operating Procedures
Abnormal Procedures
Textron Aviation Citation 560XL 190-02313-03 Rev. 8
3-54 FAA Approved
TRANSPONDER FAIL 1-2
FTRANSPONDER FAIL 1-2F CAS message displayed
This CAS message indicates that a failure of both transponders has been detected. This message
will only display when airborne.
1. XPDR 1 and XPDR 2 Circuit Breakers (RH Panel) – IN.
2. If neither transponder comes on:
a. TCAS may be inoperative, check Traffic display.
b. With transponders inoperative, perform appropriate RVSM contingency procedures for the
loss of altitude reporting.
Procedure completed
AVIONICS FAULT
AVIONICS FAULT CAS message displayed
This CAS message indicates that a fault has been detected in the avionics system. Inoperable
systems can be identified through failure indications and/or by checking the GTC system messages.
ON THE GROUND
1. Check GTC system messages and note the fault.
2. Correct prior to flight.
Procedure completed
IN FLIGHT
1. Flight may be continued in a normal manner. The fault must be corrected prior to subsequent
flight.
Procedure completed
AOA FAIL
AOA FAIL CAS message displayed
1. Minimum Airspeed – Flaps 0° – V
REF
+15 KIAS
Flaps 7° – V
REF
+10 KIAS
Flaps 15° – V
APP
Flaps 35° – V
REF
NOTE
Underspeed protection will not be available.
The following systems will be inoperative:
Stall warning (stick shaker) Angle-of-attack gauge
Low speed awareness Angle-of-attack indexer
Procedure completed
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