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Cirrus DESIGN SR22T - Original Issue; EGT, TIT or CHT Temperature Sensor Failure

Cirrus DESIGN SR22T
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3-26 P/N 13772-003
Section 3 Cirrus Design
Emergency Procedures SR22T
EGT, TIT or CHT Temperature Sensor Failure
1. Similar gages ................................................................. MONITOR
2. Flight ............................................................................ CONTINUE
using remaining gages as representative.
Amplification
Isolated red X presentation of an EGT, TIT or CHT indicates that
sensor has failed. Continued flight is permitted, using the remaining
gages as representative of the failed gage; control airspeed or mixture
in a normal manner to maintain the other cylinders or TIT within their
normal operating ranges.
Original Issue

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