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Cirrus System 55X Autopilot User Manual

Cirrus System 55X Autopilot
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Cirrus Design Section 4
SR22T Normal Procedures
P/N 13772-005 4-15P/N 13772-005 4-15
indicate faulty grounding of one side of the ignition system or magneto
timing set in advance of the specified setting.
Maximum Power Fuel Flow
For maximum power operations (Power Lever full forward - 2500 RPM,
36.0 in.Hg manifold pressure) fuel flow should be in the green arc.
For any power setting greater than 30.5 in.Hg (cruise power) fuel flow
is indicated by a dynamically calculated green arc displayed on the
fuel gage. Fuel flow should be maintained within this arc by use of the
mixture lever.
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Cirrus System 55X Autopilot Specifications

General IconGeneral
BrandCirrus
ModelSystem 55X Autopilot
CategoryAircrafts
LanguageEnglish

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