Monitoring Engine Systems (Oil, Fuel, Electrical) - Beechcraft Baron G58 Pilot Operating Handbook

Serials th-2125 and after
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Section 4
Normal Procedures
3. The engine should not be operated closer to peak EGT
than 20°C (rich side or lean side) as indicated on the
MANIFOLD PRESSURE vs RPM graph (Section 5,
PERFORMANCE).
4. If engine roughness is encountered operating at lower
power settings on the lean side of peak, enrich the mix-
ture slightly for smooth engine operation.
5. If required fuel flows cannot be achieved when leaning to
the rich side of peak, switch the fuel boost pump to LO,
then lean as required.
6. Changes in altitude and power settings require the peak
EGT to be rechecked and the mixture reset.
7. MFD Softkeys . . . . .RETURN TO MAIN ENGINE PAGE
A Lean Assist function is available through
the Garmin software utilizing the CYL SLCT
and ASSIST Softkeys. Reference Garmin
Cockpit Reference Guide for details on the
procedure.
MONITORING ENGINE SYSTEMS (OIL, FUEL,
ELECTRICAL)
The Engine Systems page is found on the MFD.
1. ENGINE Soft Key . . . . . . . . . . . . . . . . . . . . . . . . PRESS
2. SYSTEM Soft Key . . . . . . . . . . . . . . . . . . . . . . . . PRESS
3. MFD Softkeys . . . . .RETURN TO MAIN ENGINE PAGE
4-30
NOTE
Model G58
April, 2012

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