NOTICE

SECTION 7 CESSNA
AIRPLANE AND SYSTEMS DESCRIPTION MODEL 208B G1000
FUEL FLOW INDICATIONS
Details of the fuel flow indicator are included under Fuel System in a
later paragraph in this section.
OIL PRESSURE INDICATION
Oil Pressure (OIL PSI) is displayed using a varied color tape and 3 digit
display on the ENGINE page. Oil pressure is indicated using a
transducer that senses oil pressure from the accessory case and
transmits the information to the G1000. Normal operation is indicated
from 85 to 105 psi; caution region is indicated by an amber bar from 40
psi to less than 85 psi. Warning region is indicated by red lines and red
flashing digits at less than 40 psi and greater that 105 psi
OIL TEMPERATURE INDICATION
Oil temperature (OIL °C) is displayed using a varied color tape and
digital display; the display can be 3 digits on the ENGINE page. The
instrument is operated by an electrical-resistance type temperature
sensor. Normal operation is indicated between 10 and 99°C; AMBER
caution regions are indicated from -40 to less than 10°C and from 100
to 104°C. Red lines are included at -41 and 105°C. Digits vary in color
between green, amber or red in correlation with the pointer and tape.
NEW ENGINE BREAK-IN AND OPERATION
There are no specific break-in procedures required for the Pratt &
Whitney Canada Inc. PT6A-114A turboprop engine. The engine may be
safely operated throughout the normal ranges authorized by the
manufacturer at the time of delivery of your airplane.
7-48
U.S.
208BPHBUS-00