09.12.2012 Views

NOTICE

NOTICE

NOTICE

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

CESSNA SECTION 7<br />

MODEL 208B G1000 AIRPLANE AND SYSTEMS DESCRIPTION<br />

TORQUE INDICATIONS<br />

Torque (TRQ) indication is displayed at the top of both the ENGINE and<br />

SYSTEM pages. The indicator is a round gage with a white pointer. The<br />

transmitter senses the difference between the engine torque pressure<br />

and the pressure in the engine case and transmits this data to the<br />

G1000. Normal operating range is indicated by a green arc that<br />

extends from 0 to redline. Redline varies from 1865 to 1970 ft-lbs<br />

depending on prop RPM.<br />

For normal cruise flight when prop RPM is between 1600-1900, a blue<br />

torque “bug” is included on the arc. This indicates maximum allowed<br />

cruise torque per the cruise performance and maximum torque charts<br />

in section 5, Performance. The blue advisory cruise torque bug located<br />

on the EIS torque indication is not to be used as the primary means of<br />

setting cruise torque. Always refer to the appropriate performance chart<br />

in Section 5 of the POH/AFM.<br />

PROPELLER RPM INDICATIONS<br />

The propeller RPM (PROP RPM) is indicated numerically below Gas<br />

Generator RPM. The digits are white with RPM between 0-1599 RPM,<br />

green between 1600-1900 RPM, and white with a red background<br />

when RPM is greater than or equal to 1910. The instrument is<br />

electrically operated from the propeller tachometer-generator which is<br />

mounted on the right side of the front case.<br />

ITT INDICATION<br />

Interstage Turbine Temperature (ITT) is indicated below torque and is<br />

round dial gage with a white pointer. This instrument displays gas<br />

temperature between the compressor and power turbines. With the<br />

engine off or during start ITT indicator displays a green band from<br />

100°C to 740°C, an Amber caution band from 766°C-805°C and a<br />

redline at 1090°C. The gage is graduated at 100 degree intervals from<br />

600°C to 1100°C.<br />

With the engine running a green arc indicates normal operating range<br />

from 100°C to 740°C, an Amber caution region from 765°C-805°C with<br />

a redline at 805°C. The gage is graduated at 50 degree intervals from<br />

600°C-900°C. The digital readout flashes red when an overtemperature<br />

situation has occurred.<br />

GAS GENERATOR RPM INDICATIONS<br />

Gas generator RPM (N g) is displayed below ITT using a round dial<br />

gage with a white pointer. RPM is displayed as a percentage of<br />

maximum gas generator RPM. The instrument is electrically operated<br />

from the gas generator tachometer-generator mounted on the lower<br />

right portion of the accessory case. The gage has tick marks at 0, 12,<br />

50, and 105% with a redline at 101.6%.<br />

208BPHBUS-00<br />

U.S.<br />

7-47

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!