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CESSNA SECTION 2<br />

MODEL 208B G1000 LIMITATIONS<br />

INTRODUCTION<br />

Section 2 includes the operating limitations, instrument markings, and<br />

basic placards necessary for the safe operation of the airplane, its<br />

engine, standard/non-standard systems and standard/non-standard<br />

equipment.<br />

FAA APPROVED<br />

208BPHBUS-00<br />

WARNING<br />

The limitations included in this section and in<br />

Section 9 have been approved by the Federal<br />

Aviation Administration. Observance of these<br />

operating limitations is required by federal aviation<br />

regulations.<br />

NOTE<br />

• Operation in countries other than the United States may<br />

require observance of other limitations, procedures or<br />

performance data.<br />

• Refer to Section 9 of this POH/AFM for amended<br />

operating limitations, procedures, performance data and<br />

other necessary information for supplemental systems.<br />

• The airspeeds listed in Airspeed Limitations chart, and<br />

Airspeed Indicator Markings chart are based on<br />

Airspeed Calibration data shown in Section 5 with the<br />

normal static source. If the alternate static source is<br />

being used, ample margins should be observed to allow<br />

for the airspeed calibration variations between the<br />

normal and alternate static sources as shown in Section<br />

5.<br />

Your Cessna is certificated under FAA Type Certificate No. A37CE as<br />

Cessna Model No. 208B.<br />

U.S.<br />

2-3

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