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SECTION 3 CESSNA ABNORMAL PROCEDURES MODEL 208B G1000 ALTITUDE MISCOMPARE (Amber ALT MISCOMP INDICATION PFD) (Continued) IF PILOT PFD AND STANDBY ALTIMETER AGREE (COPILOT PFD STILL DIFFERS) 6. Compare indicated altitude to GPS altitude on MFD AUX-GPS STATUS page to aid in determining which primary system is most accurate. NOTE • When comparing indicated altitude to GPS altitude, deviations from standard temperature or pressure can cause indicated altitude to deviate from GPS altitude. These errors are largest at high altitude and can amount to over 2,500 feet under some conditions. However, below 10,000 feet with the correct local altimeter setting set, GPS altitude will usually be within 600 feet or better of the correct indicated altitude. Use the following guidelines to help estimate correct altitude for nonstandard conditions: • Temperatures WARMER than standard can cause GPS altitude to read HIGHER than indicated altitude. • Pressures LOWER than standard can cause GPS altitude to read HIGHER than indicated altitude. IF ABLE TO IDENTIFY ACCURATE ALTITUDE SOURCE 5. Use SENSOR REVERSION to select most accurate ADC on both PFDs. 6. Land as soon as practical. IF UNABLE TO IDENTIFY ACCURATE ALTITUDE SOURCE 5. Land as soon as practical. Consider diversion to visual conditions. 6. Maintain altitudes based on LOWEST indicated altitude. 7. ATC . . . . . . . . . . . ADVISE (of inability to verify correct altitude) 8. If unable to descend into visual conditions, plan ILS approach with course intercept well outside the Final Approach Fix (FAF). 9. Once glideslope is captured, determine most accurate altitude source when crossing FAF. 3-54 U.S. (Continued Next Page) FAA APPROVED 208BPHBUS-01
CESSNA SECTION 3 MODEL 208B G1000 ABNORMAL PROCEDURES ALTITUDE MISCOMPARE (Amber ALT MISCOMP INDICATION PFD) (Continued) 10. Reference ILS Decision Height to most accurate altimeter based on FAF crossing. WARNING TAWS alerts are based on GPS altitude and position information and are independent of ADC data. If a TAWS alert is received, it should be considered valid and appropriate terrain avoidance action should be taken. AIRSPEED MISCOMPARE (Amber IAS MISCOMP INDICATION PFD) 1. Pilot and Copilot Airspeed . . . . . . . . . . . . . . . . . . . . COMPARE (with Standby Airspeed Indicator) WARNING The Standby Airspeed Indicator uses the same Pitot-Static sources as the pilot’s side air data computer (ADC1). Do not use Standby Airspeed Indicator as sole source in determining correct airspeed. (Continued Next Page) FAA APPROVED 208BPHBUS-01 U.S. 3-55
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CESSNA INTRODUCTION MODEL 208B G100
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CESSNA SECTION 1 MODEL 208B G1000 G
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CESSNA SECTION 2 MODEL 208B G1000 L
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SECTION 3 CESSNA EMERGENCY PROCEDUR
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CESSNA SECTION 4 MODEL 208B G1000 N
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CESSNA SECTION 5 MODEL 208B G1000 P
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CESSNA SECTION 6 MODEL 208B G1000 W
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CESSNA SECTION 7 MODEL 208B G1000 A
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SECTION 7 CESSNA AIRPLANE AND SYSTE
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CESSNA SECTION 8 MODEL 208B G1000 H
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