Beechcraft Baron G58 Pilot Operating Handbook page 110

Model G58
EMERGENCY PROCEDURES
TABLE OF CONTENTS (CONT'D)
SUBJECT
Autopilot Response to Erroneous AHRS Input . . . . . 3-17
Electric Pitch Trim Failure [PTRM] . . . . . . . . . . . . . . 3-17
Unscheduled Electric Pitch Trim . . . . . . . . . . . . . . . . . . 3-18
Air Data Computer (ADC) Failure . . . . . . . . . . . . . . . . . 3-19
Attitude and Heading Reference
System (AHRS) Failure. . . . . . . . . . . . . . . . . . . . . . . . . 3-19
Failure of PFD or MFD . . . . . . . . . . . . . . . . . . . . . . . . . 3-19
Failure of PFD and MFD . . . . . . . . . . . . . . . . . . . . . . . . 3-20
Emergency Communications . . . . . . . . . . . . . . . . . . . . 3-20
Garmin Terrain Awareness and
Warning System (TAWS) . . . . . . . . . . . . . . . . . . . . . . 3-20
TAWS Forward Looking
Terrain Warning [PULL UP] . . . . . . . . . . . . . . . . . . . 3-20
Excessive Descent Rate Warning [PULL UP] . . . . . . 3-23
Additional Warning Annunciations . . . . . . . . . . . . . . . . 3-24
Fuel Flow High [FUEL FLOW HI] . . . . . . . . . . . . . . . 3-24
Cylinder Head Temperature High [CHT HI] . . . . . . . . 3-25
Oil Temperature High [OIL TEMP HI] . . . . . . . . . . . . 3-25
Oil Pressure High [OIL PRESS HI] . . . . . . . . . . . . . . 3-26
Oil Pressure Low [OIL PRESS LO] . . . . . . . . . . . . . . 3-26
Fuel Quantity Low [FUEL QTY LO] . . . . . . . . . . . . . . 3-26
Emergency Exits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-26
Spins . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-27
Severe Icing Conditions (Alternate Method of
Compliance With FAA AD 98-04-24). . . . . . . . . . . . . . 3-28
3-2
SECTION 3
PAGE
April, 2008