Beechcraft Baron G58 Pilot Operating Handbook page 140

Model G58
ABNORMAL PROCEDURES
TABLE OF CONTENTS (CONT'D)
SUBJECT
Transponder Failure . . . . . . . . . . . . . . . . . . . . . . . . . . 3A-16
Engine and/or Fuel Display Failure . . . . . . . . . . . . . . . 3A-16
Erroneous Failure Displays . . . . . . . . . . . . . . . . . . . . . 3A-17
Failed Heading During Ground Operations. . . . . . . . . 3A-18
System Failure without an
associated Failure Display . . . . . . . . . . . . . . . . . . . . . 3A-18
Failure of Cooling Fans [PFD FAN FAIL],
[MFD FAN FAIL] or [AVIONICS FAN]
Advisory Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . 3A-18
Global Positioning System (GPS) . . . . . . . . . . . . . . . . 3A-19
Loss of, or Invalid GPS Signal . . . . . . . . . . . . . . . . . 3A-19
Position Error [POSN ERROR] . . . . . . . . . . . . . . . . 3A-19
Failure of Remote Autonomous Integrity
Monitoring (RAIM). . . . . . . . . . . . . . . . . . . . . . . . . 3A-19
Garmin Terrain Awareness and
Warning System (TAWS) . . . . . . . . . . . . . . . . . . . . . 3A-20
TAWS Forward Looking Caution [TERRAIN] . . . . . 3A-20
Excessive Descent Rate Caution [TERRAIN] . . . . . 3A-21
Negative Climb Rate After Takeoff [TERRAIN] . . . . 3A-22
Premature Descent During
An Approach [TERRAIN] . . . . . . . . . . . . . . . . . . . . 3A-23
Ditching, Off-Airport Landing,
or Flying VFR Around Unique Terrain . . . . . . . . . . 3A-23
Altimeter Disagreement . . . . . . . . . . . . . . . . . . . . . . 3A-23
Additional Caution Annunciations . . . . . . . . . . . . . . . . 3A-24
Oil Pressure Low [OIL PRESS LO] . . . . . . . . . . . . . 3A-25
Fuel Quantity Low [FUEL QTY LO] . . . . . . . . . . . . . 3A-25
Alternator Load High [ALT LOAD] . . . . . . . . . . . . . . 3A-25
Surface Deice Air Pump
[L AIR PUMP] or [R AIR PUMP] . . . . . . . . . . . . . . 3A-26
3A-2
SECTION 3A
PAGE
April, 2008