Beechcraft Baron G58 Pilot Operating Handbook page 465

CONTENTS
SECTION 1 - GENERAL . . . . . . . . . . . . . . . . . . . Page 3 of 24
SECTION 2 - LIMITATIONS . . . . . . . . . . . . . . . . Page 3 of 24
SECTION 3 - EMERGENCY PROCEDURES . . . Page 4 of 24
SECTION 3A - ABNORMAL PROCEDURES . . . Page 4 of 24
SECTION 4 - NORMAL PROCEDURES . . . . . . . Page 5 of 24
SECTION 5 - PERFORMANCE. . . . . . . . . . . . . . Page 9 of 24
SECTION 6 - WT AND BAL/EQUIP. . . . . . . . . . Page 11 of 24
Section 7 - SYSTEMS DESCRIPTION . . . . . . . Page 11 of 24
SECTION 8 - HANDLING, SERV AND MAINT . Page 24 of 24
SECTION 1 - GENERAL
The information in this supplement is FAA-approved material
and must be attached to the Pilot's Operating Handbook and
FAA Approved Airplane Flight Manual when the airplane is
equipped with the Automatic Climate Control System.
The Automatic Climate Control System, incorporating an A/C
Systems LLC Air Conditioning System, is designed to cool and
heat the airplane cabin to desired temperature settings during
all phases of flight operations. The system may be used during
any phase of the flight (except a right engine failure), offering a
choice of fully automatic or mode override.
SECTION 2 - LIMITATIONS
No Change.
FAA Approved
Issued: March, 2017
P/N 58-590000-0091 3 of 24