Table of Contents
Advertisement
Airplane Flight Manual Supplement
Beechcraft Baron Models
G58, 58A, 58, E55A, E55, D55A, AND D55
The Automatic Climate Control System, incorporating an A/C Systems LLC Air Conditioning System, is
designed to cool and heat the aircraft 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.
No change to this section.
SECTION 3 – EMERGENCY PROCEDURES
ENGINE FIRE
IN FLIGHT
"OFF" on the Automatic Climate Control should be selected.
Climate Control System
ELECTRICAL SMOKE OR FIRE
"OFF" on the Automatic Climate Control should be selected.
Climate Control System
RIGHT ENGINE FAILURE
After securing and feathering the right engine:
The "Air Conditioning Compressor OFF" mode on the Automatic Climate Control should be selected by
pressing the
button until the adjacent indicator light goes out.
Air Conditioning Compressor Mode
This procedure ensures absolute maximum power is available for single engine operation.
LEFT ENGINE FAILURE
No change to this procedure.
SUSPECTED REFRIGERANT LEAK IN CABIN
The "Air Conditioning Compressor OFF" mode on the Automatic Climate Control should be selected by
pressing the
button until the adjacent indicator light goes out.
Air Conditioning Compressor Mode
Cabin Vents.
.
FAA Approved 04/23/2012
SECTION 1 – GENERAL
SECTION 2 – LIMITATIONS
.
.
.
.
.
.
.
NOTE
.
.
.
.
Document No. FTA-010-6
.
.
.
.
.
.
.
.
.
.
.
.
.
.
.
Revision IR
Page 3
.
.
OFF
.
.
OFF
.
.
OFF
.
.
OFF
.
.
OPEN
Hide quick links:
Advertisement
Chapters
Table of Contents
