Beechcraft Baron G58 Pilot Operating Handbook page 572

Airplane Flight Manual Supplement
Beechcraft Baron Models
G58, 58A, 58, E55A, E55, D55A, AND D55
BEFORE TAXI
Climate Control System
NORMAL TAKEOFF
Climate Control System
For takeoff with the "Air Conditioning Compressor ON" mode in operation,
increase the Ground Roll distance as published in the POH for the applicable
conditions by 4% and the corresponding Total Distance over a 50ft obstacle by
5%. If this incremental distance is not available, select the "Compressor
OFF" mode during the takeoff portion of the flight by pressing the
until the adjacent indicator light is out. This selection is designed to ensure safe
operation throughout the approved flight envelope – actual performance will vary
depending upon ambient conditions.
SHORT FIELD TAKEOFF
Climate Control System
For takeoff with the "Air Conditioning Compressor ON" mode in operation,
increase the Ground Roll distance as published in the POH for the applicable
conditions by 4% and the corresponding Total Distance over a 50ft obstacle by
5%. If this incremental distance is not available, select the "Compressor
OFF" mode during the takeoff portion of the flight by pressing the
until the adjacent indicator light is out. This selection is designed to ensure safe
operation throughout the approved flight envelope – actual performance will vary
depending upon ambient conditions.
If runway conditions are short, soft, or grass and if pressure altitude,
temperature, or humidity is high, it is recommended that the Automatic Climate
Control System is switched to the "Air Conditioning Compressor OFF" mode
during the takeoff portion of the flight by pressing the
adjacent indicator light goes out.
NORMAL CLIMB (CRUISE)
No change to this procedure.
For climb performance with the "Air Conditioning Compressor ON" mode in
operation, decrease the rate-of-climb as published in the POH for the applicable
conditions by 40 fpm. This selection is designed to ensure safe operation
throughout the approved flight envelope – actual performance will vary
depending upon ambient conditions.
FAA Approved 04/23/2012
SECTION 4 – NORMAL PROCEDURES
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NOTE
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NOTE
NOTE
Document No. FTA-010-6
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. . .
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button until the
NOTE
Revision IR
Page 4
Select Mode as desired
(Refer to Section 7)
Select Mode as desired
(Refer to Section 7)
button
Select Mode as desired
(Refer to Section 7)
button