Beechcraft Baron G58, Руководство по эксплуатации для пилотов

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Airplane Flight Manual Supplement Document No. FTA-010-6
Beechcraft Baron Models
Revision IR
G58, 58A, 58, E55A, E55, D55A, AND D55 Page 6
FAA Approved 04/23/2012
SECTION 5 – PERFORMANCE
The pilot is responsible for computation of Weight & Balance conditions, density altitude, wind conditions,
and runway conditions prior to departure.
The performance degradations shown below are to be applied to the existing charts in the basic POH when
the Automatic Climate Control System is On and the system is in the “Air Conditioning
Compressor ON”
mode. Performance is unchanged when the system is in the “Air Conditioning Compressor OFF” mode.
TAKEOFF WEIGHT
TO ACHIEVE POSITIVE ONE-ENGINE INOPERATIVE CLIMB AT LIFT-OFF
To determine the maximum takeoff weight which will achieve a positive one-engine inoperative rate of climb
at liftoff, with the climate control system in operation and the “Air Conditioning
Compressor ON” mode active,
increase the pressure altitude by 750 feet. For example, if the field pressure altitude is 1,000 feet, use the
maximum takeoff weight that corresponds to a pressure altitude of 1,750 feet.
TAKE-OFF DISTANCE
For takeoff with the climate control system in operation and the “Air Conditioning Compressor ON mode
active, 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 “Air Conditioning
Compressor OFF” mode during the takeoff portion of the flight by pressing
the button until the adjacent indicator light is out.
ACCELERATE – GO DISTANCE
For takeoff with the climate control system in operation and the “Air Conditioning Compressor ON mode
active , increase the Accelerate – Go Distance as published in the POH for the applicable conditions by
increasing the pressure altitude by 750 feet. For example, if the field pressure altitude is 1,000 feet, use the
Accelerate – Go Distance that corresponds to a pressure altitude of 1,750 feet.” If this incremental distance
is not available, select the “Air Conditioning
Compressor OFF” mode during the takeoff portion of the flight
by pressing the button until the adjacent indicator light is out.
CLIMB – TWO ENGINE
CLIMB – BALKED LANDING
For climb performance with the climate control system in operation and the “Air Conditioning Compressor
ON mode active, decrease the rate-of-climb as published in the POH for the applicable conditions by 40
fpm. If absolute maximum climb performance is desired, the “Air Conditioning
Compressor ON” mode
should be switched to the “Air Conditioning Compressor OFF” mode by pressing the button until the
adjacent indicator light goes out.
NOTE
The Climate Control System can display OAT. This display is advisory only and
may differ from other OAT indications displayed in the cockpit.
NOTE
If the Automatic Climate Control System is not operating properly, all or any of
the above factors may change. It is the pilot’s responsibility to monitor fuel burn,
time in flight and time to destination during all flight operations and make
appropriate decisions to maintain a safe flight.
SECTION 6 – WEIGHT & BALANCE/EQUIPMENT LIST
The pilot should reference current weight and balance data in basic POH/AFM and compute proper aircraft
weight and balance information prior to each flight.