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ACCU-SIM V35B BONANZA
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A2A
SIMULATIONS
91
FOR SIMULATION USE ONLY
FLIGHT INSTRUMENTS
The floating instrument panel contains all flight instru-
ments except the magnetic compass. On this panel are the
airspeed indicator, gyro horizon, altimeter, turn coordina-
tor, directional gyro, and vertical speed indicator, with pro-
visions tor an ADF indicator and a clock. Additional nav-
igation equipment, such as dual omni indicators, can be
mounted in the panel directly below the flight instrument
grouping.
ENGINE INSTRUMENTS
The engine instruments, located on the center panel, include
a fuel flow/manifold pressure indicator, an engine tachom-
eter, a fuel quantity indicator tor each side, and a cluster
which includes an oil pressure indicator, an oil tempera-
ture indicator, a cylinder head temperature indicator, and
an ammeter.
CLUSTER TYPE ENGINE INSTRUMENTS
The cluster type instruments, as shown in the accompa-
nying illustration, are located in the center of the panel
just below the fuel flow/manifold pressure indicator and
tachometer. Included in the square cluster are the cylin-
der head temperature and oil temperature (both calibrated
in degrees centigrade), ammeter, and oil pressure. A fuel
quantity indicator is located on each side of the cluster, the
left indicator tor the left wing fuel and the right indicator
tor the right wing fuel.
MANIFOLD PRESSURE AND FUEL FLOW INDICATOR
The manifold pressure portion of this instrument indi-
cates the pressure in the engine manifold and is calibrated
in inches of mercury. By observing the manifold pressure
indication and adjusting the propeller and throttle con-
trols, the power output of the engine can be adjusted. To
avoid excessive cylinder pressures during cruise opera-
tions, observe the maximum recommended rpm and mani-
fold pressure limits as indicated on the Manifold Pressure vs
RPM graph in the PERFORMANCE Section.
The fuel flow portion of the indicator senses fuel pressure
at the fuel distributor and is calibrated to indicate fuel flow
in gallons per hour. The green arc indicates the normal fuel
flow operating range while the red radials indicate the min-
imum and maximum allowable fuel pressures.
The higher end of the green arc includes a sawtooth seg-
ment to indicate the approximate fuel flow required for
takeoff and climb at sea level, 3000, 5000 and 7000 feet.
The pilot should use performance charts for the exact fuel
flow requirements.
The lower end of the green arc includes a sawtooth seg-
ment labeled”% CRUISE POWER” which indicates the
approximate fuel flows for powers ranging from 45% to
75% of max continuous power. The lower fuel flow of each
sawtooth corresponds to the cruise - lean fuel flow while
the higher fuel flow of each sawtooth corresponds to the
best power fuel flow. When power is set in accordance with
the cruise power setting tables in the PERFORMANCE sec-
tion, these sawtooth markings provide approximate percent
power information.
The fuel flow portion of the indicator is controlled electri-
cally and indicates fuel flow in gallons per hour. A turbine
meter installed in the fuel line rotates in proportion to the
fuel flow. The speed of rotation is converted into an electri-
cal signal which is then interpreted by the fuel flow indi-
cator. The green arc indicates the normal operating range
while the red radial indicates the maximum allowable fuel
flow.
Fuel flow values at the higher end
of the green arc are labeled “TAKE-
OFF AND CLIMB” and indicate the
approximate fuel flow required
for takeoff and climb at sea level,
3000, 5000 and 7000 feet. The pilot
should use these markings as a guide
only and refer to the tables in the
PERFORMANCE section for the exact
fuel flow requirements.
AVIONICS PANEL
Tuning and selecting equipment for
the radios, adjacent to the engine
instrument grouping, is mounted in
block form with switching on the left
edge of the block and radio heads and
tuning on the right.
SWITCHES
The magneto/start switch and
switches for the battery, alterna-
tor, pitot heat, propeller deicer, and
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