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ACCU-SIM V35B BONANZA
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A2A
SIMULATIONS
67
FOR SIMULATION USE ONLY
ALTERNATOR-OUT PROCEDURE
An inoperative alternator will place the entire electrical
operation of the airplane except engine ignition on the bat-
tery. An alternator failure will be indicated by illumination
of the warning light, located on the instrument panel below
the flight instruments.
The warning light will not illuminate until the alternator
output is almost zero. A verification of alternator malfunc-
tion would be a discharge shown on the ammeter. There is
no indication of overvoltage except that the warning light
will illuminate as though the alternator is out.
Alternator Warning Light Illuminated:
1 .
Verify alternator out with ammeter
- will show discharge.
NOTE:
If the ammeter does not show a discharge, a
malfunction in the warning light system is indicated, and the
alternator switch should be left ON.
2 .
If ammeter shows a discharge, Alternator Switch
OFF MOMENTARILY, THEN ON (this resets the
overvoltage relay). If the warning light does not
illuminate, continue to use the alternator.
3 .
If the warning light illuminates,
Alternator Switch - OFF
4 .
Nonessential Electrical Equipment -
OFF to conserve battery power
LANDING GEAR MANUAL EXTENSION
Manual extension of the landing gear can be facilitated by
first reducing airspeed. Then proceed as follows:
1 .
LOG GR MOTOR Circuit Breaker (Right
Subpanel) - OFF (pull out)
2 .
Landing Gear Switch Handle - DOWN position
3 .
Handcrank Handle Cover (at rear
of front seats) - REMOVE
4 .
Handcrank - ENGAGE and TURN COUNTERCLOCKWISE
AS FAR AS POSSIBLE (approximately 50 turns)
CAUTION:
The manual extension system is designed to lower
the landing gear only. DO NOT ATTEMPT TO RETRACT THE GEAR
MANUALLY.
5 .
If electrical system is operative, check landing
gear position lights and warning horn (check
LOG GR RELAY circuit breaker engaged).
6 .
Handcrank - DISENGAGE. Always
keep it stowed when not in use.
WARNING:
Do not operate the landing gear electrically with
the handcrank engaged, as damage to the mechanism could
occur.
After emergency landing gear extension, do not move any
landing gear controls or reset any switches or circuit break-
ers until airplane is on jacks, as failure may have been in the
gear-up circuit and gear might retract.
LANDING GEAR RETRACTION AFTER
PRACTICE MANUAL EXTENSION
After practice manual extension of the landing gear, the
gear can only be retracted electrically, as follows:
1 .
Handcrank - CHECK, STOWED
2 .
Landing Gear Motor Circuit Breaker - IN
3 .
Landing Gear Switch Handle - UP
SPINS
Spins are prohibited. If a spin is entered inadvertently:
Immediately move the control column full forward and
simultaneously apply full rudder opposite to the direction of
the spin; continue to hold this control position until rotation
stops and then neutralize all controls and execute a smooth
pullout. Ailerons should be neutral and throttle in idle posi-
tion at all times during recovery.
EMERGENCY SPEED REDUCTION
In an emergency, the landing gear may be used to create
additional drag. Should disorientation occur under instru-
ment conditions, the lowering of the landing gear will
reduce the tendency for excessive speed buildup. This pro-
cedure would also be appropriate for a non-instrument
rated pilot who unavoidably encounters instrument condi-
tions or in other emergencies such as severe turbulence.
Should the landing gear be used at speeds higher than the
maximum extension speed, a special inspection of the gear
doors in accordance with maintenance manual procedures is
required,with repair as necessary.
Summary of Contents for BONANZA ACCU-SIM V35B
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