Page 3-16
EASA Approved
Initial issue
Alternator Failure
Loss of alternator output is detected through a zero or minus values reading on the ammeter and warning lamp
CHARGE
coming on. Electrical power malfunctions are accompanied by an excessive rate of charge or a discharge rate
indicated by ammeter.
a.
THROTTLE
Increase above 3000 rpm
b.
External lights
All OFF
c.
FUEL PUMP
OFF
If no increase in the ammeter reading is noted:
d.
MASTER SWITCH
OFF - ON
If no increase in the ammeter reading is noted:
e.
All unnecessary
electrical equipment
OFF
f.
Voltmeter
Monitor battery voltage
g.
Landing
Perform at nearest airfield
CAUTION
All electrical loads are being supplied by the battery. Turn off all
unnecessary equipment! Disconnect all external equipment from
the instrument panel power outlets!
CAUTION
Be aware, if the
AVIONICS
switch is turned off, the radio
communication is lost!
NOTE
Operating time of battery depends on its condition.
NOTE
Dynon SkyView system has its own backup battery.
Содержание WT9 Dynamic LSA / Club
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Страница 122: ...Page 6 12 EASA Approved Initial issue Fig 6 4 Check of flight weight moment limits Example Metric Units...
Страница 125: ...Initial issue EASA Approved Page 6 15 Fig 6 5 Weights and moments of variable masses chart Metric Units...
Страница 127: ...Initial issue EASA Approved Page 6 17 Fig 6 6 Weights and moments of variable masses chart U S Standard Units...
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Страница 148: ...Page 7 14 Initial issue Fig 7 5 Arrangement screen 1 Fig 7 6 Arrangement screen 2...
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Страница 163: ...Initial issue Page 7 29 Fig 7 18 Arrangement screen 3 Fig 7 19 Arrangement screen 4...
Страница 164: ...Page 7 30 Initial issue Fig 7 20 Arrangement screen 5 Fig 7 21 Arrangement screen 6...
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Страница 173: ...Initial issue Page 7 39 Fig 7 29 Air outlets for cockpit venting Fig 7 30 Windshield demist knob...
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