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Figure 1.1
Doc # DA202-C1
April 16, 2009
Page S1 - 2
Revision 24
DOT Approved
Figure 1.2
2. OPERATING LIMITATIONS
2.1. Voltage supplied to the EPU receptacle should be 12-14 volts nominal.
2.15 . PLACARDS
1. On the lower left side of the instrument panel above the switches.
2. On the right side of the aircraft above the EPU receptacle.
EXTERNAL
POWER
14 VOLTS
3. On the EPU/FUSE mounting bracket in the Relay box. (Aircraft S/N C001 through C0148 and C0150 only)
HOUR METER
Doc # DA202-C1 April 16, 2009 Page S1 - 4
Revision 24 DOT Approved
3. EMERGENCY PROCEDURES
3.3.4. Fire
A. Engine Fire during Engine-Start-Up on the Ground (EPU power connected).
1.
Fuel Shut-off Valve CLOSED
2.
Cabin Heat CLOSED
3.
Mixture IDLE CUTOFF
4.
Throttle FULL
5.
GEN/BAT Master Switch OFF
6.
Ignition Switch OFF
7.
EPU Switch OFF
8.
Evacuate Airplane immediately
4. NORMAL PROCEDURES
4.1. General
The following general procedure should be used to supply External Power to the aircraft for purposes other than engine starting.
Power ON
1.
Connect external power source to the EPU light ON
EPU receptacle.
2.
EPU switch ON
3.
GEN/BAT Master Switch (Battery only) ON if desired for charging
4.
Avionics Master Switch ON if desired
CAUTION
IF THE BATTERY HAS BEEN DISCHARGED, IT IS ADVISABLE TO LEAVE THE BATTERY ON CHARGE FOR A PERIOD OF TIME LONG ENOUGH TO CHARGE THE BATTERY. CONSULT MAINTENANCE PERSONNEL IF THE STATE OF CHARGE OF THE BATTERY IS IN QUESTION. DO NOT FLY THE AIRCRAFT WITH THE BATTERY IN A DISCHARGED STATE.
Power OFF
1.
Electrical loads OFF
2.
Avionics Master Switch OFF
3.
GEN/ BAT Master Switch OFF
4.
EPU switch OFF
5.
LIFT EPU receptacle cover, PULL EPU light OFF external power plug.
4.4. Normal Operation Checklist
In addition to those items contained in Section 4, Normal Operating Procedures, Preflight Inspection, check the following items if this supplement is applicable to the aircraft you are operating:
A. In-Cabin Check
Caution Lights (EPU) illuminated if EPU power available
B. Walk Around Check and Visual Inspection
Right Wing (C0001 to C0148, C0150)
Left Side of Fuselage (C0149, C0151 and Above)
EPU Receptacle ( For EPU START) check EPU connector inserted and secure. Adequate power source available.
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