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Amperage is displayed both analog and digitally. The load being monitored is the electrical current the generator is supplying to the system. When the electrical load is increased by turning on equipment, the ammeter will show an increase. When the load being supplied by the generator drops below approximately 2 amps the VM 1000 display will flash, if installed, the EC100 displays the warning and an audible tone is heard.
7.8. Fuel Quantity
Fuel quantity is displayed on a separate indicator but is controlled by the VM 1000 Data Processing Unit and EC 100 remote display. Display resolution is 1 US gallon. When 5 US gallons remain in the main tank the fuel system display is flashed an audible tone is heard and the EC 100 displays the warning.
Figure 1
8. HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE
Service and maintenance of the VM 1000 / EC 100 system shall be performed according to the Diamond Aircraft Maintenance Manual (Document number DA201-C1).
INTENTIONALLY LEFT BLANK
CHAPTER 9
SUPPLEMENT 7
Auxiliary Fuel System
1.
GENERAL S7-2
2.
OPERATING LIMITATIONS S7-2
3.
EMERGENCY PROCEDURES S7-2
4.
NORMAL PROCEDURES S7-3
5.
PERFORMANCE S7-4
6.
WEIGHT AND BALANCE S7-4
7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS S7-5
8.
HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE S7-6
1. GENERAL
This supplement addresses the optional installation of an auxiliary fuel tank system (Mod No 60). The optional auxiliary fuel system installation provides extended range operation by increasing the total fuel capacity of the DA20-C1 by 5 US gallons.
Only portions of the flight manual affected by the installation are included in this supplement.
2. OPERATING LIMITATIONS
NOTE
Refer to all of the Operating Limitations with the following inserted into the appropriate place.
1. Initiate fuel transfer only when main tank is less than 3/4 full.
2.4. Placards
1. On the lower right corner of 3. Above the auxiliary fuel filter
the instrument panel. cap on the R/H side of the fuselage.
2. Above the auxiliary fuel filter 5. On the underside of the
cap on the R/H side of the fuselage, to the right, just
fuselage. forward of the wing trailing
edge.
3. EMERGENCY PROCEDURES
Emergency procedures are not affected by the Auxiliary Fuel Tank system.
4. NORMAL PROCEDURES
NOTE
Refer to all of the Normal Operating Procedures with the following inserted into the appropriate places.
CAUTION
THE AIRCRAFT MUST BE GROUNDED PRIOR TO AND DURING FUELING. USE THE GROUND STUD, LOCATED UNDER THE TRAILING EDGE OF THE LEFT WING.
NOTE
It is recommended to fill the main tank first and to full capacity before filling the auxiliary tank.
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