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5. Engine Cleaning........................................................................................................2
6. Ice and Snow Removal.............................................................................................2
Servicing
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CHAPTER 12-00
GENERAL
1. General
This Chapter gives these servicing tasks which apply to the whole airplane:
− Section 12-10. Replenishing procedures for fluid systems.
− Section 12-20. Lubrication data.
− Section 12-30. Cleaning and snow and ice removal.
The procedures for preventive and corrective maintenance of systems are given in the related
Chapter of this manual. Refer to Chapter 05 for time limits and schedules.
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CHAPTER 12-10
REPLENISHING
1. General
Use the procedures in this Section to replenish the fluid systems on the airplane. Figure 1 shows
the location of the servicing points.
2. Fuel System
A tank in the fuselage holds the fuel for the DA20-C1. The tank can hold 24.5 US gal (93 liters) of
fuel. A fuel tank with a capacity of 20 US gal (76 liters) may be installed in place of the standard
tank as an option. The tank is located below the baggage compartment floor.
The tank filler-neck is located on the left side of the fuselage about 18 in (45 cm) aft of the canopy.
It is about 18 in (45 cm) above the left wing root. The fuel tank drain is located below the tank. The
drain pipe comes through the fuselage bottom skin.
WARNING: DO NOT ALLOW FIRE OR HEAT NEAR FUEL. FUEL BURNS
VIOLENTLY AND CAN CAUSE INJURY TO PERSONS AND DAMAGE
TO THE AIRPLANE
WARNING: DO NOT GET FUEL ON YOUR SKIN. FUEL CAN CAUSE SKIN
DISEASE
WARNING: GROUND THE AIRPLANE AND THE FUEL SUPPLY VEHICLE
BEFORE REFUELING. IF YOU DO NOT GROUND THE AIRPLANE,
STATIC ELECTRICITY CAN CAUSE FIRE DURING REFUELING
WARNING: MAKE SURE THAT A FIRE EXTINGUISHER IS AVAILABLE
WARNING: TURN OFF ALL GROUND EQUIPMENT IN THE REFUELING AREA
WARNING: DO NOT OPERATE ELECTRICAL SWITCHES IN THE AIRPLANE
CAUTION: USE ONLY FUEL TYPES GIVEN IN CHAPTER 2 OF THE FLIGHT
MANUAL
Servicing
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Figure 1 - Replenishing Points
DA20-C1 AMM
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A. Refueling
Detail Steps/Work Items Key Items
(1) Turn the engine off.
(2) Ground the airplane. At the refueling ground connection.
(3) Ground the refueling vehicle.
(4) Remove the fuel filler cap.
(5) Refuel the airplane.
(6) Replace the fuel filler cap. Make sure that the fuel filler cap is locked.
(7) Remove the ground cable from the airplane. At the refueling ground connection.
(8) Remove the ground cable from the refueling
vehicle.
B. Defueling
Detail Steps/Work Items Key Items
(1) Ground the airplane. At the refueling ground connection.
(2) Put a container below the drain valve. Make sure you have enough containers to
hold the fuel.
(3) Open the drain valve. Push the drain pipe up.
(4) When the fuel stops draining, close the drain
valve.
Let the drain pipe move down.
(5) Remove the ground cable from the airplane. At the refueling ground connection.
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3. Engine Oil System
WARNING: ENGINE OPERATION WITH NO OIL (OR VERY LOW OIL LEVEL) WILL
CAUSE ENGINE MALFUNCTION OR FAILURE
The engine installed in the DA20-C1 has a wet-sump oil system. The oil sump can hold 6 US
quarts (5.7 liters). See table 1 for approved oils.
The oil filler point is located aft of the rear right cylinder. A panel in the top cowling gives access to
the filler (Figure 1). The oil filler cap has a dip-stick attached.
Some oil consumption is normal. Measure the oil contents before each flight (or engine ground runup).
If necessary, fill the sump to the correct level.
A. Replenish the Engine Oil System
Detail Steps/Work Items Key Items
(1) Open the access panel in the top cowling.
(2) Release the oil filler cap
(3) Measure the oil contents:
− Clean the oil dip-stick.
− Install the filler cap.
− Remove the filler cap again.
　
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