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S Turn the cap counter-clockwise a small
distance to release the pressure.
S When the pressure has fully released, turn
the cap fully counter-clockwise.
(9) Check coolant level. Repeat items (5) to (8) until
the system is completely de-aerated and full.
(10) Install the cap to the coolant tank.
(11) Install the engine cowlings. Refer to Section 71-11.
AIRCRAFT
Servicing DA 40 Series
AMM
Page 14
20 Sep 2007 12-10-00 Doc # 6.02.01
Rev. 5
7. Brake System
The brake fluid reservoirs are located on the brake master cylinders on the co-pilot’s side. You get
access in the cockpit below the instrument panel.
WARNING: DO NOT GET BRAKE FLUID ON YOUR SKIN OR IN YOUR MOUTH.
BRAKE FLUID CAN CAUSE DISEASE.
CAUTION: REMOVE SPILLED BRAKE FLUID IMMEDIATELY. BRAKE FLUID CAN
CAUSE DAMAGE TO PAINT AND OTHER MATERIALS.
A. Fill the Brake System Reservoirs
Detail Steps/Work Items Key Items/References
(1) Clean the top of the brake fluid reservoir and filler
cap.
(2) Remove the filler cap.
(3) Fill the reservoir to the correct level. Use only MIL-H-5606A hydraulic fluid.
12 to 25 mm (0.5 to 1 in.) below the top
of the filler hole.
(4) Install the filler cap.
AIRCRAFT
DA 40 Series
AMM
Servicing
Doc # 6.02.01
Rev. 5 12-10-00 Page 15
20 Sep 2007
8. Tires
The DA 40 has these tires:
% Main tires: (a) 6.00-6; 6PR, 120 mph
% Only in combination with the standard MLG strut or the “thin” MLG strut
% (MÄM 40-123/e)
% (b) 15 x 6.0-6; 6PR,120 mph (OÄM 40-124)
% Only in combination with the “thin” (MÄM 40-123/e) or the “tall” (OÄM 40-283)
% MLG strut.
% Pressure: 2.5 bar (36 psi)
% Nose tire: 5.00 x 5, 6PR, 120 mph, TSO C62; pressure 2.0 bar (29 psi).
A. Examine the Tires and Measure the Pressure
Detail Steps/Work Items Key Items/References
(1) Examine the tires. Look specially for:
S Cuts and friction damage.
S Correct alignment of the slippage markers.
Move the airplane as necessary so that
each part of each tire can be seen.
If the slippage markers do not align,
remove the wheel for shop
maintenance.
(2) Measure the tire pressure. If necessary, inflate
the tires to the correct pressure.
Main tire: 2.5 bar (36 psi).
Nose tire: 2.0 bar (29 psi).
AIRCRAFT
Servicing DA 40 Series
AMM
Page 16
20 Sep 2007 12-10-00 Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Servicing
Doc # 6.02.01
Rev. 5 12-20-00 Page 1
20 Sep 2007
Section 12-20
Scheduled Servicing
1. General
This Section gives lubrication data. It tells you where components are located. It gives a list of
approved lubricants. It also gives the components which MUST NOT be lubricated.
Most systems and components have maintenance-free bearings. These can be sealed ball/roller
bearings or Teflon bushes. These bearings MUST NOT be lubricated. Table 1 shows the bearings
which MUST NOT be lubricated.
Table 1 - Items which MUST NOT be Lubricated
Rudder pedal sled. DO NOT LUBRICATE
Flap rod-end bearings. DO NOT LUBRICATE
Aileron rod-end bearings. DO NOT LUBRICATE
Elevator rod-end bearings. DO NOT LUBRICATE
Throttle control cable, propeller control cable
and mixture control cable (Lycoming version
only). (See Note 7).
DO NOT LUBRICATE
Elastomeric spring. (See Note 8). DO NOT LUBRICATE
AIRCRAFT
Servicing DA 40 Series
AMM
Page 2
20 Sep 2007 12-20-00 Doc # 6.02.01
Rev. 5
2. Lubrication Schedule
Table 2 shows the lubrication schedule. Clean each lubrication point before lubrication.
See Figures 1 and 2 for the location of lubrication points listed on the left side of the table. The center
columns show the type of lubricant. The right column shows the lubrication interval.
Table 2 - Lubrication Schedule
Location Type of Lubricant Interval
No. See Figures 1 and 2 1 2 3 4 5 6 (Hours)
see Notes (1), (2)
(1) Brake pedal pivot 200
(2) Rudder cable S-tubes 200
(3) Flap actuator extension rod 200
(4) Upper rudder pivot bearing 200
(5) Nose wheel bearing (See Notes 3, 5 and 6) 200
(6) Wing main bolts 1000
(7) Battery terminals 1000
(8) B-bolts 1000
(9) B-bolt spherical bearings 1000
(10) A-bolts 1000
(11) A-bolt spherical bearings 1000
(12) Brake pedal pivot shaft interior 1000
(13) Flap actuator universal pivot block 1000
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