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examine the airplane internally, specially
in the area of the external damage.
Make a record of the damage you find
and ask Diamond Aircraft for advice
before you repair or operate the
airplane.
(5) Examine the main landing gear. Look specially in
these areas:
S Wheel fairings.
S Main gear leg attachment points.
Refer to Section 32-10.
(6) Examine the nose landing gear. Look specially in
these areas:
S Wheel fairing.
S Nose gear attachment points.
Refer to Section 32-20.
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Detail Steps/Work Items Key Items
Page 10
20 Sep 2007 05-50-00 Doc # 6.02.01
Rev. 5
(7) Operate the flight controls through their complete
range of movement. Look specially for:
S Stiff or unusual feel during movement.
S Restriction of movement.
S Noisy operation.
Refer Section 27-00.
(8) Examine the metal conduction tubes and
bonding strips in the fuselage and in the wings.
Look specially for:
S Heat damage or discoloration.
S Fusion of bonding joints.
S Burn or scorch marks to the structure around
the conduction tubes.
Use the bonding tester when you are not able to
see the whole length of a tube or bonding strip.
Make a record of any damage you find
and ask Diamond Aircraft for advice
before you repair or operate the airplane
Refer to Section 51-80.
Follow the instructions of the tester
manufacturer. The resistance must be
less than 0.001 ohm.
(9) Do a test of these lighting systems:
S External lights:
S Navigation lights.
S Strobe lights.
S Landing light.
S Taxi light.
S Internal lights:
S Instrument panel lights.
S Instrument flood lights.
S Dome lights.
Refer to Section 33-40.
Refer to Section 33-10.
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Detail Steps/Work Items Key Items
Doc # 6.02.01
Rev. 5 05-50-00 Page 11
20 Sep 2007
(10) Do a test of the Pitot heat system. Refer to Section 34-10.
(11) Do a test of these communications systems:
S Com 1 VHF.
S Com 2 VHF if installed.
S Intercom.
Refer to Section 23-10.
Refer to Section 23-50.
(12) Do a test of these attitude and direction systems:
S Magnetic compass.
S Gyro-Compass system if installed.
S Electric horizon/attitude gyro if installed.
S Turn & slip indicator.
Refer to Section 34-20.
(13) Do a test of these dependent position
determining systems:
S Global positioning system (GPS) if installed.
S VOR if installed.
S Distance measuring equipment (DME) if
installed.
S Transponder and altitude encoder if installed.
S Marker beacon receiver if installed.
% S ADF (if installed).
%
Refer to Section 34-50.
(14) Operate the engine power controls through their
range of movement. Look specially for:
S Stiff or unusual feel during movement.
S Restriction of movement.
S Noisy operation.
Refer to Section 76-10 (Lycoming
version) or 76-01 (TAE version).
(15) Do a visual check of engine bondings and
wirings.
TAE version only.
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Detail Steps/Work Items Key Items
Page 12
20 Sep 2007 05-50-00 Doc # 6.02.01
Rev. 5
(16) Operate the cockpit heating controls through
their range of movement. Look specially for:
S Stiff or unusual feel during movement.
S Restriction of movement.
S Noisy operation.
Refer to Section 21-40.
(17) Operate the parking brake control through its
range of movement. Look specially for:
S Stiff or unusual feel during movement.
S Restriction of movement.
S Noisy operation.
Refer to Section 32-40.
(18) Do an engine run-up. Look specially for
abnormal operation of the following systems:
S Engine indicating systems.
S DC generation.
Refer to Section 71-00 (Lycoming
version) or 71-01 (TAE version).
Refer to Section 31-00.
Refer to Section 24-30 (Lycoming
version) or 24-33 (TAE version).
(19) Do an ECU test. TAE version only. Refer to Section
05-20, Paragraph 7.B.
(20) Do an ECU swap test. TAE version only. Refer to Section
05-20, Paragraph 7.B.
(21) Contact the engine manufacturer. TAE version only.
(22) Do a compass check swing.
AIRCRAFT
DA 40 Series
AMM
Dimensions and Areas
Doc # 6.02.01
Rev. 5 06-TITLE Page 1
20 Sep 2007
CHAPTER 06
DIMENSIONS AND AREAS
AIRCRAFT
　
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