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Do the test at the top of the control stick.
S Maximum play allowed ± 2.5 mm (± 0.1 in.).
(Refer to Section 27-10).
X X X
5. Do a function test of the aileron control system.
(Refer to Section 27-10).
X X X
6. Do a function test of the rudder control system.
(Refer to Section 27-20).
X X X
7. Do a function test of the elevator control system.
(Refer to Section 27-30).
X X X
8. Do an function test of the trim-system. Look
specially for incorrect operation and indication.
(Refer to Section 27-38).
X X X
9. Do a function test of the flap system. (Refer to
Section 27-50). Look specially at the pre-load.
With the flaps set to UP:
S Correct pre-load 3 - 5 daN (6.7 - 11.2 lb)
X X X
10. Lower the airplane off jacks.
(Refer to Section 07-10).
X* X X
11. Do an operational test of the external lights. X X X
12. Do an operational test of the Pitot heat. X X X
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
100 hr items marked X* apply to US registered airplanes only Interval
Inspection Items 50 100 200 1000 Time Initials
Doc # 6.02.01
Rev. 5 05-20-00 Page 45
20 Sep 2007
13. Examine the airplane. Look specially for loose
items and tools. Close all access panels. Install
these items:
S Engine cowlings.
S The instrument panel cover.
S The seat shells.
S The control-stick boots.
S The engine cowlings.
X X X X
WARNING: DO NOT LET PERSONS INTO THE DANGER AREA OF THE
PROPELLER. PROPELLERS CAN CAUSE INJURY OR DEATH.
WARNING: SET THE PARKING BRAKE TO ON. IF YOU DO NOT DO THIS THE
AIRPLANE CAN MOVE. THIS CAN CAUSE INJURY OR DEATH.
14. Put the chocks against the main airplane wheels. X X X X
15. Do the post maintenance engine test.
S For the engine run procedures refer to the
Airplane Flight Manual.
S Record the data (Refer to Paragraph 7,
Engine Ground Test Record).
X X X X
16. Examine the engine for leakage. X X X X
17. Make sure the engine oil filter is tight. (Refer to
Section 79-00 for the Lycoming version or Section
79-01 for the TAE version).
X X X X
18. Do a test flight. Put the engine ground test and
the flight test reports in the Airplane Maintenance
Log.
X X X
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 46
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
5. Maintenance Report
Complete a copy of the Maintenance Report after all of the applicable maintenance tasks in the
Maintenance Checklist have been initialed.
DA 40
Airplane Serial Number: Registration Number:
Check: __________ (50 hr., 100 hr., 200 hr., 1000 hr., Annual)
REMARKS:
The airplane is airworthy with respect to its maintenance condition.
_________________
Place
_________________
Date
_________________
Authorized
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Doc # 6.02.01
Rev. 5 05-20-00 Page 47
20 Sep 2007
6. Check Flight Report
CHECK FLIGHT
(See Maintenance Checklist for Applicability)
DA 40
Page 1 of 3
Registration: Pilot: Airdrome:
Date: Take-Off: Landing:
Functional Check, Flight Behavior
Findings
N/A NO YES
Fuel quantity indicators
Strobe lights (ACL), navigation lights
Warning, caution and status lights
Altimeter(s), QNH adjustment
Radio, radio check
Audio panel, intercom
Navigational instruments
Electrical fuel pump (Lycoming) or fuel transfer pump (TAE)
Starter behavior
Engine starting behavior, cold
Oil pressure indicator
Fuel pressure indicator (Lycoming version only)
Fuel temperature indicator (TAE version only)
Fuel flow indication
Voltmeter
Ammeter, alternator
Essential bus
Manifold pressure indicator (Lycoming) or load indicator (TAE)
RPM indicator
Exhaust gas temperature (EGT) indicators (Lycoming version only)
Cylinder head temperature (CHT) indicators (Lycoming version only)
AIRCRAFT
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 48
20 Sep 2007 05-20-00 Doc # 6.02.01
Rev. 5
CHECK FLIGHT
(See Maintenance Checklist for Applicability)
DA 40
Page 2 of 3
Functional Check, Flight Behavior
Findings
N/A NO YES
Oil temperature indicator
Coolant temperature indicator (TAE version only)
Gearbox temperature indicator (TAE version only)
Instrument lighting
Flood light
Map light, overhead
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钻石40系列AMM 1(41)
