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3. Scheduled Maintenance Time Limits
(Refer to Section 05-20).
The following recommended hourly and calendar time limits apply to the scheduled maintenance
checks which are necessary to maintain the airplane in a good technical condition. Do the scheduled
maintenance at the intervals and within the tolerances shown below:
Scheduled Maintenance
Check (Hourly).
Do At These Times Maximum
Tolerance
% 5 Hour Engine Check
% (TAE Engine only)
At 5 hours since new do a 5 hour engine check of the
TAE engine and re-torque engine mount attachment
% bolts on the firewall.
- 2 hours
+ 1 hour
% 25 Hour Engine Check
% (Lycoming engine only)
At 25 hours since new do a 50 hours engine check of
% the lycoming engine and re-torque engine mount
% attachment bolts on the firewall.
± 10 %
50 Hour Check
% (Lycoming Engine only)
At 50 hours since new and every 50 hour intervals. ± 10 %
100 Hour Check At 100 hours since new and every 100 hour intervals. ± 10 %
200 Hour Check At 200 hours since new and every 200 hour intervals. ± 5 %
1000 Hour Check At 1000 hours since new and every 1000 hour
intervals or 12 years, that which comes first.
± 5 %
2000 Hour Structural Check At 2000 hours since new and every 2000 hour
intervals or 12 years, that which comes first.
± 2.5 %
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 2
20 Sep 2007 05-10-00 Doc # 6.02.01
Rev. 5
The intervals between the inspections must be adhered to within the tolerances shown. These
tolerances must not be added up. For example: if the 100 hour inspection was done at 110 hours, the
next inspection must be done at 200 ±10 hours, not 210 ±10 hours.
If an inspection is carried out earlier than allowed by the specified tolerance, all subsequent inspection
intervals are counted from that inspection. For example: If the 100 hour inspection was done at 83
hours, the next inspection must be done at 183 hours.
If the airplane was flown less than 200 hours
Scheduled Maintenance
Check (Calendar)
Do At These Times Maximum
Tolerance
Annual Inspection (for airplanes
registered in the USA).
At 12 months since new and every 12 month
interval do a 100 Hour Check.
Annual Inspection (for airplanes
registered in other countries).
At 12 months since new and every 12 month
% interval do a 200 Hour Check, if no 200 Hour
% Check was performed during the last 12
% month due to flight time.
30 days
Note: For maintenance of airplanes registered in the USA, do the items marked X and
the items marked X* in the Maintenance Checklist.
For maintenance of airplanes registered in other countries, do only the items
marked X in the Maintenance Checklist.
Note: At this time, the DA 40 with the TAE engine is not type certified in the USA.
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Doc # 6.02.01
Rev. 5 05-10-00 Page 3
20 Sep 2007
4. Component Time Limits
A. Maintenance Requirements
The following table lists airplane components and systems which require overhaul or specific
checks.
Where an interval is given in both flight time and calendar years, the limit which is reached first
must be applied.
% For TAE Engine parts refer to TAE 125-01 ‘Operation and Maintenance Manual’, OM-02-01 in the
% latest approved revision and the TAE Service Documentation (e.g. Service Bulletin, Service
% Instruction, ...).
VFR in the "Kind of Operation" column means that this limit applies to day VFR, night VFR and IFR
operation. NVFR in the "Kind of Operation" column means that this limit applies to night VFR and
IFR operation. IFR in the "Kind of Operation" column means that this limit applies to IFR operation.
% Note:
% In the following table the FADEC (TAE version only) is removed.
% Note:
% In the following lists the components marked with an asterisk (*) are Airworthiness Limitation
% items. The Airworthiness Limitation items are listed in Chapter 4 and Chapter 5 of the AMM.
ATA
Ch.
Component Maintenance Requirement Interval Kind
of
Ope.
hrs. yrs.
22 Autopilot system. Mechanical check (refer to
Section 22-10).
1000 1 VFR
24 Alternator, ALU-8421LS-T
(Lycoming version only).
Overhaul. 2000 VFR
24 Essential Bus.* Check both ends of each wire
connected to the battery relay
for insecure connection. Check
essential bus copper bar
(behind circuit breakers) for
looseness.
　
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