AIRCRAFT
Airworthiness
Limitations
DA 40 Series
AMM
Page 2
20 Sep 2007 04-00-00 Doc # 6.02.01
Rev. 5
Intentionally left blank
DA 40 Series
AMM
Airworthiness
Limitations
Doc # 6.02.01
Rev. 5 04-00-00 Page 3
20 Sep 2007
1. Airworthiness Limitations
This Section is approved and shows the mandatory limitations established by the airframe
manufacturer.
Personnel must obey the limitations given in this Section.
A. Certification Maintenance Requirements
(1) Component and System Checks
The component and system checks under this paragraph are also included in Section 05-10.
The following table lists airplane components and systems which require monitoring through
scheduled maintenance.
Where an interval is given in both flight time and calendar years, the limit which is reached first
must be applied.
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.
ATA
Ch.
Component Maintenance Requirement Interval Kind
of
Ope.
hrs. yrs.
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.
1000 NVFR
% 34 Pitot-static system. Clean system, perform
leakage test (refer to Section
34-10).
1000 2 NVFR
51 Bonding system and static
discharging system.
Resistance measurements
(refer to Section 51-80).
1000 NVFR
79 Oil radiator. Proof-test at 250 psi (or
replace).
2000 12 IFR
AIRCRAFT
Airworthiness
Limitations
DA 40 Series
AMM
Page 4
20 Sep 2007 04-00-00 Doc # 6.02.01
Rev. 5
(2) Structure Checks
The DA 40 has been designed and tested under a 'damage tolerant structure' philosophy.
Therefore the structural inspections given in Chapter 05 cover all required structure checks.
There is no structural life limit.
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