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B. Replacement Requirements
The replacement requirements under this paragraph are also included in Section 05-10.
The following table lists life limited airplane components which must be replaced at a specific time.
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.
% Note: The life limited airplane components listed in the following table and further
% recommended intervals are stated in Chapter 5 of this Airplane Maintenance
% Manual.
ATA
Ch.
Component Replacement Time Kind
of
Ope.
hrs. yrs.
24 Emergency battery (Lycoming version only).
Replace all cells at the same time. All cells must have
the same expiration date.
2 years, or upon
reaching the date
marked on each cell,
or after use.
IFR
24 ECU backup battery (TAE version only). 2 VFR
27 Rudder cables, 3.2 mm (1/8 in.) diameter. 3000 5 VFR
28 Fuel hoses behind the firewall. On condition. VFR
2000 12 NVFR
73 Fuel hoses in engine compartment (Lycoming version
only).
On condition. VFR
2000 12 NVFR
73 Fuel hoses in engine compartment (TAE version only). 5 VFR
75 Coolant hoses (TAE version only). 5 VFR
79 Oil hoses (Lycoming version only). On condition. VFR
2000 12 NVFR
% 79 Oil hoses (TAE version only). 5 VFR
DA 40 Series
AMM
Airworthiness
Limitations
Doc # 6.02.01
Rev. 5 04-00-00 Page 5
20 Sep 2007
% C. Colour of Airframe
It is mandatory to paint the DA 40 white as described in Chapter 51 of this manual. This will prevent
% the temperature of the structure from becoming too high. Examples of approves shades are:
% ) RAL 9016
% ) Mercedes DB 147
% ) BMW 218
% ) Volvo XG28
% ) Volvo BC76
% ) Saab 5AC6
% ) Alfa Romeo 230
% Before painting the DA 40 in a different shade the manufacturer must be contacted.
%
% Only certain areas which are defined in Chapter 51 of this manual (for example, registration markings,
% placards and warning markings) may have a different color.
D. Repairs
Repairs which are not described in Chapter 51 of this manual may only be carried out in
accordance with a repair scheme which has been approved by the manufacturer or the competent
National Airworthiness Authority.
AIRCRAFT
Airworthiness
Limitations
DA 40 Series
AMM
Page 6
20 Sep 2007 04-00-00 Doc # 6.02.01
Rev. 5
2. Continued Airworthiness
Regular inspections of the airplane including replacement and overhaul of certain components are
required to ensure Continued Airworthiness of the DA 40.
A. Airplanes registered in the USA
The time limits given in Chapter 04 should be applied to ensure Continued Airworthiness of the DA
40 unless an alternate inspection program is agreed on with the FAA.
The manufacturer recommends that you apply the time limits and maintenance checklists given in
Chapter 05. Annual and 100 hour inspections of the DA 40 airplane must include all inspection
items as required by FAR 43, Appendix D in scope and detail of an annual/100 hour inspection.
B. Airplanes registered in other countries
The time limits given in Chapter 04 should be applied to ensure Continued Airworthiness of the DA
40 unless an alternate inspection program is agreed on with the competent National Airworthiness
Authority.
The manufacturer recommends that you apply the time limits and maintenance checklists given in
Chapter 05. National maintenance requirements must be complied with.
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Doc # 6.02.01
Rev. 5 05-TITLE Page 1
20 Sep 2007
CHAPTER 05
TIME LIMITS AND MAINTENANCE
CHECKS
AIRCRAFT
Time Limits and
Maintenance Checks
DA 40 Series
AMM
Page 2
20 Sep 2007 05-TITLE Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Time Limits and
Maintenance Checks
Doc # 6.02.01
Rev. 5 05-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 05
TIME LIMITS AND MAINTENANCE CHECKS
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Chapter Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
　
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