钻石40飞机维护手册 DA 40 SERIES AMM 1(31)

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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.  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 

Doc # 6.02.01 Page 3
Rev. 4 09 Jan 2003

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Limitations
AMM

(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.
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.
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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 

Page 4 Doc # 6.02.01 09 Jan 2003 Rev. 4
04-00-00
AMM
Limitations
C. Paint
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. 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.
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.
　
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