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(1)  Make sure that the engine is safe: S Set the ignition switch to OFF. S Set the throttle to IDLE. S Set the mixture control to LEAN CUT-OFF 
(2)  Remove the engine cowlings.  Refer to Section 71-12. 
(3)  Disconnect the airplane battery.  Refer to Section 24-31. 
(4)  Disconnect the spark plug cables from the spark plugs. 
(5)  Move the mixture control lever between RICH and LEAN CUT-OFF. S Make sure the lever moves freely with no restrictions. 
(6)  Set the mixture control lever to RICH and hold it in position. S Make sure that the mixture lever at the carburetor hits the stop. If necessary, adjust the Bowden cable outer sheath at the support bracket at the bottom of the engine.  With the mixture lever on the stop at the carburetor, there must be at least 3 mm (0.125 in) clearance (bounce) between the lever in the engine control assembly and the cover plate. 

DA 40 Series AMM

DA 40 F

Detail Steps/Work Items  Key Items/References 
(7)  Set the throttle control lever to LEAN CUT-OFF and hold it in position: S Make sure that the mixture lever at the injector hits the CUT-OFF stop. If necessary, adjust the Bowden cable outer sheath at the engine controls bracket at the carburetor.  With the mixture lever on the LEAN CUT-OFF stop at the injector, there must be at least 3 mm (0.125 in) clearance (bounce) between the lever in the engine control assembly and the cover plate. 
(8)  Move the mixture control lever between RICH and LEAN CUT-OFF: S Make sure that the lever moves freely with no restriction. 
(9)  Do items 6 - 8 again as necessary to get the correct values. 
(10)  Do an inspection of the control connections which you disconnected. If necessary for your airworthiness authority, do a second inspection of the controls. 
(11)  Install the cables to the spark plugs.  Torque to 12.4 to 13.6 Nm (110 - 120 in.lb). 
(12)  Connect the airplane battery.  Refer to Section 24-31. 
(13)  Install the engine cowlings.  Refer to Section 71-12. 
(14)  Do an engine test.  Refer to the DA 40 F Airplane Flight Manual. 

76-02-00
DA 40 Series AMM
DA 40 F

Intentionally left blank
DA 40 F

The title of Section 77-40 is amended to read:
Section 77-40 % Integrated Engine Indication - Lycoming IO-360-M1A Engine
Section 77-42 is added:
Section 77-42 Integrated Engine Indication - Lycoming O-360-A4M Engine
1.
General ....................................................... 1

2.
Description/Operation............................................ 1

 

Trouble-Shooting
1. General ..................................................... 101

Maintenance Practices
1.
General ..................................................... 201

2.
Remove/Install the Indicator Panel................................ 201

3.
Replace an Engine Indicator Gauge Sensor/Transducer............... 202

 

DA 40 Series AMM
DA 40 F

Intentionally left blank
DA 40 F

CHAPTER 77
ENGINE INDICATING

Section 77-00 is amended to read:
Section 77-00 % Engine Indicating - Lycoming Engines
1. General
This Section tells you about the engine indicating system for airplanes with the Lycoming engine
%  installed. The DA 40 and DA 40 F has an integrated engine instrument which gives engine indications
%  in a single display unit. The DA 40 and DA 40 F also has an annunciator panel which has warning lights for low oil pressure and low fuel pressure. The transducers that provide the signals for the warning lights on the annunciator panel are installed in parallel with the fuel pressure and oil pressure transducers of the integrated engine display system. The maintenance practices for the annunciator panel transducers are similar to those of the integrated engine instrument.
　
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