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AMM
9. Engine Shut-Down
Detail Steps/Work Items Key Items/References
(1) Set the mixture control to fully RICH. Fully forward.
(2) Set the propeller control to MAX RPM. Fully forward.
(3) Set the throttle lever to IDLE. Fully back. Let the engine idle until the cylinder head temperature decreases.
(4) Set 1000 RPM with the throttle lever.
(5) Move the mixture control to fully LEAN. The engine must stop within 5 seconds.
(6) Set the ALT/BAT switch to OFF.
10.After Engine Shut-Down
Detail Steps/Work Items Key Items/References
(1) Read the engine oil level. Add oil if necessary. Refer to Section12-10.
(2) Look under the bottom cowling for signs of oil leaks and signs of fuel leaks.
(3) Install the Pitot probe cover.
Doc # 6.02.01 Page 249
Rev. 4 09 Jan 2003
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AMM
11.Engine Break-In
You must do this procedure after a new engine has been installed. Refer to Lycoming Service Instruction No. 1427, latest issue.
Detail Steps/Work Items Key Items/References
(1) Do a careful pre-flight inspection. Refer to Airplane Flight Manual.
(2) Do a normal take-off. S Mixture control lever .............. RICH S RPM lever ................. HIGH RPM S Throttle .................... MAX PWR Reduce to 2400 RPM as soon as possible.
CAUTION: CLIMB WITH A SMALL CLIMB ANGLE TO AVOID ENGINE OVER-HEATING.
(3) Climb to an altitude which is suitable for cruise. Stay below 5000 ft.
CAUTION: AVOID LOW MANIFOLD PRESSURE DURING HIGH ENGINE SPEEDS (DO NOT OPERATE BELOW 15 INCHES HG). IF YOU MUST REDUCE ENGINE POWER, FIRST REDUCE THE RPM.
(4) Cruise for 2 hours and 30 minutes. S Cruise at 75 % power during the first hour. S Change power setting a few times between 65 % and 75 % during the second hour. S Cruise with 2400 RPM and full throttle during the last 30 minutes.
CAUTION: DESCEND AT A MODERATE RATE AND LOW CRUISE POWER SETTINGS.
(5) Descend and land. Refer to Airplane Flight Manual.
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% Section 71-01 % Power Plant - TAE 125 Diesel Engine % 1. General
% This Chapter tells you about the power plant with the TAE 125-01 Diesel engine installed in the DA % 40. It tells you about the components that make the power plant. It also tells you how to remove/install % the power plant.
% For data on the engine test after installation refer to the Operator's Manual for the TAE 125-01 engine. % Refer to the DA 40 Airplane Flight Manual for engine start/stop procedures.
% Refer to these Chapters for data about other engine systems:
%) Chapter 72 Refer to the TAE 125-01 Operator's Manual for data on the engine.
%) Chapter 73 Engine fuel and control. Refer to the TAE 125-01 Operator's Manual for data on % the fuel injection system.
%) Chapter 76 Engine controls.
%) Chapter 77 Engine indicating.
%) Chapter 78 Exhaust system.
%) Chapter 79 Oil system components installed in the airframe. Refer to the TAE 125-01 % Operator's Manual for data on the engine oil system.
%) Chapter 80 Starter system control and installation. Refer to the TAE 125-01 Operator's % Manual for data on the starter.
% Note: Equipment which is certified for installation in the DA 40 is listed in Section 6.5 of % the Airplane Flight Manual. Such equipment may be installed in accordance with % the Airplane Maintenance Manual.
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