Operation Manual E4.01 - Austro Engine

1 Operation Manual Issue date: Page: 1 Revision no: 20 Operation Manual Issue date: Page: Intro 1 Revision no: 20 Intentionally left blank Operation Manual Issue date: Page: Intro 2 Revision no: 20 Date: Wiener Neustadt, Author: Austro Engine GmbH Rudolf Diesel Stra e 11 A-2700 Wiener Neustadt Document number: Revision: 20 Operation Manual Issue date: Page: Intro 3 Revision no: 20 Intentionally left blank Operation Manual Issue date: Page: 1-1 Revision no: 20 1 Index 1 Index.

2 1-1 2 Identification .. 2-1 Type Designation .. 2-1 Engine Identification .. 2-1 Record of Revision .. 2-2 List of Revision .. 2-3 List of incorporated Temporary Revisions .. 2-6 Design Holder .. 2-7 2-7 List of Abbreviations .. 2-7 3 General Information .. 3-1 Description and Using .. 3-1 Safety .. 3-2 Safety Information .. 3-2 Dimension and Volume .. 3-3 Technical Data Sheet .. 3-4 Engine Performance .. 3-4 High power performance .. 3-5 Fuel consumption .. 3-6 Propeller Setpoint Curve .. 3-6 Engine and Gearbox Data Sheet .. 3-7 Limitation Section .. 3-8 Oil.

3 3-8 Coolant .. 3-10 Fuel .. 3-10 Fuel Grade .. 3-11 Speed .. 3-12 Voltage .. 3-12 Performance .. 3-12 Information Section .. 3-13 Engine Oil .. 3-13 Coolant .. 3-14 Fuel .. 3-14 Operating Envelope .. 3-15 4 Delivery, Storage and Standstill Period .. 4-1 Delivery .. 4-1 Storage up to 6 months .. 4-1 Storage over 6 months .. 4-1 Engine depreservation .. 4-1 Standstill Period .. 4-2 5 Operating Instructions .. 5-1 Engine Start Procedure .. 5-1 Pre-Start Inspection .. 5-1 Engine Start .. 5-2 Warm Up .. 5-2 Before Take-off Check .. 5-3 During Flight 5-3 Engine OFF.

4 5-3 Low Oil Pressure .. 5-3 Operation Manual Issue date: Page: 1-2 Revision no: 20 Restart in 5-3 Restart of Engine by starter .. 5-4 6 Emergency Procedures .. 6-1 Power loss and abnormal Engine behaviour .. 6-1 Low Oil Pressure .. 6-1 High Oil Temperature .. 6-1 High Gearbox Oil Temperature .. 6-1 Low fuel pressure .. 6-2 High Fuel Temperature .. 6-2 High Coolant 6-2 Engine Fire .. 6-2 Electric power supply out of range .. 6-2 Restart of Engine by windmilling .. 6-2 7 System Description .. 7-1 Intake System .. 7-1 Exhaust System .. 7-1 Fuel System .. 7-2 Coolant System.

5 7-4 Standard Coolant System .. 7-4 Coolant System with optional Gearbox Oil Cooler .. 7-5 Lubricating System .. 7-6 Electrical System .. 7-7 EECU Functions .. 7-9 Engine Speed and Power Regulation .. 7-13 Error Handling .. 7-15 Description of ECU Switch Over .. 7-15 Resetting ECU caution in Operation .. 7-16 Caution Handling Table Software VC33_x_05_17 .. 7-17 8 Additional Information .. 8-1 Propeller Self Test (Automatic Run-Up Test) .. 8-1 Operation Manual Issue date: Page: 2-1 Revision no: 20 2 Identification Type Designation TC-Designation: E4 Model: E4 (Sales Name AE300) For detailed information about available configurations refer to latest revision of Austro Engine Service Bulletin MSB E4-002.

6 If not otherwise stated this Manual is applicable to all available configurations. Engine Identification Relevant data for Engine identification including the serial number is stated on an Engine identification plate, which is fixed onto the crankcase beneath the starter. For further questions contact Austro Engine GmbH. Fig. : Engine Identification Operation Manual Issue date: Page: 2-2 Revision no: 20 Record of Revision All revisions of this Manual must be recorded in chapter List of Revisions. All incorporated Temporary revisions must be recorded in chapter List of incorporated Temporary Revisions.

7 The new or amended text is indicated by a vertical black line at the left hand side of the revised page, with the revision number and date appearing at the bottom of the page. Cover pages of Temporary revisions are inserted in front the cover page of this Manual . The other pages of Temporary revisions are inserted adjacent to or in front of the corresponding OM pages. Temporary revisions are used to provide information on systems or equipment until the next permanent revision of the Engine Manual . It is the responsibility of the installer to ensure that this Manual is maintained to a current status.

8 If the address or the ownership of the Engine /aircraft changes, an address card has to be sent to Austro Engines GmbH. Operation Manual Issue date: Page: 2-3 Revision no: 20 List of Revision Re. No. Reason Chapter Page(s) Date of Revision Approval Date of Approval Date Inserted Signature 0 First Release all all 1 Authority remarks updated all all 2 Authority remarks updated 1 2 3 6 7 Cover page2 1,.2 1,3,4,6,7 2,4,6,8,9,11 13 1,2 2,3,5,6,7,9, 12,14,15,1617 3 Type plate updated, details to negative g and low oil pressure added, Add. Info Propeller Self Test added.

9 Worm Up rpm changed. Engine Perform. curve changed. 1 2 3 4 5 7 8 Cover page2 1,2 1,3,4 4,8,9,13 1 2,3 13,14 1 4 Oil temperature changed form 125 to 130 . 2 3 Cover Page2 3,4 8,9 2010-02-03 EASA 5 Design holder updated. Text at propeller and Engine off corrected. 2 3 5 Cover Page2 3,4,5 2 3 2010-05-05 Operation Manual Issue date: Page: 2-4 Revision no: 20 Re. No. Reason Chapter Page(s) Date of Revision Approval Date of Approval Date Inserted Signature 6 TS-1 Qualification and Gearbox oil temp. added. 2 3 5 Cover Page 2 4,5 8,9 2,3 2010-06-24 EASA 7 MDC-E4-126 2 3 Intro.

10 2 4,5 7,8,9 2010-09-07 EASA 8 MDC-E4-196 1 2 3 Intro. 2 1,2 4,5 9,10 2011-01-25 EASA 9 MDC-E4-239 2 3 Intro. 2 4,5 8,9 2011-07-19 DOA *) 10 MDC-E4-249 2 3 Intro. 2 4,5 8-14 2011-10-24 DOA *) 11 MDC-E4-172 1 2 3 7 Intro. 2 1-2 4,5 9-15 3-19 2012-03-08 EASA 12 MDC-E4-281 1 2 7 Intro 2 1-2 4,5 14-23 2012-06-27 DOA *) 13 MDC-E4-219 2 3 Intro 2 4,5 9 2012-09-05 DOA *) 14 MDC-E4-279 2 3 Intro 2 4,5 11 2012-09-24 EASA 15 MDC-E4-288 2 3 Intro 2 4,5 8,9 2013-04-30 EASA 16 MDC-E4-297 2 3 Intro 2 4,5 11,12 2013-05-27 EASA 17 MDC-E4-307 1 2 3 4 Intro 2 1,2 4,5 12,14 1,2 2013-06-04 DOA *) 18 MDC-E4-306 2 3 Intro 2 4,5 8,9,12 10-12-2013 EASA Operation Manual Issue date: Page: 2-5 Revision no: 20 Re.