Thielert Aircraft Engines GmbH Tel. +49-(0)37204/ 696-0 Fax +49-(0)37204/ 696-2910 Platenenstr. 14 www.centurion-engines.com D - 09350 Lichtenstein [email protected] Approved Airplane Flight Manual Supplement for the DA 40 D Equipped with TAE 125-02-114 Engine Installation Issue 1-0 SERIAL No. _______________ REGISTER No. _______________ This supplement must be attached to the EASA approved Airplane Flight Manual when the TAE 125-02-114 engine has been installed in accordance with EASA STC 10036328. The information contained in this supplement supersedes or adds to the EASA approved Airplane Flight Manual only as set forth herein. For limitations, procedures, performance and loading information not contained in this supplement, consult the basic EASA approved Airplane Flight Manual. This Airplane Flight Manual Supplement is approved with EASA STC 10036328. TAE-Nr.: 50-0310-50021 This page intentionally left blank AFM Supplement DA 40 D LOG OF REVISIONS Approved Revision Chapter Description Date Endorsed - All Initial Issue 1 Sept. 01, EASA STC 2011 10036328 (cid:1) Note: The parts of the text which changed are marked with a vertical line on the margin of the page. Page iii Issue 1 Revision -, Sept. 2011 AFM Supplement DA 40 D LIST OF EFFECTIVE CHAPTERS Chapter Issue/ Revision Date 1 1/0 Sept., 2011 2 1/0 Sept., 2011 3 1/0 Sept., 2011 4A 1/0 Sept., 2011 4B 1/0 Sept., 2011 5 1/0 Sept., 2011 6 1/0 Sept., 2011 7 1/0 Sept., 2011 8 1/0 Sept., 2011 9 1/0 Sept., 2011 APPROVAL The content of approved chapters is approved by EASA. All other content is approved by TAE under the authority of EASA DOA No. EASA.21J.010 in accordance with Part 21. GENERAL REMARK The content of this AFM supplement is developed on basis of the EASA-approved AFM, DAI Document No. 6.01.05-E. Page iv Issue 1 Revision -, Sept. 2011 AFM Supplement DA 40 D TABLE OF CONTENTS CHAPTER 1..........GENERAL (a non-approved chapter) CHAPTER 2..........OPERATING LIMITATIONS (an approved chapter)) CHAPTER 3..........EMERGENCY PROCEDURES (a non-approved chapter)) CHAPTER 4a........NORMAL OPERATING PROCEDURES (a non-approved chapter) CHAPTER 4b........ABNORMAL OPERATING PROCEDURES (a non-approved chapter)) CHAPTER 5..........PERFORMANCE (a non-approved chapter)) CHAPTER 6..........WEIGHT AND BALANCE / EQUIPMENT LIST (a non-approved chapter)) CHAPTER 7..........DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS (a non-approved chapter)) CHAPTER 8..........AIRPLANE HANDLING, CARE AND MAINTENANCE (a non-approved chapter)) CHAPTER 9..........SUPPLEMENTS Page v Issue 1 Revision -, Sept. 2011 AFM Supplement DA 40 D This page is intentionally left blank Page vi Issue 1 Revision -, Sept. 2011 AFM Supplement DA 40 D CHAPTER 1 GENERAL 1.1 INTRODUCTION This supplement must be attached to the EASA approved Airplane Flight Manual when the TAE 125-02-114 engine has been installed in accordance with EASA STC 10036328. The information contained in this supplement supersedes or adds to the EASA approved Airplane Flight Manual only as set forth herein. For limitations, procedures, performance and loading information not contained in this supplement, consult the basic EASA approved Airplane Flight Manual. 1.2 CERTIFICATION BASIS The certification basis for the TAE 125-02-114 engine installation is CS-23, dated November 14, 2003. 1.5 DEFINITIONS AND ABBREVIATIONS (i) Miscellaneous EASA: European Aviation Safety Agency TAE: Thielert Aircraft Engines 1.8 SOURCE DOCUMENTATION UPDATE AND REVISION OF THE MANUAL (cid:1) WARNING: A safe operation is only assured with an up to date AFM supplement. Information about actual AFM, supplement issues and revisions are published in the TAE Service Bulletin TM TAE 000-0004. (cid:1) Note: The TAE-No of this AFM supplement is published on the cover sheet of this supplement. Page 1-1 Issue 1 Revision -, Sept. 2011 AFM Supplement DA 40 D This page intentionally left blank Page 1-2 Issue 1 Revision -, Sept. 2011 AFM Supplement DA 40 D CHAPTER 2 OPERATING LIMITATIONS 2.4 POWERPLANT LIMITATIONS a) Engine manufacturer:..........Thielert Aircraft Engines GmbH b) Engine designation:........TAE 125-02-114 (Centurion 2.0 S) c) RPM limitations (shown as propeller PRM) Maximum:.................................................................2300 RPM Maximum overspeed:..........................2500 RPM (max 20 sec) d) Engine Power Max. take-off power:................114 kW (155 HP) at 2300 RPM Max. continuous power:...........114 kW (155 HP) at 2300 RPM Max. recommended cruise power:......................................85% e) Oil Pressure Min. oil pressure:.............................................................1.2 bar Min. oil pressure (at Take-off power):.............................2.3 bar Min. oil pressure (in flight):..............................................2.3 bar Max. oil pressure:............................................................6.0 bar Max. oil pressure (cold start < 20 sec.):..........................6.5 bar g) Oil Temperature Min. oil temperature (engine starting temp.):....................-32°C Min. oil temperature (min. operating limit temp.):...............50°C Max. oil temperature:.......................................................140°C h) Coolant Temperature Min. coolant temp. (engine starting temp.):.......................-32°C Min. coolant temp. (min. operating limit temp.):.................60°C Max. coolant temperature:...............................................105°C Page 2-1 Issue 1 Revision -, Sept. 2011 AFM Supplement DA 40 D m) Propeller pitch angle (0.75R):..................................13.5° to 28° n) Oil Specification:..................AERO SHELL OIL DIESEL ULTRA ........................................................SHELL HELIX ULTRA 5W-30 .........................................................SHELL HELIX ULTRA 5W-40 ................................................AERO SHELL OIL DIESEL 10W-40 o) Coolant:................Water/Radiator Protection at a ratio of 50:50 Radiator Protection:...................BASF Glysantin Protect Plus/G48 ..............................................................Mobil Antifreeze Extra/G48 ............................................................ESSO Antifreeze Extra/G48 ....................................Comma Xstream Green - Concentrate/G48 ........................................................................Zerex Glysantin G48 (cid:2) CAUTION: The use of water which does not meet the specifications according to the applicable TAE OM-02-02 may cause engine damage. (cid:2) CAUTION: If the coolant level is too low the reason must be determined and the problem must be corrected by authorized personnel. p) Gearbox Oil:...............................Shell Spirax S6 GXME75W-80 ...............................................................Shell Spirax S4 G 75W-90 ............................................Shell Getriebeöl EP 75W-90 API GL-4 ......................................................Shell Spirax GSX 75W-80 GL-4 (cid:2) CAUTION: Use approved oil with exact designation only! (cid:2) CAUTION: If the gearbox oil level is too low the reason must be determined and the problem must be corrected by authorized personnel. q) Maximum restart altitude:...............................................14000 ft Page 2-2 Issue 1 Revision -, Sept. 2011