Thielert Aircraft Engines GmbH Tel. +49 37204 696-0 Fax +49 37204 696-2912 Platanenstraße 14 www.centurion-engines.com D - 09350 Lichtenstein [email protected] Supplement Airplane Maintenance Manual Apex Aircraft n ROBIN DR400/135CDI e e CENTURIObN 2.. 0 R s P R a h A P Doc. No. : AMME-60-02A y . t C E n Issuei 1 - Revision 5 o ibil to t C ati s ■ CdA UTIONc: m n a This Supplement to thoe Airprlaene Mntaintenoarnce Manual must be read completely beforse pmaineternanceo actionnf, as it contains important e f c i ssafety inform ation. R n e er a s h a tr e ■ CrAtUTION: u The organizations aPlnd stafff who carry out these maintenance actions must be approvedr by the authority, with the exception of o thfe “Pre-flight check” (cid:1) Note: The supplement to the airplane maintenance manual is to be included at every DR400/135CDI / CENTURION 2.0 installation (cid:1) Note: Please report any service difficulties to the Technical Support Centre at Thielert AircraftEngines GmbH. See above for contact information. Supplement Airplane Maintenance Manual DR400/135CDI / CENTURION 2.0 AMM-60-02 n e e b . s R P R a h A P E A y . t C E n ibili to t C atio s d c m n a oThis pagee intenttionally brlank r n o sp er o nf e f c i s R n e er a s h a r t t e r u l P f r o f Chapter: AMM-60-00 Issue no.: 1 Issue Date: November 16, 2007 Page: 2 Revision no. : 5 Content: 6 Revision date: May, 2011 Supplement Airplane Maintenance Manual DR400/135CDI / CENTURION 2.0 AMM-60-02 Table of contents DR400 AMM (Doc. 1001606GB) Corresponding section 0.1 List of revisions.......................................AMM-60-00 0.2 List of applicable chapters......................AMM-60-00 1 Introduction ..........................................AMM-60-01 4 Airworthiness .......................................AMM-60-04.....................................2 5 Time Limits / Maintenance Checks.....AMM-60-0 5.....................................2 n e 6 Dimensions and Areas.........................AMMe-60-06.....................................1 b . 12 Servicing...............................................sA MM-60-1R2........ .............................3 P R a 21 Environmental Systems.................h......AMMA-60-21...P................................13 E A y . 24 Electrical Power.......................t.............ACMM-60-E24.........n..........................12 i o 28 Fuel...................................i...b.i.l........t...o.. ...AMtM -6C0-28a..t.i..................................9 s d c m 31 Indicating / Recording nSystems..........AaMM-60-31...................................10 o e t r r n o 37 Vacuum...............s...p..........e..r............o.......AMnMf-60-37...................................10 e f c i 61 Propeller........R............n...s...........e. ...........e..rA MM-60-61.....................................5 a s h 71 Power Plant.......................a....................AMM-60-71.....................................5 r t t e r u 73 Engine Fuel SystemsP.l...........f...............AMM-60-73.....................................9 r 74 Ignition..............................o....................AMM-60-74.....................................5 f 75 Liquid cooling.......................................AMM-60-75 77 Engine Indicating..................................AMM-60-77 78 Exhaust.................................................AMM-60-78.....................................5 79 Oil ..........................................................AMM-60-79.....................................5 80 Starting..................................................AMM-60-80.....................................5 91 Charts & Wiring Diagrams...................AMM-60-91...................................12 Chapter: AMM-60-00 Issue no.: 1 Issue date: November 16, 2007 Revision no.: 5 Page: 3 Revision date: May, 2011 Content: 6 Supplement Airplane Maintenance Manual DR400/135CDI / CENTURION 2.0 AMM-60-02 0.1 List of revisions Document No. Issue/Revision Date Approved by AMM-60-00 1/0 November 16, 2007 R. van den Bosch AMM-60-01 1/0 November 16, 2007 R. van den Bosch AMM-60-04 1/0 November 16, 2007 R. van den Bosch AMM-60-05 1/0 November 16, 2007 R. van den Bosch AMM-60-06 1/0 November 16, 2007 R. van den Bosch AMM-60-12 1/0 November 16, 2007 R. van den Bosch AMM-60-21 1/0 November 16, 2007 R. van den Bosch AMM-60-24 1/0 November 16, 2007 R. van den Bosch AMM-60-28 1/0 November 16, 2007 R. van den Bosch AMM-60-31 1/0 November 16, 2007 R. van den Bosch AMM-60-37 1/0 November 16, 2n007 R. van den Bosch AMM-60-61 1/0 November 16,e 2007 R. van den Bosch e AMM-60-71 1/0 Novemberb 16, 200. 7 R. van den Bosch AMM-60-73 1/0 Novemsb er 16, 20R07 R. van den Bosch P R AMM-60-74 1/0 Noveamber 16, 2007 R. van den Bosch h A P AMM-60-75 1/0 November 16, 2007 R. van den Bosch E A y . AMM-60-77 1/0 tNovembCer 16, 2E007 R. vnan den Bosch i o AMM-60-78 1/0 bilNovoe mber 16C, 2007tiR. van den Bosch AMM-60-79 1/0 i Notvembert 16, 2007a R. van den Bosch AMM-60-80 1/0n s dN ovembaecr 16, 20m07 R. van den Bosch AMM-60-91 1o/0 reNovenmtber 16o,r 2007 R. van den Bosch AMM-60-00 sp1/1 er Noovembern f22, 2007 R. van den Bosch AMM-60-05 e 1/1 f Ncovembier 22, 2007 R. van den Bosch s AMM-60-00 R 1n/2 e Maeyr 27, 2008 R. van den Bosch AMM-60-05 a1/2 as Mhay 27, 2008 R. van den Bosch r t AMM-60-12 t 1/2 e rMay 27, 2008 R. van den Bosch u l AMM-60-21 1/P2 f May 27, 2008 R. van den Bosch AMM-60-71 1/2 or May 27, 2008 R. van den Bosch AMM-60-75 1/2 f May 27, 2008 R. van den Bosch AMM-60-00 1/3 July 10, 2008 R. van den Bosch AMM-60-05 1/3 July 10, 2008 R. van den Bosch AMM-60-71 1/3 July 10, 2008 R. van den Bosch AMM-60-00 1/4 October 18, 2010 R. van den Bosch AMM-60-21 1/4 October 18, 2010 R. van den Bosch AMM-60-75 1/4 October 18, 2010 R. van den Bosch AMM-60-79 1/4 October 18, 2010 R. van den Bosch AMM-60-00 1/5 May, 2011 R. van den Bosch AMM-60-01 1/5 May, 2011 R. van den Bosch AMM-60-05 1/5 May, 2011 R. van den Bosch AMM-60-06 1/5 May, 2011 R. van den Bosch AMM-60-71 1/5 May, 2011 R. van den Bosch AMM-60-75 1/5 May, 2011 R. van den Bosch Chapter: AMM-60-00 Issue no.: 1 Issue Date: November 16, 2007 Page: 4 Revision no. : 5 Content: 6 Revision date: May, 2011 n e e b . R s P R a h A P E A y . t C E n i o bil o C ti i t t a s d c m n a o e t r r n o sp er o nf e f c i s R n e er a s h a r t t e r u l P f r o f Supplement Airplane Maintenance Manual DR400/135CDI / CENTURION 2.0 AMM-60-02 n e e b . s R P R a h A P E A y . t C E n ibili to t C atio Thiss page di ntentionaclly blanmk n a o e t r r n o sp er o nf e f c i s R n e er a s h a r t t e r u l P f r o f Chapter: AMM-60-00 Issue no.: 1 Issue Date: November 16, 2007 Page: 6 Revision no. : 5 Content: 6 Revision date: May, 2011 Supplement Airplane Maintenance Manual DR400/135CDI / CENTURION 2.0 AMM-60-02 1 Introduction This operating and maintenance manual contains basic information related to the proper operation of the engine in various situations and under different conditions. It also contains instructions for maintenance. The information and descriptions of components and systems in this manual were correct at the time of publication. Any amendments released through the update information service must also be taken into account. Please contact Thielert Aircraft Engines GmbH if you have any questions. We would be glad to assist you further. 1.1 Accompanying applicable documents (cid:127) Apex Aircraft, DR400 Maintenance Manual (Doc no.1001606GB) (cid:127) Installation Manual IM 02-02 for CENTURION 2.0 (cid:127) Installation Manual IM 02-02 for CENTURION 2.0 in DR400/140B (cid:127) Repair Manual RM-02-02 for CENTURION 2.0 (cid:127) Operation and Maintenance Manual OM 02-02 for CENTURION 2.0 (cid:127) Operation and Installation Manual E-124 for Propeller MTV-6-A/187-129 (cid:127) Installation Manual IM-TAE-CED-125 and Operation Manual OM-TAE- CED-125 (cid:127) Constant Speed Unit Manual CSU CENTURION 2.0 (cid:127) Component Repair Manual CRM-02-02 1.2 Identification of parts of TAE 125 installation Engine identification Refer to OM-02-02. Chapter: AMM-60-01 Issue no.: 1 Issue date: November 16, 2007 Revision no.: 5 Page: 1 Revision date: May, 2011 Content: 6 Supplement Airplane Maintenance Manual DR400/135CDI / CENTURION 2.0 AMM-60-02 Engine Mount identification The Engine Mount of the CENTURION 2.0 is indicated by a part number and a serial number as shown in the following picture. Figure 01-1b Identification of Engine Mount Chapter: AMM-60-01 Issue no.: 1 Issue Date: November 16, 2007 Page: 2 Revision no. : 5 Content: 6 Revision date: May, 2011 Supplement Airplane Maintenance Manual DR400/135CDI / CENTURION 2.0 AMM-60-02 CED identification The CED is identified by a label. An example of the identification label of a CED is shown below. Figure 01-1c Identification Label CED-125 Propeller identification The serial number of the propeller MTV-6-A/187-129 consists of five digits and is provided at the back side of the propeller flange and on a label at the front side of one propeller blade. 1.3 Copyright © These technical data and the information contained therein are the property of Thielert Aircraft Engines GmbH and may not be reproduced either in full or in part, or passed on to a third party without written consent from Thielert Aircraft Engines GmbH. This text must be included in any full or partial reproduction of this documentation. Copyright © Thielert Aircraft Engines GmbH Chapter: AMM-60-01 Issue no.: 1 Issue date: November 16, 2007 Revision no.: 5 Page: 3 Revision date: May, 2011 Content: 6 Supplement Airplane Maintenance Manual DR400/135CDI / CENTURION 2.0 AMM-60-02 1.4 Conventions in this manual The following symbols and warning signs are used in the manual. They must be heeded strictly to prevent injury and material damage, to avoid impairment of the operating safety of the aircraft and to rule out any damage to the aircraft as a consequence of improper handling. ▲ WARNING: Disregarding these safety rules can lead to injury or even death. ■ CAUTION: Disregarding these special instructions and safety measures can cause damage to the engine or to the other components. (cid:1) Note: Additional note or instructions for better understanding of an instruction. The indications "right", "left", "front" and "rear" are always relative to the flight direction. The following symbol is used: ► Example of flight direction right: 1.5 Validity of this manual This manual applies only to the engine having the following serial number:_____________________________________ installed in: DR400/135CDI serial number:_____________________________________ Updates and modifications must be taken into account. 1.6 Abbreviations The following abbreviations are used in this manual: (cid:127) FADEC Full Authority Digital Engine Control (cid:127) CED Compact Engine Display (cid:127) CSU Constant Speed Unit Chapter: AMM-60-01 Issue no.: 1 Issue Date: November 16, 2007 Page: 4 Revision no. : 5 Content: 6 Revision date: May, 2011