Preview only show first 10 pages with watermark. For full document please download

Amm-tr-oam-40-363.

   EMBED


Share

Transcript

DA 40 NG AMM AIRCRAFT Temporary Revision Battery Heating System TEMPORARY REVISION AMM-TR-OÄM 40-363 Battery Heating System This Temporary Revision AMM-TR-OÄM 40-363 is approved in conjunction with the Optional Design Change Advisory OÄM 40-363 and is valid in conjunction with the Airplane Maintenance Manual (AMM) until this Temporary Revision has been incorporated into the AMM. The limitations and information contained herein either supplement or, in the case of conflict, override those in the AMM. The technical information contained in this document has been approved under the authority of DOA No. EASA.21J052. Doc. No. 6.02.15 Section Affected Pages 24-31-00 1a, 1aa, 3a, 3aa, 201a, 202a 92-00-00 1c, 1cc Instruction ) Print this document double-sided on yellow paper (odd pages and "a" pages on front sides, even pages and "aa" pages on reverse sides). ) Insert this cover page as the first page of the AMM. ) Insert the other pages of this Temporary Revision in front of the corresponding AMM pages. Doc # 6.02.15 AMM-TR-OÄM 40-363 COVER Page 1 06 Jun 2013 Temporary Revision DA 40 NG AMM Battery Heating System AIRCRAFT Intentionally left blank Page 2 06 Jun 2013 COVER Doc # 6.02.15 AMM-TR-OÄM 40-363 DA 40 NG AMM AIRCRAFT Temporary Revision Battery Heating System AFFECTED CHAPTERS: CHAPTER 24 ELECTRICAL POWER Section 24-31 Battery System 2. Main Battery Description and Operation The Paragraph is added: % If OÄM 40-363 is installed, eight heater foils are attached to the main battery. The heater foils can be % powered by an external 230 V / 50 Hz power supply via a connector located in the lower aft baggage % compartment. Doc # 6.02.15 AMM-TR-OÄM 40-363 24-31-00 Page 1a 06 Jun 2013 Temporary Revision DA 40 NG AMM Battery Heating System AIRCRAFT Intentionally left blank Page 1aa 06 Jun 2013 24-31-00 Doc # 6.02.15 AMM-TR-OÄM 40-363 DA 40 NG AMM AIRCRAFT Temporary Revision Battery Heating System 3. ECU Backup Battery Description and Operation The Paragraph is added: % If OÄM 40-363 is installed, three heater foils are attached to the ECU backup battery. The heater foils % can be powered by an external 230 V / 50 Hz power supply via a connector located in the lower aft % baggage compartment. Doc # 6.02.15 AMM-TR-OÄM 40-363 24-31-00 Page 3a 06 Jun 2013 Temporary Revision DA 40 NG AMM Battery Heating System AIRCRAFT Intentionally left blank Page 3aa 06 Jun 2013 24-31-00 Doc # 6.02.15 AMM-TR-OÄM 40-363 Temporary Revision Battery Heating System DA 40 NG AMM AIRCRAFT Maintenance Practices 3. Remove/Install the Battery A. Remove the Battery from the Airplane The following item is added: Detail Steps/Work Items % % (4A) If OÄM 40-363 (battery heating system) is Key Items/References At the inline connector. installed disconnect the battery heaters. Doc # 6.02.15 AMM-TR-OÄM 40-363 24-31-00 Page 201a 06 Jun 2013 Temporary Revision Battery Heating System DA 40 NG AMM AIRCRAFT B. Install the Battery in the Airplane The following item is added: Detail Steps/Work Items % % (4A) If OÄM 40-363 (battery heating system) is Key Items/References At the inline connector. installed, connect the battery heaters. Page 202a 06 Jun 2013 24-31-00 Doc # 6.02.15 AMM-TR-OÄM 40-363 DA 40 NG AMM AIRCRAFT Temporary Revision Battery Heating System CHAPTER 92 WIRING DIAGRAMS 1. General The following item is added to the table: Title % Schematic, Battery Heaters Doc # 6.02.15 AMM-TR-OÄM 40-363 Drawing No. Rev. No. of No. Sheets D44-9221-40-01 92-00-00 - 1 Page 1c 06 Jun 2013 Temporary Revision DA 40 NG AMM Battery Heating System AIRCRAFT Intentionally left blank Page 1cc 06 Jun 2013 92-00-00 Doc # 6.02.15 AMM-TR-OÄM 40-363 ALL RIGHTS RESERVED FOR THIS DOCUMENT WHICH MAY NOT BE REPRODUCED OR DISCLOSED TO THIRD PARTIES WITHOUT THE PRIOR WRITTEN CONSENT OF DIAMOND AIRCRAFT INDUSTRIES A B C D E F Confidential 8 8 7 7 6 2 DECIMAL 1DECIMAL DECIMAL ANGLE RAD u0,25 u0,5 u1 u1° u0,5 DIMENSION TOLERANCES FINISH IN MICROMETER 3.2 UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN MM A3 FORMAT METRI C 5A FIRST ANGLE PROJECTION DIMENSIONS BATT. HEATERS 230V AC 6 - NO - SOLID EDGE V18 5 D44-9221-40-01.dft FILENAME SOFTWARE: THIS DRAWING WAS PRODUCED USING INTERCHANGEABLE PART N ON E CLASSIFICATION: DP-S-17-00001 DEPARTMENT 7 8 9 10 11 12 13 14 15 16 #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG 4 APPROVED: SYSTEM: TL N/A N/A N/A STRESS: MANUF.: N/A Industries GmbH QA: CHECKED: DRAWN 6 #20 AWG Aircraft 5 #20 AWG Diamond 4 #20 AWG 2 1 3 #20 AWG #20 AWG #20 AWG 2 #20 AWG 3 01 - #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG #20 AWG SH REV ALL ZONE 3 SIGN DATE 25.04.13 OÄM 40-363 FIRST RELEASE 2 SCALE NTS SH 1 01 D44-9 2 2 1 -4 0 -0 1 DWG.NO. 710197 DAI A CODE DA 40 N G 01 "-" REV Confidential OF N. A. Otto-Straße 5 A-2700 Wiener Neustadt MAIN BATTERY HEATERS BACKUP BATTERY HEATERS APPROVAL 25.04.13 SEE TB DATE 1 Schematic, Bat tery Heaters DWG.ORIG. TITLE PROJECT REVISION DESCRIPTION 2 Diamond Aircraft Industries BATT. HEATER 230V AC 1 #20 AWG BATT. HEATER 230V AC #16 AWG 4 #16 AWG IDENTIFICATION MARKINGS 5 A B C D E F