C-212-100 AIRCRAFT SERIES MAINTENANCE MANUAL VERSIONS: AA1 El contenido de éste documento es propiedad de EADS CASA. Se suministra en confianza y la seguridad comercial de su contenido debe mantenerse. Este documento no debe utilizarse para ningún propósito distinto al que ha sido suministrado, ni la información contenida puede revelarse a personas no autorizadas. No debe ser reproducido ni distribuido a terceros, en todo o en parte, sin antes haber obtenido autorización escrita por parte de EADS CASA. EADS CASA. Todos los derechos reservados. THIS C-212-100 AIRCRAFT MAINTENANCE MANUAL WITH NEW ORIGINAL ISSUE JULY 15/2008 IS A TRASLATION TO THE ENGLISH LANGUAGE OF THE “MANUAL DE MANTENIMIENTO DEL AVIÓN DEL EJERCITO DEL AIRE TIPO T-12, O.T.E. 1T12-2” WITH ORIGINAL ISSUE DECEMBER 31/1995 IN REVISION 6 DATED MAY 30/1998. JUL. 15/08 REV. ORIGINAL ISSUE C-212-100 AIRCRAFT MAINTENANCE MANUAL VERSIONS: AA1 The content of this document is the property of AIRBUS MILITARY. It is supplied in confidence and commercial security on its contents must be maintained. This document not be used for any purpose other than for which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to AIRBUS MILITARY. ©AIRBUS MILITARY 2009. All rights reserved. AIRBUS MILITARY Avenida de Aragón 404, 28022 Madrid, SPAIN Engineering Support Technical Publications Fax (34) 954-59-3623 E-mail = MTA.MSI.Support.Documentation.Services@military.airbus.com Original issue: JULY 15/08 Revision 1, JUN. 15/11 Printed in Spain C-212-100 MAINTENANCE MANUAL RECORD OF REVISIONS INSERTED REV. No. ISSUE DATE 000 Jul. 15/08 CASA 001 Jun. 15/11 CASA DATE BY REV. No. ISSUE DATE INSERTED DATE BY REC.REV. C-212-100 MAINTENANCE MANUAL RECORD OF TEMPORARY REVISIONS REV. No. CHAP/SECT/SUBJ P. BLOCK ISSUE DATE INSERTED DATE REMOVED BY DATE BY INCORPORATED INTO MANUAL BY REV. No. Keep this record at the first pages of the Manual just after the standard revisions record. When Temporary Revisions are received, insert them into the Manual and make the appropiate entries in this record. R.T.REV. C-212-100 MAINTENANCE MANUAL INTRODUCTION 1. General This manual has been prepared generally in accordance with ATA Specification 100. 2. Content This manual contains information on systems and units of equipment to the level required to service the aircraft, to understand and maintain the systems to a safe standard, and to remove and install units of the systems. Servicing instructions of units removed from the aircraft are contained in the relevant Component Maintenance Manual. 3. Using the Manual A. Chapterization Chapters are allocated in accordance with ATA Specification 100. B. Chapter Breakdown Each chapter is broken down into sections: Example: 30-00-00 Ice and Rain Protection 30-10-00 Airfoil De-Icing 30-20-00 Air Intakes 30-30-00 Pitot and Static Ice Protection Each section is broken down into subsections or subsystems: Example: 30-30-00 Pitot and Static Ice Protection 30-31-00 Pitot-Probe-Ice protection 30-32-00 Angle-of-Attack Sensor-Ice Protection Effectivity: All INTRO Pag. 1 Jul. 15/08 C-212-100 MAINTENANCE MANUAL Each subsection is divided into subjects: Example: 30-11-11 De-Icer Boots 30-11-12 Water Separator 30-11-13 Regulator Valve Descriptive and maintenance information for the complete system is contained in the pages bearing the first element number only (30-00-00). Where a system is broken down into subsystems, descriptive and maintenance information for the subsystem will be found on the pages bearing the first and second element number (30-11-00). Removal and installation information of units within a system will be found on the pages bearing all three element numbers (30-11-11). C. Tab Dividers The manual is separated into chapters with yellow tab dividers, each divider indicating the corresponding chapter number and title. D. Page Numbers Page numbers blocks are allocated for different topics, the pages being numbered consecutively: Pages 1 thru 99 - Description and Operation Pages 101 thru 199 - Troubleshooting Pages 201 thru 299 - Maintenance Practices Pages 301 thru 399 - Servicing Pages 401 thru 499 - Removal/Installation Pages 501 thru 599 - Adjustment/Test Pages 601 thru 699 - Inspection/Check Pages 701 thru 799 - Cleaning/Painting Pages 801 thru 899 - Approved Repairs As no one block of page numbers if fully used, and some page blocks will not be used at all, the page numbering for a topic will have unused page block numbers in the sequence. Effectivity: All INTRO Pag. 2 Jul. 15/08 C-212-100 MAINTENANCE MANUAL E. Figure Numbers Figures are numbered consecutively within each chapter, the figure numbers reflecting the topic: F. Description and Operation - Figures 1, 2, 3, etc. Troubleshooting - Figures 101, 102, 103, etc. Maintenance Practices - Figures 201, 202, 203, etc. Servicing - Figures 301, 302, 303, etc. Removal/Installation - Figures 401, 402, 403, etc. Adjustment/Test - Figures 501, 502, 503, etc. Inspection/Check - Figures 601, 602, 603, etc. Cleaning/Painting - Figures 701, 702, 703, etc. Approved Repairs - Figures 801, 802, 803, etc. List of Effective Pages The List of Effective Pages located at the front of each chapter can be used to check the completeness of the chapter and the latest issue of the pages. The data against each page should correspond to the date on the relevant page within the chapter. G. Table of Contents The Table of Contents located after the List of Effective Pages can be used to rapidly locate a particular section or subject and to determine the effectivity of the same against different aircraft types. H. Effectivity The system to indicate the effectivity of each topic is as follows: each page has a "See TOC" indication at its bottom to forward the reader to the Table of Contents. When a determined page is applicable to a specific aircraft, the version designation of this aircraft is indicated at the bottom of the page. To cover the differences of configuration among aircraft versions in the topics, the codes CONFIG.1, CONFIG.2, etc, are used. Refer to the INTRODUCTION ANNEX II, Aircraft Series, for the cross-reference among the versions designation, CASA serial numbers and the aircraft serial numbers. Effectivity: All INTRO Pag. 3 Jul. 15/08 C-212-100 MAINTENANCE MANUAL J. Equipment and Materials The table of "Equipment and Material" of a topic includes: - The special tools and equipment necessary to do the maintenance task. When the related tool or equipment is included in the Illustrated Tools and Equipment Manual, it is identified with the location number in this manual. The location number is as follows: ITEM xx-xx-xx. - The consumable materials necessary to do the maintenance task. When the related consumable material is included in the Consumable Material List, it is indicated with the identification number in this list. The identification number is as follows: Z-xx.xxx. 4. Units of Measurement The measurements used in the manual are expressed as International System of Units (SI) units followed by an Imperial Measurement Conversion. Where a measurement, for example pressure, is read on an instrument installed to the aircraft, only the units of measurement marked on the instrument face are given. Some examples and explanation of the abbreviations used are: 5. Distance: meters (feet) expressed as: m (ft) centimeters (inches) expressed as: cm (in) Weight: kilograms (pounds) expressed as: kg (lb) Volume: liters (U.S. gallons) expressed as: l (US gal) liters (U.S. pints) expressed as: l (US pt) cubic centimeters (cubic inches) expressed as: cc (cu in) Torque: Newton meters (pounds force inches) expressed as: Nm (lbf.in) Meter Deca-Newtons (pounds force feet) expressed as: mdaN (lbf.ft) Pressure: Kilograms per square centimeter (pounds per square inch) expressed as: kg/sq cm (lb/sq in) List of Abbreviations Refer to the INTRODUCTION ANNEX I for the list of abbreviations used in this manual, arranged in alphabetic order. Effectivity: All INTRO Pag. 4 Jul. 15/08 C-212-100 MAINTENANCE MANUAL INTRODUCTION ANNEX II AIRCRAFT SERIES SERIAL NUMBER VERSION SERIAL NUMBER VERSION SERIES 100 087 088 094 096 098 099 100 102 104 105 110 111 113 114 ...................... 001 ...................... ...................... 002 ...................... ...................... 003 ...................... ...................... 0011 ...................... ...................... 0012 ...................... ...................... 004 ...................... ...................... 005 ...................... ...................... 006 ...................... ...................... 007 ...................... ...................... 008 ...................... ...................... 0013 ...................... ...................... 0014 ...................... ...................... 009 ...................... ...................... 0010 ...................... Effectivity: All AA1 AA1 AA1 AA1 AA1 AA1 AA1 AA1 AA1 AA1 AA1 AA1 AA1 AA1 -1 MILITARY -2 MILITARY -3 MILITARY -11 MILITARY -12 MILITARY -4 MILITARY -5 MILITARY -6 MILITARY -7 MILITARY -8 MILITARY -13 MILITARY -14 MILITARY -9 MILITARY -10 MILITARY INTRO ANNEX II Pag. 1 Jul. 15/08 C-212-100 MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK Effectivity: All INTRO ANNEX II Pag. 2 Jul. 15/08 C-212-100 MAINTENANCE MANUAL GENERAL INFORMATION - LIST OF CHAPTERS AA1 Date 06 - DIMENSIONS AND AREAS 07 - LIFTING AND SHORING 08 - LEVELING AND WEIGHING 09 - TOWING AND TAXIING 10 - PARKING AND MOORING 11 - PLACARDS AND MARKINGS 12 - SERVICING 21 - AIR CONDITIONING 22 - AUTO-FLIGHT 23 - COMMUNICATIONS GENERAL 24 - ELECTRICAL POWER 25 - EQUIPMENT/FURNISHING 26 - FIRE PROTECTION 27 - FLIGHT CONTROL SYSTEM 28 - FUEL SYSTEM 29 - HYDRAULIC POWER 30 - ICE AND RAIN PROTECTION 31 - INDICATING SYSTEM 32 - LANDING GEAR 33 - LIGHTS 34 - NAVIGATION 52 - DOORS 53 - FUSELAGE - GENERAL 55 - STABILIZERS 56 - WINDOWS 57 - WINGS 71 - POWERPLANT 73 - ENGINE FUEL AND CONTROL 74 - IGNITION 75 - AIR 76 - ENGINE CONTROLS 78 - EXHAUST 79 - OIL SYSTEM 80 - STARTING Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jun. 15/11 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jun. 15/11 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jul. 15/08 Jun. 15/11 Jul. 15/08 Jul. 15/08 Jul. 15/08 L.O.C. 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