24-30-99 ‘company of Sep 23/2019 DrorarOPERATING AND MAINTENANCE MANUAL sart This document and all information contained herein are the property of Saft. Its use is restricted solely to the maintenance of Saft batteries and may under no circumstances be used for any other manufacturer's prod- ucts. No person may, in whole or in part, duplicate, use or disclose this information for any other purpose without the prior written consent of Saft Page 2 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL ion History of revi HISTORY OF REVISION Dat ‘Modification Tarracions, SSSOHE ed ‘corecons; 17801, 447CH@ aca carectons corrections, TOW, 27478 added TEIGH®, 295762, 2576 Padded ad conactons "AAOTE-21, 2708-2 added and corecons Corrections “407614, 4078-19, ITOH aced Comectons, 4076 ade 231%, 276, 27082, 407, ADT, ATE aed 4076-1, 4076-2 added "35CH6 assed Corrections BAT6, ZTE, PATS, ANTE, AT OTE, ATED ced Comectons ‘S300H2, 437CH Ta, 2778-2 added 2TOGHT, a02TE- 14, 345C1 eed PrOCHIO acded "AZTECHT ad, update of fowchar fr Peroial Check and General Overhaul Comectons 25401, 2401-3, 23490-1 aaed Page 1 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart History of revision Page 2 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL HISTORY OF REVISION - INTRODUCTION - 1. General ~ 2. Website - 3. Definitions 4. Safety ‘4-1. Physical. - 4-2. Electrical 4.3, Chemical - Aircraft Conversions Ground Applications Placing a new battery in service - initial commissioning Battery Ratings - 8-1, Capacity ~ 9. Recycling ~ 10. End of life cells, 11, Measurements 41-1. Units of Measure 11-2. Measurement Conversion Table - 11-3. Temperature Conversion Table ~ 11-4. Abbreviations DESCRIPTION AND OPERATION - 1. Description 4-1. General 1-2. Batteries - 13. Cells 4-4. Connectors 2. Operation - 2-4, Temperature - 2-2. Maintenance - 23. Ventilation ~ 3. Charge 3-4, Constant Current Charge - 3-2. Rapid Partial Charge 33, Constant Potential Charge - 344, Other methods of charging = TESTING AND FAULT ISOLATION - 1. Introduction ~ 41-1, Battery electrical faults - 4-2. Cell faults. ~ 4-3. Physical faults DISASSEMBLY 1. Introduction - 2. Safety 3. Equipment 3-1. Standard tools 3.2. Special tools = 4, Disassembly procedures - 4-1, Removing the cover (010) ~ 4-2. Removing the cells (100) - 4-3, Removing the vent valves (160) 4-4, Removing the connector 4.5, Removing the sensor (if applicable) 4-6, Disassembly of the battery - CLEANING --- 1. Introduction 2. Safety 3. Equipment Page 1 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart 344, Standard tools 3-2. Special tools - 3.3, Consumables - 4. Light Cleaning 4-1, Procedure 5. Thorough Cleaning - 5-1, Procedure 6. Lubrication INSPECTIONICHECK - 4. Introduction ~ 1-1, General 2. Safety - 3. Equipment 3+4, Standard tools 3:2. Special tools - 4, Maintenance intervals 4-1, Periodical check = 4.2. Regular check 4.3, General overhaul Recording Periodical check - 6-1. Visual Inspection - 6-2. Insulation check - 6-3. Nut tightness - 6-4, Polarization test - 6-5. Residual discharge 6-6, Adjust electrolyte level 6-7. Supplementary test - 7. Regular check 7-4, Cell shorting - 7-2. Capacity check 8 General overhaul 8-1. Component inspection 8:2. Replacement of faulty components 8.3, Sensor check - 8-4. Vent valve test 9. Return to Service After Storage ASSEMBLY - 4. Introduction ~ 2. Safety - 3. Equipment 3+4, Standard tools 3-2. Special tools - 4. Battery Assembly 4-1, Installation of the vent valve (160) 4-2, Assembly of the battery = 4.3. Fillin FITS AND CLEARANCES -- 8001 4. Introduction ~ 8001 2. Specification table SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES - - 9001 1. Introduction - ‘9001 2. Standard tools 9001 3. Special tools 2002 31. Tool kit - ‘2005 4. Consumables ILLUSTRATED PARTS LIST 1. Detailed part list - 2. Battery part lst Page 2 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL 24, BACIO2 ~ = 10009 3. Links part ist = 10009 34. List ~ = 10009 3.2. Drawings - + 10014 4.Cell part lst = = 10020 STORAGE (INCLUDING TRANSPORTATION) - - 15001 4. Introduction = = 15001 1-1. General ~ 15001 4-2, Storage room ~ 15001 4-3. Temperature conditions + 15004 2. Inactive long term storage = 18001 3. Inactive stand-by storage ~ + 15002 344, Definition - ~ 15002 3-2. Ambient temperature with ‘topping’ or ‘refresh charge! + 15002 3.3. Action atthe end of the standby period - = 18003 4. Active stand-by mode 5. Spares 5+1. Spare Cells 5:2. Spare O-rings, gaskets and vent valves - 5-3. Other spares - 6. Servicing after discharged storage 7. Transportation procedure - Use of a trickle charge) - + 15003 = 15003 15003 15003 15003 15004 15004 Page 3 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart PAGE INTENTIONALLY LEFT BLANK Page 4 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL INTRODUCTION 1. General 2. Website 3. Def 4. Safety 4-1. Physical 4-2. Electrical INTRODUCTION ‘This manual provides the information necessary for an experienced shop technician to maintain Saft nickel- ‘cadmium batteries. It describes construction of the battery, as well as techniques used to operate, maintain, repair, overhaul, and generally care for the battery. Following these instructions will enhance the ability 10 ‘obtain optimum performance and maximum life from Saft batteries. Saft offers training classes that will assist in the optimization of battery life and the lowest possible maintenance costs. Contact your preferred Saft rep- resentative for further details, All aircraft batteries require checking and maintenance in order to make sute they are safe when installed ‘and they perform their required functions especially in emergency conditions on board the aircraft, Mainte- nance checks also permit any problems to be identified and corrected. The maintenance interval is the period {or which correct operation is assured with a low probability of failure and allows high levels of MTBUR and MTBF to be achieved. Apart from the question of safety, the avoidance of failure on board the aircraft, with ‘consequent costly impact on delays, reduces operational costs. NOTE:Some Saft battories have a specific Component Maintenance Manual (CMM) assigned to them. fa. CMM exists, that information will supersede the contents of this manual for that particular battery type and this document will become supplemental. Contact a Saft representative, or check the Saft website at www.saftbatteries.com/cmmi, for a complete listing of available Component Maintenance Manuals. Every effort has been made to provide complete and accurate instructions. Ifa situation should arise that is ot adequately described in this manual, please contact Saft via the internet at wwnw.saltbatteries.com or at ‘one of the following addresses Seft America Inc (V09062) So (5177) 7H Industral Boulevard 2squalC Pasque Valdosta, Georgia 31601 - USA 2300 Leva Pret - France To +1 (220) 2472331, ‘ols #39 198 69 1600 Fax (229) 247-8405 fax 123 198.6216 18 Saft manufactures a wide range of batteries for aircraft applications. These batteries vary in size, weight, ca- pacity andior electrical performance to fit the specific requirements of the application. The Specification ta- bles in E1TS AND CLEARANCES chapter list the basic specifications for the Saft batteries covered by this, manual. For information on Saft batteries not listed here, contact your local Saft representative. {Al Saft technical documentation, distributors and repair shops can be found on www.saftbatteries.com. ions Warnings call attention to use of materials, procedures, or limits, which must be followed precisely to avoid injury to persons, Cautions call attention to procedures which must be followed to avoid damage to equipment. Notes call attention to procedures which make the job easier. |: Except for those steps that require the battery to be charged, do all steps on discharged batteries, {refer to Residual discharge paragraph) to avoid the possibility of electric shock. Tighten vent- valves (160) prior to beginning discharge. Battery cells deliver very high current when short-cir- cuited. Exercise caution. Remove rings, watches, necklaces, metallic belts or other jewelry to avoid electric shock. 1: Do not tlt the battery while doing maintenance, any contact of skin with electrolyte can cause se- vvere burns. Safety rules are different from one country to another. Always follow local safety regulations. ‘There are three types of risks. - Handling: the battery is heavy. When you lift it, bend your legs and not your back. = Use protective shoes, = Do not wear rings, watches, chains, belt buckles, necklaces or any other metallic objects. Page a Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart INTRODUCTION - Use insulated tools 4-3. Chomical For a complete listing of hazards, refer to the safety information sheet available on Saft's website at ‘ww saftbatteries.comicmm - Electrolyte is very corrosive and can damage the skin: use gloves and an apron. If t touches the skin, flush affected part with large quantity of water. Remove contaminated clothing, after flushing begit - Electrolyte is very dangerous for eyes, use protective goggles. If the electrolyte comes in contact with an eye, flush it with water during 15 to 30 minutes. Get medical attention immediately. - Saft recommend the use of an amphoteric solution (both acidic and basic behavior) and chelator {able to trap cations as a chelate complex) according to the local regulation. - Electrolyte ingestion can cause damage to the throat and the respiratory tract. Do not try to vomit Get medical attention immediately. - Skin contact with nickel can cause chronic eczema. ~ Inhalation of cadmium oxide can cause dry throat, headaches, vomiting, chest pain. If inhaled, re- ‘move to fresh air. If not breathing, give artificial respiration. I breathing is dificult, give oxygen. Get ‘medical attention immediately. Potassium hydroxide in the electrolyte can cause eczema 5. Aircraft Conversi ns Saft aircraft batteries come in a wide variety of configurations that are approved for installation on selected aircraft. When replacing a lead-acid battery with a Saft nickel-cadmium aircraft battery, itis vitally important to clean all mounting and holding fixtures in the aircraft prior to installation. All traces of acid and salt should be removed by washing with a neutralizing agent such as sodium bicarbonate (baking soda) in water. Once the area has been fully cleaned and prepared, the surface should be painted with an alkaline resistant paint. ‘This preparation should ensure that your new Saft battery will not be harmed by sulfuric acid residue. 6. Ground Applications ‘Your Saft battery can be used in such ground applications as starting gas turbine generators, ground mobile ‘equipment, or in shop testing equipment. The same principles used in fight operations apply when the bat- {ety is used in ground applications. Ventiation ofthe battery during ground use can be accomplished through ‘ ventilation system or by simply removing the cover (only in a well-ventilated area). Check with your local ‘authorities for regulations in effect for your area, 7. Placing a new battery in service - initial commissioning NOTE:Whethor or not the battery has been subject to disassembly and reassembly, before its issue to service and installation, the tightness of all connector nuts / screws must be checked to ‘make sure that torque values correspond with those specified. Saft batteries are shipped discharged. A Visual Inspection, Insulation check, Nut tightness, Charae, Adjust slectralyte level should be done prior tothe battery being placed into the aircraft for service. Refer to the INSPECTIONIGHEGK chapter. If the battery has been stored for longer than 3 months, refer to Servicing after discharged storage ‘Storage period includes transportation and delay of delivery. Starting date for this period is the date of man- ufactuting (MF), Page b Sep 23/2019Sart INTRODUCTION 8. Battery Ratings 8-4. Capacit Nickel-cadmium batteries are rated in terms of capacity in ampere-hours (Ah) (rated capacity). ‘American Standard AS8033 defines capacity as “the dischargeable ampere-hours (An) available from a fully ‘charged cellfbattery at any specified discharge rate/temperature condition", Other definitions for battery ratings can be found in EN2570, IEC 60952 and RTCA DO 293. ‘A battery rated for 1C, Ah show that the battery is rated at a value based upon a discharge time of 1 hour at 23°C + 3°C (73.4°F + 5.4°F), In other words, a battery with a rated capacity of 40 Ah (1C; Ah) will deliver no less than 40 A for one hour when new. Atypical discharge curve for Saft VHP series cells can be found in Figure 1. ‘Type VHP cells (20 cells) Coad terminal votoge ve capactydscharged for varous charge curent at 23°C (73.5°F) 1C1A and 10618 28 Voltage (V) 26 24 2 sc1an 2 18 toc1An 16 Capacity (%C1Ah) a 2 0 © 8 100 120 Discharge Curve for VHP Series Cell Figure 1 Page c Sep 23/2019 OPERATING AND MAINTENANCE MANUALOPERATING AND MAINTENANCE MANUAL sart INTRODUCTION 9. Recy All batteries eventually lose their abil to perform and are eligible for scrap and recycling. Saft takes envi- ronmental matters seriously and advocates proper recycling of nickel-cadmium batteries and their compo- nents. To that end, Saft operates recycling faciliies in both Europe and North America. Nickel-cadmium batteries contain nickel, cadmium, and potassium hydroxide and should be disposed of properiy. In all cases, rely on local and national regulations for proper battery disposal andior shipping to an ‘appropriate recycling location. Ni-Cd Universal Recycling Symbols Figure 2 ‘You can find the nearest recycling collection point on our website www. safibatteries.com, 10. End of life cells EASA regulations ‘Part 145, require that end of lfe cells must be disposed of in a manner that does not alow them to be returned to service. The following procedure provides a means of complying with these regula- tions. While other authority requirements (such as FAA) may be less explicit, Saft recommends that the fol- lowing procedures be adopted In order o ensure tat end of ife cells cannot be re-used, the following procedure is recommended ~ Ensure that appropriate protective measures (refer to Safely paragraph) and MSDS are taken. “Ensure thatthe cel is fully discharged (refer Call shorting paragraph) Put one ofthe terminals fom the call Between the two sides ofa bench vice and bend unt the terminal breaks. Inthe event of electrolyte leakage, ensure that appropiate clean up measures as described in the MSDS are observed - Dispose of the cell in accordance with applicable transport, health and safety and recycling regulations (Refer to Recyeling paragraph Page d Sep 23/2019Sart OPERATING AND MAINTENANCE MANUAL INTRODUCTION 11, Measurements ‘The measurements which are given in this manual come from the original manufacturing drawings. ‘This OMM uses the “Systeme International” (S.|) units for quantities and values. It also gives the imperial Units in parentheses. 414-4. Units of Measure ian “c 144-2. US. Units * ng tn F 14-43. Multiplying Prefixes ‘Ampere hows Rates curent Rated capac fran hour Grom Degree Coss Percent nm Foot Inch Inch of mercury Pun Pun fore ach Degroe Fahrenheit oa Deca io Moga 41-2, Measurement Conversion Table 112. thea 1N 19 to From U.S. Standard System to 1.8. Measurement 0.1450 ps 0.3087 01580 i 0.2248 t 22046 0.0304 8507 tin Page e Sep 23/2019OPERATING AND MAINTENANCE MANUAL INTRODUCTION sarTt 14-2:2, From U.S. Standard System to |.S. Measurement 1 ps toe tina 1B ‘tgal(us) 1 btn se 9.9048 xP 254mm 94518 en 44462N 28,3405 9 933064 KPa 0453069 3.7854 lin 1120 Nm 4.3888 Nm 11-3. Temperature Conversion Table 11-3-4, SI MEASUREMENT Degrees Celsius (°C) Celsius = (Fahrenheit - 32) x 0.5555, 11-3-2, U.S, STANDARD SYSTEM Degrees Fahrenheit (°F) Fahrenheit = (Celsius x 1.8) + 32 11-4, Abbreviations ‘The abbreviations given below are used in this manual AECMA one EASA 4 vara Mos. a wreuR aye? European Associaton of Aerospace Indus [Ai Transport Assocation of America dat of manutsere European ir Safely Authority Federal vation Aut fowe Intomatona Transport Ai Association International Martine Dangerous Goods stated pans ist Moan ine between unechedled removal pat number sabessembiy tobe detines Vatoge Page f Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL DESCRIPTION AND OPERATION DESCRIPTION AND OPERATION 1. Description 444. General “The batteries are connected to the aircraft system: ~ According to the aircraft manufacturer, to start the engine or the APU. On the ground, to provide power before electrical power is supplied to the aircraft systems, - In ight, fa malfunction or a failure occurs in the power supply system. Cover assembly Filing instruction plate Connector ‘Sensor connector: Identification plate > Nickel-Cadmium Aircraft Battery 1-2. Batteries NOTE: The item numbers are those of the detailed parts list chaptor. Each Saft nickel-cadmium battery consists of a metalic box (020), usually stainless steel, plastc-coated steel, painted steel or titanium, containing a number of individual cells. These cells are connected in series to obtain a specified voltage, usually 12 or 24 volts nominal. Individual ces are enclosed in a polyamide con- tainer that provides insulation, allowing them to be fitted side-by-side in the battery box. Interconnection of ‘cells is via rigid, highly conductive, nickel-plated copper links(030). Each link is held in position by nickel-plat- ‘ed copper nuts (110) on the cells’ terminals (or nickel-plated steel screws for intemally threaded terminals). Inside the battery box, individual cells are held in position by partitions, liners and spacers (200), and a cover assembly (010). Each battery is designed with appropriate ventiation to allow the escape of gases produced during an overcharge condition and to provide cooling during normal operation. 13. Cols ‘The cell is the active component of the battery. This is where the electrochemical reaction occurs that con- verts chemical energy into electricity. In Saft aviation batteries, the design features are on the cutting edge of today's technology. Page 1 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart DESCRIPTION AND OPERATION ‘The active elements of the nickel-cadmium cell are either two groups of thin, porous, sintered nickel plates (VO, VP, VXP & Delta Plus (VHP) Series) or one group of positive sintered nickel plates and one group of negative Plastic Bonded Electrode (PBE) plates [ULM® Series (CVH, CVK, CVD)). In all cells, the positive Plates are sintered nickel, impregnated with nickel-hydroxide. The negative plates are either sintered nickel impregnated with cadmium-hydroxide, or cadmium-oxide applied in a non-sintered coating process (PBE), which is later converted to cadmium-hydroxide during manufacturing. In the cel, the positive and negative Plates are immersed in electrolyte, a solution of potassium hydroxide and water. ‘Within the cell container, a three-part separator separates the plates of opposite polarity. The outer layers are a fel-lke fabric, This fabric allows the electrolyte to stay in contact with the plates by “wicking”, The inner layer Is either an organic or a micro-porous synthetic material that acts as a gas barrler to control oxygen recombination during recharge, Each set of positive and negative plates is connected to a plate tab that employs a continuous welding joint for maximum energy transfer. These terminals are connected to the respective terminal posts. The terminal post is what allows external connections to be made. An O-ring seals the terminals. Each cells equipped with a vent-valve that can be removed to allow access to the electrolyte (forthe addition Of cistiled or deionized water). This valve also serves as a pressure-checking device, designed to limit the pressure inside the cell to 0.7 bar (10 psi) maximum, Many cells have a raised edge surrounding the vent-valve to contain any minor release of electrolyte that may occur during overcharge. ‘Saft cells are composed of a cover and body made of polygamy plastic. These are thermally welded together {0 form a single, leak proof container. This engures that ifthe battery is maintained and used under normal circumstances, it wll never leak. ~ Cutaway of a Vented Cell Figure 1 Page 2 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL DESCRIPTION AND OPERATION 41-4, Connectors Each Saft battery is connected to the aircraft by either a standard main power connector, such as an MS3509 type, or a special connector as specified by the aircraft manufacturer. Refer to "FITS AND CLEARANCES" to determine the connector used on the batteries covered by this manual 2. Operation 244. Temperature ‘Although Saft nickel-cadmium batteries are capable of operating in a wide temperature range [-40°C (-40°F) to +71°C (+160°F)], optimum performance Is obtained between +5°C (+41°F) and +45°C(+113°F), Charging is inefficient at temperatures below -30°C (~22"F) and is not recommended above 57°C (135°F). Charging must be stopped at temperatures above +71°C (+160°F). Unless otherwise stated, charge and discharge testing should be done when the battery temperature is be- tween #15°C and + 35°C. Pressure 750 to 1060 hPa Relative humidity < 85% 2.2. Maintenance ‘All maintenance, including charging, discharging, should be done specifically in accordance with the instruc- tions contained in this manual or a corresponding Component Maintenance Manual (CMM). Ifa CMM exists {for a battery, that information will supersede the contents of this manual and this OMM will become supple- mental 23. Ventilation Battery ventiation and cooling is accomplished through two methods. Most Saft batteries are equipped with tubes designed for the connection of a battery venting system. In others, holes in the battery box allow for heat dissipation and ventilation of any hydrogen produced, Page 3 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart DESCRIPTION AND OPERATION 3. Charge 3-4, Constant Current Charge ‘This procedure applies to a fully discharged battory. If the battery state of charge is unknown, discharge the battery at 1C,A constant current unti the battery voltage falls below 1 V / cell prior to the charge. - Remove the cover assembly (010). - Loosen, but do not remove, all vent-valves (160). ‘The operator may select one of the three below methods to charge the battery Minimum ‘Current and Current | non End of main charge fans Minimum voltage Oca | 10h Every cell > 1.5 Vor 12h DAG,Afor4h | 15vicel or VOVPHPRRE Which ever comes first 1.28 Veal fer CVHFEVODENK osc | 2h Everycell>1.55Vo0r25h | O.1G;Afor4h | 15k fr VOvENHPIe Neneh overcomes frst 1158 Vel fr CvWiCVDCVK TCA 1h Every cell> 157 Vor 4.25h | O.AC,Afor4h | 15 Viel or VOVPIHPARP fahich ier Gomes ar 1158 Veal er CvWiCvDICVK Table 1 - Charge Rates NOTE: Ifa cell voltage rises above 1.5 V during the first minute of the main charge, add § ml of dis- tilled water to that coll NOTE: Always apply the main charge for the minimum duration. NOTE: A coll whose voltage does not rise above the main charge voltage criterion may not be d fective. The only low voltage failure criterion is the minimum voltage at the end of the charge. A cell whose voltage rises above 1.75 V at 1C,A or 0.5C;A during main charge or above 1.70 V at 0.1C,A during main charge or final charge is defective During the last 18-30 minutes of the final charge, adjust the electrolyte level. 3-2. Rapid Partial Charge ‘One ofthe following two procedures can be used in an emergency situation to charge the battery to approx- imately 80% of its capacity. Do not use these procedures for charging the battery during normal main- tenance. ~ Charge the battery at 0.5C;A until the battery reaches an average of 1.55 Vicell. Do not charge for ‘more than 2 hours and 30 minutes Charge the battery at 1C,A until the battery reaches an average voltage of 1.57 Vicell. Do not charge for more than 1 hour and 15 minutes. Page 4 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL DESCRIPTION AND OPERATION 3-3. Constant Potential Charge CAUTION: Constant potential charging should not be attempted if the open circuit battery voltage is below 1.0 V per cell Inan emergency, a partially discharged battery may be recharged using a constant potential charging system such as exists on the aircraft, Do not use this procedure for charging the battery during normal maintenance: With the use of a constant potential system, itis imperative that the charge rate be checked periodically for ‘accuracy, and that the charger be set according to the average ambient operating temperature. The figures below can be used as a guide to ensure the correct charge rate used for a given ambient temperature. NOTE: A maintenance check of the battery should be done at the earliest opportunity to check bat- tery performance. Connect the battery to the constant potential power source. Charge for a minimum of 1 hour at 1.425 Vicell to obtain approximately 90% of the rated capacity ofthe battery. Recommended constant potential cell charge voltage atvarious temperatures Charge voltage (V) 18 15 14 Cell temperature 2 eee ta eae) SO er e8 ete cee e104 erat? e140) C30 2010 0 ce i Recommended Constant Potential Cell Charge Voltage Figure 3 ‘This figure shows the typical charge curves for Saft nickel-cadmium aviation batteries, Typical constant potential charge of Ni-Cd cell at normal temperature - charging voltage; 1.425 V z | w 8 140 = Charged capacity (Ah) = F60 2100) & BO be 00) 8 3 | B20 # 20/0 ch : aging curent 5 Charging time (h) ‘Typical Constant Potential Charge Curve Figure 4 NOTE:A maintenance check of the battery should be done at the earliest opportunity to check battery performanes Page 5 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart DESCRIPTION AND OPERATION 3-4, Other methods of charging In addition to the constant current method of charging, other methods that fully charge the battery can be Used. Howover, in any case, cell voltage checks (U > 1.50 V for VO,VP, VHP, VXP and U> 1.55 V for CVH) and electrolyte adjustments must be carried out using a final overcharge sequence at constant ‘current 0.1 C1A during 4 hours. If specific instructions are not given in the charger operating manual, you must first contact Saft. Page 6 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL TESTING AND FAULT ISOLATION TESTING AND FAULT ISOLATION 1. Introduction ‘This chapter gives the tests and inspections requited to find the cause of a fault condition of the unit either removed for unscheduled maintenance or during scheduled maintenance. The test procedure is given in the tables below. For each test refer to the specified procedures which specify all necessary information. 4-1. Battery electrical faults Problem Probable cause Correction (ieee bate eperaroaveaie |e) une cenralcoweds owaias | Chea cantalctnge Fis ange AE trade (clr o INSPECTION CHECK) (©) Link broken (2) Zev vl wi the battery slo" ‘Charge te baton, charge (a) Bator fay discharge Do an insulation check eter fo INSPEGTIONOHEGI) (Bary cout oren orca dteve | Mate sie ternal tt (oer SPEC: TONIGHECK). Refer to lated subsequent steps (©) Cet compete ery (@) Low insaton (a) Leakage of electro Disassemble and dean fe bat (refer t DIAS. SENBLY and CLEANING), Do anclctolye level check (fet INSPECTION. HECK Table 1 - Battery electrical faults Page 1001 Sep 23/2019OPERATING AND MAINTENANCE MANUAL TESTING AND FAULT ISOLATION sarTt 4-2, Cell faults {iy Too much walt decease oral Bator cal Probable cause Ta) Ghage rch mor than th tor too muh charge at high temperature, (0) Previous maintenance has not Been dene Correction ‘Damn te cae o orconave ge Irovossary. eel e normal eperating iemporture (ter to DESCRIPTION AND OPERATION} (2) High walor deporion: water con Surpton none or mor cll) svar tren ram te other calle nthe at tery (a) mare han 308s above the average valve of ‘edad watern alco leaking oa). (bless han 20% below he average value of ‘dd waterin al cal: cfs) wit damaged sep- sats). Disesconble ho baton (too DISASSEMBLY) Clan te battery (eter fo CLEANING). Replace the falls). Charge and do an colt vel neck ter to Note the cet cation and check the level of water con: ump vrsus oor cts the next maintenance (@)Acall has higher votage at he [Sart charge tan dofed in para Charge chapter DESCRIPTION AND /SeERATION (@) Dyce ‘When the cee coca, add 5 (5 mio ated ‘water ote et. Donal ast mare accra Unt the tof he charge. NOTE: If you charge a cell with a quantity of electrolyte which is not sufficient, this can cause temperature to increase too much. (WAcall nasa ower votage ate end of charg than eine Charge chapter DESCRIPTION AND SeERATION (g) The oot was operated al omperatres and haga ats outside the lims, and tb separator iSdamoged (b) Usual wear ater long operon Replace tho ol (fer o DISASSEMBLY, ASSEMBLY “AND Storage (ngusng anspor). (Eh Low capac cal (ey nsufiient Balorang (b) sal wear ator long operaton, (6) Unusual operation, operation at high tempera Tire or aperaton wih iow seco. ‘Repeat Gharoe dacharg at CyAH and Gal aharing upto tree tes Replace the al (fer o DISASSEMBLY, ASSEMBLY AND Sloss lincuding asprin). Do he appicable proces (refer to INSPECTION (HECK (Gi Cel wha swaien case {Wy Oat opereied win ow eco vel tea faton of eeparators and csmaged plates, Replace te ol (ter io DISASSEMBLY) (7 Gat with zoo ola when te bat ety excltis open (@) Shore aroatod cat place the oo (foro DISASSEMBLY) Table 2 - Coll faults Page 1002 Sep 23/2019sarTt OPERATING AND MAINTENANCE MANUAL TESTING AND FAULT ISOLATION 4-3. Physical faults, Problem Probable cause Correction () Leakage of elecohe ‘@)insorec adusiment of ects level (0) Cet polity incorrect ring high-rate c= ‘charge (fr example, during the engine sta ©)omen charge tion porate oo (6) Ta ower nits not cores tgntans. Disassemble and dean the baer (refer DIS- ‘ASSEMBLY ard CLEANING eraptr). Doan ‘lect evel check (fer to NSPEGTION ‘HECK Disassemble and lan the battery (refer to DIS. ‘ASSEMBLY and CLEANING). ‘Doan electrons lave check refer to INSPEC: "TONIGHECK) Investgato the cause of excessive charge. nec Sioa ral cprting terre (eer to DESCRIPTION AND OPERATION) Diesteembie and dan the bat (eter DIS. ‘ASSEMBLY and CLEANING), Do an electra aval cack tro INSPEC: ‘TONIGHECK. “Torque te lower nt (refer fo ASSEMBLY chap- or (@)Bleatoty ound nthe batery box. {@) Damaged cal case (Pr Leakage of lecuoyte Do a eak tos ofthe cls (ert INSPECTION! HECK. Replace the col necessary andrefer to rlate subsequent seps. Dlassemble and clan the bat (fer to INSPECTIONCNEGK and CLEANING). Do an electohte level check eer to SPEC. TTONIGHECK) (@)Comrosin on te trks {@) Operation in aed (©) Mechanical damage to nicks plating ‘Make sure the bata lst bench and he storage ‘teas have no materi whch can ge of sod fines, Replace tne dsmaged inks (refer fo DISASSEN- BLY, ASSEMBLY ANO Storage Gnduding tans: etalon). (The nis are Goat (ai Looe terminate nas Make ear he nul are torqued otorto NSPEC. TONCHECK) Table 3 - Physical faults Page 1003 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart TESTING AND FAULT ISOLATION PAGE INTENTIONALLY LEFT BLANK Page 1004 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL DISASSEMBLY DISASSEMBLY 1. Introduction NOTE:Refer to the TESTING AND FAULT ISOLATION chapter to identify the possible cause of a mal- function. This will give the necessary level of disassembly. ‘The instructions found in this section are designed to allow the maintenance person to completely disassem- bie the battery for the purpose of General Overhaul. However, some maintenance operations do not require ‘complete disassembly. Disassemble only to the extent necessary o effect appropriate repair or replacement. 2. Safety Refer to chapter Standard tools in SPECIAL TOOLS, FIXTURES. EQUIPMENT AND CONSUMABLES. 3. Equipment 34. Standard tools Refer to chapter Standard tools in SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES, 3-2. Special tools ‘When special tools are used inthis chapter, they are identified by a code number listed in SPECIAL TOOLS, ELXTURES, EQUIPMENT AND CONSUMABLES chapter. 4, Disassembly procedures NOTE: All () part identification numbers herein are IPL Fig. 1 item numbers and are using hypertext facility. 4-1, Removing the cover (010) Depending on the type of cover, undo the retaining latches or the retaining screws. Remove the cover taking ‘care to avoid contact between the cover and the cell terminals or links. 4-2. Removing the cells (100) NOTE: Make note of the proper placoment of the links (030 to 090) prior to removal, To facilitate ease of removal, remove the center coll in each row first. Remove the nuts (110) and the spring (120) washers that attaches links to the cells. Cut cable grip if applicable, Remove all inks (030 to 090), Fully screw the extractor tool onto a cell terminal then pull up to remove the cell (100), 4-3. Removing the vent valves (160) Loosen the vent valve with the special tool Remove the vent valve (160) wit its O-ring, 4-4, Removing the connector Remove the screws (210) and the washers (220) Remove the connector (230). 4-5, Removing the sensor (if applicable) NOTE: Note the sensor installation before removing. Unscrew the sensor from the links (030 to 090) Depending on the type of sensor, undo the retaining nut or the retaining screws. Remove the connector and the sensor harness taking care to avoid damaging the cabling Push the connector through the hole in the battery box (020). 4-8. Disassombly of the battery Remove the cover (010). Remove the cels (100). Page 3001 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart DISASSEMBLY Remove the liner spacer kit (200). Note placement prior to removal to ensure proper placement during re- assembly Remove the connector (230). Remove the sensor (if applicable). Page 3002 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL CLEANING. CLEANING 4. Introduction ‘The instructions in this chapter are forthe general cleaning of your Saft aircraft battery. The instructions un- der ‘Light Cleaning” are to be done each time the battery is removed from the aircraft, and can be accom plished with no disassembly of the battery. The section “Thorough Cleaning” includes the instructions for the ‘leaning of a disassembled battery for the purpose of General Overhaul 2. Safety Refer to chapter Standard tools in SPECIAL TOOLS, FIXTURES. EQUIPMENT AND CONSUMABLES, 3. Equipment 34. Standard tools Refer to chapter Standard tools in SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES. 3-2. Special tools When special tools are used in this chapter, they are identified by a code number listed in SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES chapter. 3-3, Consumables ‘When consumables are used in tis chapter, they are identified by a code number listed in SPECIAL TOOLS, EDCTURES, EQUIPMENT AND CONSUMABLES chapter. 4, Light Cleaning On an assembled battery, CAUTION: Do not use solvent, potroloum spirits, trichlorethylene or other products containing chlo- 44, Procedure CAUTION: To prevent injury when using compressed air, direct air stream away from the body. Use Safety goggles to prevent oye injury from airborne particles. = Remove the battery cover assembly (00). ~ Check the battery Vent tubes to ensure that they are clean and clear. = Tighten the vent valves (160) withthe Universal vent wrench (T04) = Remove potassium carbonates (white deposits) from the top of all cells (100) using a sti bristle, ‘non-metalic brush - Disperse residual salts and dust particles from the battery using blasts of clean, dry compressed a. + Goat all upper nuts (or screws) (110) and links (030 to 090) with M02. 5. Thorough Cleaning On a disassembled batory. 5-1. Procedure Faly disassemble the battery (refer to DISASSEMBLY chapter). 5-1-1, Cells (100) Make sure thatthe vent valve (160) is ight. CAUTION: Do not soak the cals in water. To easily remove all the electrolyte and mineral salts from the terminals, the cover and the sides of the cell ‘cases: clean in warm water with a soft brush, Rub the cell with a cloth and let dry. 5-1-2, Box (040) and handle (if applicable) Clean with lightly soapy water, rub with a cloth and let dry. 544-3. Nuts, spring washers and links. Page 4001 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart CLEANING Clean in lightly soapy water with a brush, rinse well with clean water and let dry 6-1-4. Liner spacer kit (200) and sensor (if applicable) Clean in warm water and let dry 5-1-5. Vent valve (160) CAUTION: The cleaning of the vent valve (160) must be done when the cells are assembled in the box. Remove the vent valve (160) (Refer to DISASSEMBLY chapter) Cover the cell holes to keep out unwanted material Soak the vent valve for some time (during the night, for example) in a container of di all salts from the vent hole. led water to remove 6. Lubrication When the battery is clean (and after installation of the vent valve), coat all upper nuts (or screws) (100) and links (030 to 020) with Moz. Page 4002 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK INSPECTION/CHECK 1. Introduction 41-4. General ‘This chapter includes the checks, the maintenance procedures and the functional tests that must be done to use Saft batteries in fight and on the ground. These maintenance steps must be completed ina battery shop: - Periodical check: adjustment of electroyie levels. Regular check: capacity test and periodical check. General overhaul: disassembly, full cleaning, assembly and regular check NOTE: All () part identification numbers herein are IPL Fig. 4 item numbers. 2. Safety Refer to chapter Standard tools in SPECIAL TOOLS, FIXTURES. EQUIPMENT AND CONSUMABLES. 3. Equipment 344. Standard tools Refer to chapter Standard tools in SPEGIAL TOOLS. FIXTURES. EQUIPMENT AND CONSUMABLES. 3-2. Special tools ‘When special tools are used in this chapter, they are identified by a code number listed in SPECIAL TOOLS, FIXTURES, EQUIPMENT AND CONSUMABLES chapter. 4. Maintenance intervals ‘The aircraft manufacturer is responsible for defining the usage and function, including maintenance intervals, {or aircraft batteries installed in its aircraft. Saft only provides recommendations that require the agreement of the aircraft manufacturer. When maintenance intervals are referred to in OPERATING HOURS, it means the sum of the fight and ‘ground operation time when the battery is connected to the aircraft network. The ratio of operating hours to flying hours depends on the operator. It is generally in the range of 1.2 for long range operation to 1.8 for short haul operation. ‘When maintenance intervals are referred to in CALENDAR TIME it means the time the battery has been in- stalled and operating on-board the aircraft and does not include storage periods NOTE:Maintenance steps must be completed in a battery shop. Saft distinguishes between three types of maintenance 4-1, Periodical check ‘The periodical check consists essentially of voltage and insulation checks, discharge of residual capacity and ‘charge with electrolyte level adjustment. The main purpose ofthis periodical check isto replace water which is consumed by electrolysis during battery overcharge. Its normally applied between regular checks but can be omitted if the water consumption measured at the regular check is within allowable limits 4-2. Regular check ‘The regular check is the same as the periodical check except that the battery is also deep discharged ("bak ancing)), followed by a capacity check cycle. 4-3. General overhaul ‘The general overhaul is the same as the regular check except that the battery is also disassembled and thor- ‘oughly cleaned and inspected. 5. Recording Its very important to record the battery check values (capacity, end of charge voltage, water consumption) ‘as required in the battery logbook for each maintenance. Its recommended that an operator tracks these maintenance data in order to check the interval is correct relative to that particular operation. This may also allow the interval to be extended if the data justifies i Page 5001 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart INSPECTION/CHECK 6. Periodical check PERIODICAL CHECK Visual Inspection OK? Insulation check U> 4.05 Vieell ro cell with reversed polarity Polarization test OK ‘Supplementary test OK? Nut tightness ‘General overhaul with Replacement of faulty compo- Battery accepted after Periodical check neni Periodical check Figure 1 At specific intervals according to aircraft use, or every 3 months, test the battery according to the above fig- ure. Consult the airframe manufacturer for specific maintenance intervals or special procedures to be fol lowed. NOTE: Time periods are given as a guideline. Modify in accordance with operational experience. Periodic and Regular maintenance checks may be combined if operating hours permit. 6-1. Visual Inspection Visual inspection should be done each time the battery is removed for maintenance. Page 5002 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK = Remove the cover assembly (010), = Visually check each cell (100) for any evidence of electrolyte leakage. If there is salt or electrolyte traces do a General overhaul. Excessive salts around a terminal post show possible leakage from the terminal Oxing. Make sure the torque ofthe lower nut (refer to chapter ASSEMBLY) ~ Inspect the links (030 to 090) and all upper nuts or screws (110), and washers (120 and 150). The hardware should be free of bends, tamish, corrosion, burns, or any loss of nickel plating. Minor tar- nish can be polished off witha fine wire brush. Defective hardware should be replaced, ~ Check the main power connector (230) for evidence of arcing, corrosion, cracks or cross-threaded terminals. Replace any defective connectors. 1: Worn aircraft connectors andior loose connections can greatly affect the performance of the bat- tory. A defective main power connector (230) can cause battery self-discharge as well as low voltage in service. = If applicable, the temperature sensor andior heater blanket harmess assembly should be inspected for obvious damage. This in no way replaces the ful testing procedures found hereafter that ensure {ull operation ofthe sensor assembly. - Inspect the electrical connector for bent or loose pins, corrosion, cracks, faily wie connections, ev idence of arcing, or eracked or loose potting material - Inspect the thermistor, thermostat, andor thermocouple assemblies (as applicable) for any darn- aged oF loose wire connections, cracks, dents, or other physical damage. - Visually check all wiring insulation to ensure there is no evidence of eracks, cuts, or bubbling. Any evidence of damage to the temperature sensor andlor heater blanket harness assembly requires the sensor replacement. = Inspect the battery box (020) and cover (010) for any damage. Minor dents may be repaired with a ‘small rubber mallet. Ensure the cover gasket (011), if applicable, is undamaged and fully secured to the metal cover (010). 6-2. Insulation check ‘A breakdown in electrical insulation between the cells (100) and the battery box (020) will result in a "leakage" current, which over time will discharge the battery. The most common cause for the loss of insulation isthe leakage of electrolyte from the cells (100) that acts as a conductor between the cells and the battery box (020), Because leakage current can affect battery performance, i 's necessary that it be kept toa minimum (On a completely assembled battery, use a megohmmeter, set to 250 V DC, to measure the insulation resistance between the pos- itive terminal of each cell (100) and the battery box (020). Refer to the table below for the acceptance criteria 250 KQ. 2a 10MQ Must be cleaned, Acceptable but Acceptable for Mandatory level of Doa General cleaning is recom- | _ inservice battery | insulation for new or ‘Overhaul mended For anew battery (di- | in service battery Check the cause rectfromfactory withno | after cleaning (overcharge...) ‘charge made by the Jcustomer) a cleaning is recommended Page 5003 1 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart INSPECTION/CHECK 6-3, Nut tightness Tighten and check the torque of all upper cell nuts (110) (refer to FITS AND CLEARANCES), 6-4, Polarization test ‘Charge the battery at 0.1C;A for 1.5 hours. Keop the battery in open circuit for 1 hour. Measure the open circult voltage of each cell. If any cells zero (0) V or negative polarity, do a General over- haul. Ifa cells are above zero (0) V, continue with maintenance as specified, Identify the cells with 0 V, they will be changed during the replacement of faulty components, 6-5. Residual discharge Discharge the battery at the 1C A or 0.5CA rate until each cell in the battery is discharged to 1.0 volt or be- low. 6-6. Adjust electrolyte level 1: Using anything other than distilled or deionized water in nickel-cadmium cells will cause electro- lyte contamination and damage. ‘Always take appropriate precautions to prevent any foreign substances from entering the cell. Anything other than distiled or deionized water that enters the cells will cause electrolyte contamination and will affect over- all performance. ‘The amount of time that the vent-valves are removed from the cell for maintenance should be limited to pre- vent as much air as possible from entering the cell. Carbon dioxide inthe air will combine with the electrolyte to form potassium carbonate, Potassium carbonate wil increase the internal resistance ofthe cells and thus decrease the performance at low temperatures and during high rate discharges. Always ensure that the vent- valves are properly secured while the battery isin use. Electrolyte level adjustment is to be done during the last 15-30 minutes of the 4 hours overcharge at 0.1C,A, rate of charge. | : Take care not to tit cells while vent-valves are loosened or removed. Contact of electrolyte with skin can cause burns. If contact occurs, flush area with large amounts of water. Electrolyte in the eyes is very serious. Flush with water and contact a doctor immediately. 1: The battery must be fully charged before adjusting the electrolyte level Use only distilled or deionized water (see chapter SPECIAL TOOLS, FIXTURES, EQUIPMENT ‘AND CONSUMABLES). Do not re-use water removed from cells. ‘The quantity (in cm?) required to level the first cell will serve as a guide for requirements of the remaining cells but the amount of water required for each cell can vary, so carry out this check on a cell by cel basis. Each cell must be leveled individually the quantity of water added per cell's above 80% of the electrolyte water volume shown in the specification tables (refer to chap- ter FITS AND CLEARANCES), check the charging system. If it is functioning properly, shorten the time period between servicing ‘Adjust the level of electrolyte, one cel at atime, using the folowing instructions: = 1, Remove the vent-valves (with the O-ring) (160) withthe vent-vaive wrench (T01) 2. Check the nozzle length before fiting itto the syringe Page 5004 | Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK - 3. Insert the syringe (T02) into the cell opening unti the shoulder of the nozzle rests on the vent- I valve seat. i= Refer to FITS AND CLEARANCES for proper distance between electrolyte and vent-valve seat, Position of Syringe in Cell Vent Seat Figure 2 ~ 4. Withdraw the plunger and check for any iquid in the syringe. ‘Any excess liquid in the cell will be drawn into the syringe unt the electrolyte is level withthe end of the nozzle. This is the correct level forthe electroiyte. Ifthe liquid level is too low, the syringe will remain empty, indicating that the end of the syringe noz- 2le did not reach the liquid in the cell In this case, replenish low electrolyte. 5, Draw 5 cm? of the distiled water (MO) into the syringe and inject it into the cel 6. With the syringe nozzle remaining on the vent-valve (100) seat, slowly withdraw the plunger in the syringe. - 7. Ifthe syringe remains empty, repeat steps 5 and 6, counting the number of 5 cm? injections re- uired to achieve the correct level. Record the amount of water added to each cell on the mainte- nance record 8. Atthe point in step 6 when some excess liquid is drawn into the syringe, the correct level for that cell has been reached. Expel the excess liquid into a separate container for disposal. Do not re-use the liquid removed from cells. Check wth local authorities for proper disposal of hazardous waste. 6-7. Supplementary test ‘The supplementary testis used to confirm faults on cells during the maintenance or to rebalance cell capacity I (severely imbalanced battery. Itis not a standard charge procedure, ‘Atthe end of complete charge (refer to Constant Gurrent Charge), continue to charge for 5 h at 0.1 GA. Measure the voltage ofthe individual cel voltages every 30 min. The individual cel voltages: ~ must not decrease by 0.03 V during the test = must be = U2 1.5 V for VOVPIVHPIVXP = U> 1.55 V for GVHICVDICVK - Adjust the electrolyte level (refer to Adjust electrolyte level). Page 5005 1 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart INSPECTION/CHECK 7. Regular check REGULAR CHECK ‘Visual Inspection OK? U> 1.08 Veal no cell with reversed polarity ‘Charge ‘and Adjust electrolyte level ‘Supplementary test OK? Battery accepted after Regular check Regular check Figure 3 At specific intervals according to aircraft use, or AFTER A MAXIMUM OF 6 MONTHS, test the battery ac. ‘cording to the above figure. Consult the airframe manufacturer for specific maintenance intervals or special procedures to be followed, Page 5006 | Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK NOTE: Time periods are given as a guideline. Modify in accordance with operational experience. Pe- riodic and Regular maintenance checks may be combined if operating hours permits. 7-4. Cell shorting ‘As each cell's voltage drops below 1.0 V, connect an equalizing resistor (103) across each cel’s terminals. Il Leave the resistors in position for 12 to 16 hours to allow each cell to completely discharge and the battery 10 cool NOTE: As an alternative to the resistor a shorting clip can be applied when the voltage has dropped. 10.0.5 Vicell 7-2. Capacity check I Discharge the battery at 1C;A. until all cel individual voltages fall below 1.0 V. Record the time when each cell falls below 1.0 V and the battery voltage falls below 20 V. ‘This time must be equal or greater to 61 min for VO and VP and 1 h for VHP, VXP, CVH, CVD and CVK cells Page 5007 | Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart INSPECTION/CHECK 8. General overhaul ‘Scheduled GENERAL OVERHAUL yes [—U> 1.05 Viel Polarization test [| (Charge and Adjust electro- Ite level DISASSEMBLY ‘Supplementary test OK? | Vent valve test ‘ASSEMBLY. Insulation check ‘Charge and Adjust electro. Iyte level Baltery accepted after general overhaul At specific intervals according to aircraft use, or AFTER A MAXIMUM OF ONE YEAR, test the battery ac- ‘cording to the above figure. Consult the airframe manufacturer for specific maintenanc® intervals or special procedures to be followed, ‘General overhaul with Replacement of faulty compo: nents. General overhaul Figure 4 Page 5008 | Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK 8-1. Component inspection 8-4-1. Colls Make sure that the lower terminal nuts are tight (refer to EITS AND CLEARANCES chapter). I Make sure that cell boxes show no leakage. 8-4-2. Box Make the sides of the box straight and remove dents. 844.3. Nuts, links and spring washers Discard the components that show signs of corrosion or damage, 8-4-4. Connector CCheck the main power connector (230) for evidence of arcing, corrosion, cracks, or cross-threaded terminals. Replace any defective connectors. 8.2. Replacement of faulty components 8-2-4. Cells - 3/5 cells rule Saft strongly recommends to change all the cells or replace the complete battery it = one or moro cells are found to be faulty and § of the original colls in the battery had previously been changed, = 3 or more cells are found to be faulty during the same maintenance. ‘The 3/6 cells rule does not apply to the following fallures: = technical fallure such as terminal thread damage, ~ cell leakage, - cell short-circut NOTE:All cells that are changed must be replaced by a now Saft cell 8-2-2, Other components ‘Any other components that are to be changed must be replaced by a new Saft component. 8-3. Sensor check 8-3-1, Insulation check I Make sure that the insulation between each pin of the connector and all metal parts of the sensor is > 10 MQ. @ 250 VDC 8-3-2. Sensor check I Do this test in a climatic chamber with the sensor disassembled from the battery. Check the sensor, i appli- cable, according to the table below. ‘When a sensor includes a thermostat with the sentence "closes on rise" or “opens on rise’, test the thermo- slat switching temperature while the temperature in the climatic chamber is increasing, When a sensor includes a thermostat with the sentence "closes on fall, test the thermostat switching tem- I perature while the temperature in the climatic chamber is decreasing, Fet77PIN | VOS052PIN Sensor Sensor Tercne CE assosonie@ 7 C28 CU KB 22Kn@ 26°C22°C(TT-F 4°) €: 27otw S27 Ko @ 25 C22 CTF 24°F) EP cpenacon tao @ 8° 25°C WO"F 20°F) 103200 15238 ‘AB opens on ise @8°C #570 (40°F 29°F) AB 18 @5°C (1 Flores T76CH Crary ‘A: doses on se @60°0+5°C (40 F297) C5: coves one @ 65°C 5-0 (M40°F 29°F) “Teche 2665600 co ai02Te B70 0327 Kz 0 @25°C22 °C TT RAF) 5: doses on ee @ 7178 "0 (00°F 9°) Il Table 1 - Sensor check Page 5009 | Sep 23/2019OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK sarTt F6177 PIN Sensor "V08052 PIN Sensor Tac Tare e2s2se-000 Ta coses niece @TFO25 COO Tre) 155: cower on ee @ 71-G5°C (100"F 29°F) 23: short cet Ten “13032 replaced by AB 2000820 @e0-Cei-C(MT F228) fHoas3 Ap massa gm-Cs3-C US 45-F) rarecre ‘66800 ‘16802000 RB MO9KD= 1 @25°C22°C (TTF AF) BE Drew aT KOG 25°C 22 CT Fed A) recta 166800 ‘16802000 RB OTSKO OP "Ce 2-7 F247) Be aewsKn@ 2 Ca2-CTFs4F) ware o77i25-000 ©. dowes on ise @ 71°C 570 (100°F 29°F) raricHt 6287 BE doses nee @ 57 "CSC (135 F297 HOKE “11880 AB 3KO@I5°C22O7 F247) mide pot wih 490K 1% resistor Delos on ae @ 71°C 25°C (160 F 49°F) SCDH a1i961 8-0: doses on rise @ 05°C = 5°C (140°F 29°F) 8.0: shotorout aoscrs aiB8i2 AB. 20410 240K @25'CAD OT FAA Gre skas xm pin Er operon ise @ 71 °C.25°C (60°F 29°F) Gu 5kns 1 aoren2 23857000 ‘AB: opens on tse @ 71-02 9°C (160-F £9°F) 5 dose ster open 60°C 8-6 (40°F £9°F) aorcHs ware 077125-000 doses on ise @ 71°C 5°0 (160°F 29°) aaron ‘0829 19736000 RODE 0B 110 @ 25022007 F24-F) Borer JoKn@25-C12°C(77 Fa4F) aorern ‘19422-000 “46; shor creut opens on ise @ 67°C 25°C(153°F 29°F) Hint2 2080 24840 @ 25°C 2607 24°F) ovens “3861 ‘1950-000 ‘RB: 1740230.@2127°C,7080F) ‘h6 20002 3108 57-69" (1a5149"F) G5: 1mns3n@2127"6 70-80") ©: 20005310 @ 57 60°C (195148) asrone “13801 ‘1960%-000 AB 1740230@ 212770 70-80"). AB 20002509 67-630 (135145"F) Go.1r40s3n@ 227°C 7080) noon s3n@ 57 69°C (195148) aaecr2 23660-000 acre ware o77i25-000 doses onion @71°C57O (00°F 2077) avon aaa76 ‘AB doses anise @71C+5°C (160 F297 XG: ones on ree @ 71°C 58°C (160° 29°F) aaron i088 “Eyelet: mil point wih 4 0 KD 18 eabtor Breyeet- 4 99K Me resttor espe «490 Ka Treanor "hermit 90.38 +040 @0°C (32) EF. termistor 0038 20450 @ 0°C (2° aaron a8 AB. 276 0327 KE 10 @ 25022 °G(T7-F RAF) C5: doves on ise @ 71°C #570 (160°C 29°), SoSH ar ‘17125-000 doses on se @ 71°C 5°C (160°F 29°F) oie wer RB coves nie QT CHSC (IIS FAIA BG: doves on rae @ 71°C 5°C (160 #9°F) aa) cd 077125-000 Ds doses on ie @ 71°C 5°C (160°F 9°) vars aiaise AB. W0KD22KN@ 2 (Ge? OTT F247) 5: doses on tse @ 71-050 (160°F 9°) 16064 wars ‘230s6-000 “2: doses on ise @ 74°C 5°C (160 F 29°F) 13 closes on ise @ 71°0 28°C (100°F £9°F) 23: shor oreut 1567 ware 77125000 doses on roe @71°045°C (60°F OF) 16562 "2007 doses on ise @ 57 "C50 (TSE E29 7F) Tees 407 o19220-000 ‘AB doses on ise @ 57 "C#5"O (195 °F297F) 5: doses on ie @ T1-C 35°C 180F 29°F) Table 1 - Sensor check Page 5010 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK F617 PIN] 08052 PIN Sensor ‘Sensor e582 762007 Co coscroniee OT rSCF EOF 768647 6057 ‘18652.000 7A doses on os @ 71-0 45°C (160°F 29°F) B.C: shor rout 136 27-000 7X: doves on ioe @ GS"C25°C (MBF OF) Cb coser onrive @63°C#5°C 140 F £9°F) eee ‘Cae 500 ‘AB: doses on se @ 57 "025°C (135°F =0°F) Co: ceeet one @ 71°C #5-C (100 -F £9°F) rasa are ITH (CD: doses onvise @71°C+5°0 (160°F 29°F) ara a7 OITA (CD: ceses once @71°C 5-0 (160"F 29°F) wine 762003 CD coses onvive @ST°C45-O (195 F ESF) wire 766800 ‘16002.000 AB WO9KNs Te @S CAPCOM EAA B.C: 276 19 s27 Kin 26°C 22°C F 24°F) ais 162368 157-000 "AE-BO: doses one @ 71°C 5°C (80-F 29°F) IAF-DE coset on ise @ 57 °C 5°C (195 F £9°F) are aoe ‘RB: doses once @ 57°02 5°C (135°F =0°F) BE choses on ios @ 57 "045°C (135 °F #9°F) CD coses nie @65 "C5 °C (145 F #9°F) GE closes on rise @O5 °C 25°C (145 °F 29°F) ant a345 RC. 1080 1112 @ 23°C (73°F) BG s0kn @ 23°C 79°F) DE 00g 23°C(73F) EF KO @23°C(73°F) B76 are OI7A2E00 CD: coses onvise @71'C=5 "O00 F#OF) avez 1767 19220.000 TRB doses onioe @ 57 02570 (135 F=0'F) Cb. ceses one @ 71 °C5-C(160-F 29°F) ares eB 00 1-2: Gosos on ise @ 57 "0-25 0138 F=07F) peoeeeeaeeeoier ee wares 766500 1002.000 AB AO9KD2 1% @25C12- CT Faay 86 araaerna@2-cs2 C07 F247) TIe7 19050 vepaced by RE 2000420 @60C41-C (iF e20F) AB I40250@24'°C#3 °C 5 F26F) ‘AB: doses on se @71°C-25°C (160°F #9°F) 23768 ‘16052.000 Aen @ 2 CTSA) RB: 200.0.@ 60°C (140"F) Cb: 40 @ 24°C 755) Cb.2000@60°C (140°) eave O19N96.000 (RB: dosos ones @ 68 °O#5°0 (45 F=0'F) 864 AGT 19220.000 TRB dosos on oo @ 57 02570 (135 .F=0'F) Cb. ceses noe @ 71 °C35-C (160 -F 29°F) rs064 6057 ‘8652-000 7B dosos on foo @7"025°C (160°F =0°F) B.C: shor rout 25062 T6057 ‘8652.000 7A doses on fos @T1-OA5 °C (160 -F FOF) B.C shor rout 71064 ae CD coser nro 71 CSCO FRO 77082 zd rod Cb cesar oniiee @71 CSCO FEOA avez a7 10220.000 TRB dosos on oo @ 5702570 (135 F=0°F) C.D. coses nie 71°C 5°C (100 "F 29°F) T76s 766578 Re MOK @29°C(79-F) EF 40KO@ 23°C(73°F) DG: shontorcut a7610 "19000 veplaced by AB 2000+ Bao CrCl FE2eF) ‘aie AB I40250@24°C3°C 5 F286) 7176.15 ‘13380 ‘AB doses on oe @ 71 -025°C 160°F 29°F) CD: ceses nse @71°C+5°0 (100 "F£9°F) EF opone on tse @ 71°C 25°C (80"F 20°F) 77616 “19003 replaced by RB 2000420 B60 C4 1-0(141 F228) ie33| AB IM0250@24°C23°C (5 F258) a000A-F 716051 18652.000 7X: doses on oe @ 71-0 45°C (160°F £9°F) B.C: shor dreut 06a eos ee ‘AB. closes on ise @71°C5°O (160°F 20°F) B.C: short creat ‘Table 1 - Sensor check Page 5011 Sep 23/2019OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK sarTt Fet77 PIN] VOS052 PIN Sensor Sensor oo Treo ‘79852000 AB cscsmme@T Crs C(O FEO) Bc shor ereut soso ‘o10422-000 6: shor creut 8.9: openson ise @ 67°C. 45°C (18°F £9°F) Hint2 20810 2440 @ 25°C 22°C 07 24°F) owen 716109 016420.000 “2: eases on tee @ 57 °C25°C 135 °F 29°F) 344 opens ise @ 8-025 °C 8 -F r9°F) aosoara are 017125-000 doses on ise @ 71°C 5°C (160°F 29°F) aor are o17725-000 doses one @71-C=5°C (180°F 29°F) ore Wae7 19z=0000 ‘RB doses on fie @ 57 "CRS-CTTSB E297) C5 doves one @ 71°C 50 (100°F 9°) ores ‘23046-000 ‘KB: doses on ree @ 69°C +5°C (16 *F 29°F) 5 doses nine @ 03°C 25°C (140-F 29°F) aori10 “68800 o7e802-000 ‘RB MO9K= 1% @25°C22°C(7T-F 4A) BLE: Bre waar KOG 25°C 22 Fed sore Ware 7725-000 (doses on ise @ 71°C 570 (100°F 97) 0762 161087 doses on ae @ 57 "C25 °C (G5 FAO A) sore ‘o19757-000 ‘RL: short oa Bc sKa@25°C22°CO7F24°F) ao768 “0828 o19756-000 RCD 85 1050 @25°Ca2-C07 F247) Borer soka@25°C22°C(77"F 24°F) ore o10422-000 66; shor creut £9: openson ise @ 68°C + 3°C (15°F 25°F) Wst2 20010 24810 @25°C22-C07 F447) aor? o7040e-000 ‘AB: doses on ree @ 63°0-+5°C (6 F£9°F) sore. ‘3861 ‘1950-000 BB 1740290 @21-27°070-00°7), KB 20003010 57-630 (135-148 F) o:4230@2127"C 70-80") €:2000330@ 57-65" (135188) sore aaa ass 000 BG: closes on ae @ 57°C 25°C (195 F 29°F) EFF closes on se @ 67°0 25°C (135 F 29°F) God e260 ‘AB doses on re @71°C-# 5°C (160"F 29°F) sare “9058 esacedby KB: 7000 @ 80°C 350 (140.F 29°F) ‘Boa XB 1r40@ 21727 70 70RD") aore.%8 ‘XB: doses on se @ 57°C ¥5°C (135 F29°F) doves on ive @ 71°C #570 (100°F 29°) DE shortereut cod ‘23627-000 ‘Rt: ahot eat Beiskn@ 25°C (7 -F) aore24 12288 ‘AB doses on lve @71 °C 5-0 (60°F 29°F) CO: dones nro 11°C 29°C (80°F 29°F) Be Shon ret sore are 017725-000 D1 eoses on se @71-C=5°C (60°F29°F) sores Wae7 rszz0 000 RB cooes nie @5T-CHSC (ISS FAOA Co: dores nro @ 71°C 29°C (00°F 29°F) sore o19422-000 45:00 @23'C(73°) 148: opens on rise @ 67°C 25°C (153°F 29°F) Hist22040 2440 @ 25°C 22°07 24°F) so788 “0888 ‘21936-000 “AB Goses on re @ 57°C 5°C (135°F 9°) CO: doees nro 71°C28°C (80°F 29°F) Er osn@20"C 68") aore70 10828 019766-000 ‘RODE 108. 1119 @ 2602207 F247) Borer JoKn@25-Cs2°C (77 Fe4F) ore 3361 “AB doses on fio 67°C 2576 (195F = 9°F) Co: doees onnive@ 710 45°C (00°F +9"F) ER won@25"C42"C (TT Fear) sore? ar2288 ‘RB! Goses on ne @71 "C2 5°C (160°F 29°F) doses nse 11-025 °C 180°F 29°F) DE: shortereut ao7e8 16000 ‘o7es02-000 AB. 499KD:1OI CHE-COT Te4 BE mow aerKn@ e-Cs2 Cur Fat) Table 1 - Sensor check Page 5012 Sep 23/2019sarTt OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK F6177 PIN Sensor 'V09052 PIN ‘Sensor ore ais86r 9508-000 RE Tenvsn@e27 C7000 7), RB 200043:0@57 63°C (195.145°F) CD 174023082127 0(70-00"T), Cd.20002306 57 63°C (135-148 "F) ore aio 7B opens on se @ 1250 (10'F29 F) B.C: opens on ise @ 128°C (10°F £9°F), e130 DE closes on roe @ 71°C 25°C (160"F 29°F) 076-6 ana 7B cosos on se @ 05 °O#5°0 (149 °F =9°F) Cb: coset nro 65°C 5° (140 "F£9°F) 768 a8 558.000 BC: coses on se @ 57 "C25 01195 F207 EF clgos on neo @ 57°C 25°C (135 F =0°F} 76-79 2657-000 ‘AB: opens on ise @ 71°C 5°C (160°F 9°) Cb: eloee ater open 80°C #5 °C (a0 F 29°F) avez “ia03s replaced by 8894 8: 2000 @ 60-C25°O (40-F 20°F) iB 174.0@ 2127 °C (7080"F) co asi 7X mide pont CB: opens on oe @ 71°C (60°F) Ep 225K @25°C22°C(7 F24-F) (CD. ceses onvise @ ST °C 5-0 (135°F 29°F) "RB doses on ioe @ 57 "025°C (135 °F =F) Cd coses one @ 71 °C45-C (160 -F£9°F) BG sKn@25°C2 CUT" 24°F) sores Ware 1725000 CD: closes onsise @71 "C5 °O(0F £9") Cb 15Kn@25"C42-C(77-F 24 "F) EF isha @25°C22°C(7T Fa") Ge 15k @ 25°C 2-07 F24-F) ao7e0 CITE OO RB 276 0327 KOs 29KO@I5 Cs 2-07 FEAF) CE closos on rise @ 60 "025°C ("40 F = 0"F) DF doses on oo @ 71° #5°C (160°F =9°F) asi7cnt O1eA20.000 12: doses once @ 57"C-#5.°0 (195 °F 29°) S44 doses on fa@ 8°C#5°C (46°F 9°) raanocH ai678 ‘RB doses on se @ 5702570 (195 °F = 9°F) Cb: coset nro @ 71 "C5" 100" £9°F) aanrcna ai386 ‘18504.000 AB 1740330@21-27 °C 70.807) KB 2000430.@ 57 63°C (195-145°F) Cb r4n230.@ 2127 0 (70-80°F) Cd.20002306 57 63°C (135148 "F) Ero a07e RB 276 0327 KOs 10% @25 "C420 FRAP) C.D. cosas on ise @71"C-5°C (160°F 29°F) aH CORED GE 2KNe200@25-0+7 007 F847) Ge ikos 00@ 25°C 22°C (77°F =4"F) Chaterycare> 202 Floater case > 20 MO wear 725000 GD: coses onvise @7HC=5°O (100F £9") weave 0787-000 RB SOI Kn@ 25 °C#2O(T7 F24F) KC 108m 1110 @ 26°C-22-C(77-F 24°F) BG 261 34KO@ 25°C 2°C (7 F847) DE 301 KN@ 25-C42°C (7 F+4°F) DF 10s 1110 @28"C22"007 F247) EF 2610 s4Ka@ 25°C22°C 07 F=4°F) 6106-1 mr) 7A doses on ee @71"C25°C (100°F 29°F) Bc ong 2 C1 F) ‘RB: doses on lbe @ 71°C 25°C (160°F =9°F) Bc on@ 25°C (73°F) ‘RB: doses on be @ 57 °C25°C (135°F = 9°F) Co. cesee nrc @ 71 °C45-C (160 -F£9°F) 7a2863 ons 00 B.C: cses on rie @60"0= 570 (40°F =0°F) Cb. eeses nse @ 60°C 15°C (140 -F £9°F) 7288 ome 7X mide pont BC sKn2 1 @25°C22°0 (TF 24°F) EF closes on te @71-C25°C (160°F $9°F) reeves cor RBI740@ 24°C (75°F) RB: 2000°@ 60 "C45°C (40 "F20°F) ‘Table 4 - Sensor check Page 5013 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sarTt INSPECTION/CHECK Fet77 PIN] VOS052 PIN Sensor Sensor ms Dres-000 Reven@n cs 7) 8.70010 @ 60°C (140°) 5:1magee-cus-r) 0:20. 60°C (140"F) nia 165000 79802000 ‘AB499KD2 1 GIS CHPOOT FAA BG: 26 STK 25°C 22°07 F247) pairs 108? 075049-000 “12: doses on be @ 57°C 5°C (195°F = 9°F) nie Te 1566000 12 coses onrse @ 57704576 (195°F £97F) 776 eras BE doses nse @57°C5°G (105 F297) BLLtahort aut 2aT6 71057 doses on ise @ 7°70 (TSE TF=97F) 278 61057 doses on ise @ 87°C S70 (TSETFA97F) Zot 07 omrrs-000 ‘AB doses on ie @ ST "C570 (185°F297F) C5: doses on io @ 71 -C 5°C (180°F 29°F) ZaoTS “9049 ‘AB: doses nse @ 57 "045°C (195 F297) doses on iso @ 71 -C-5°C 180°F 20°F) ER tan@scr2-cirrser) Ear 18800 ‘AB: doses on ise @ 57 "C2570 195°F 29°F) 5: doses on ie @ 71 -C5°C 180-F 29°F) Er ien@z-ce2 ctr etary Gi opens en rae @8°C 28-0 46 F 29°F) aaa. “7087 019220-000 “AB doses on ise @ 57°C 5°C 135°F 29°) Codon onrse@@71°C28°C (80°F 29°F) asre ‘o7es02-000 ‘AB 4O7SKO 25°C 2°0 (7 °F 24°F) B.C: 2 wszIKO@ 2 C2 CUTE 24°F) 762 079490-000 between lugs operson ite @ 05°C 8 22°O (00°F 25°) Eos] ‘66800 ‘o7e802-000 ‘AB WO9KO= 1% @25°C22°0 (7 F 4 °F) B.C: Ze Sa KG 25°C 22-7 F247) 76762 o197a7-000 ic opens on rise @ 65°0#5°C (10°F =0°F) aeret “e2001 doses on ise @ 57°C 570 (155°F 29°F) 736782 ars ‘AG: t0ew Tn @2°CT3"F Bc: soKn@ 23 C073 "F) DE toon@2s-c03y EF. 20K0@ 23°C (73°F) TeTeS “i008 ‘AB doses nse @57"C 45°C (198 F297 5: opens on tse @ 71°C +5°C (100° £9°F} 5062 16526 “RB doses on re @ 57°C 5°C (195°F 29°F) 5 doves on ise @71°C-#5 70 (100°F 29°F) Fito 063 e088 AB ones nee QT CrSC (160 F2O 7) e084 aa ‘AB: doses on iso @71°0+5°C (100°F 29°F) 5 dooes on ise @ 87°C 50 (185°F 29°F) 085 wate ‘KB doses anise @ 71°C 15°C (160 F29°F) 261087 “15260 “AB: doses on ise @71°C6°0100°F 29°F) G5: 27600 S27 King 25°C22 CTT F4-F) 2064 ware orr25000 Cs doses on ise @ 71°C 5°C (160°F 29°F) 3085 “e800 ‘7802000 AB 499KO= 1h @25°022°0 (7 -F4-F) B.C: 2761 SAT KON 25°C 22°07 F247) e084 ware 77125000 doses on five @71°045°C (60°F £9°F) 25004 116051 “AB: doses on ise @71°C#5°O (00°F 2977) C5: show orcut weet es ‘AG: 10610 @ 25 Ca2COT Fea A) Bc: soKn@ 25 cs2-C(7 F477) DE loon @2s-C22°C (rT FsaF) EF dO Kn @ 25-0 22°C (71 F847) Tie? WT o17765-000 ‘AB: doses nse @ 57 "05°C (195 F297) C5: doves one @ 1-05 0 (100°F 9°) ware “r2008 ‘NE: opens on ise @ 12°C 25°C (54°F 29°F) EF openson ae @ 12°C 250 (64°F 9°F) R=220220 B.C: pens on too @ 71°C 25°C (160"F 29°F) GH avin g 20°42 -C ar t38°F) Table 4 - Sensor check Page 5014 Sep 23/2019sarTt OPERATING AND MAINTENANCE MANUAL INSPECTION/CHECK F6177 PIN Sensor 'V09052 PIN ‘Sensor fare2 wer ‘oreza6 00 AB ancoonise@oT ors (ss FeO Eb: doses onnee @ 11-2 8-C(100-F 29°F) 000 cd 0175-000 (CD: cases on rise @ 71°C 5°C (60°F 29°) aoa7670 wesiTe 000 sowe7 10869 ‘2166-000 ‘KB. doses on se @ 57°01 5°C (195 F 29°F) C.: coses one @ 71°C 5-0 (100°F 29°F) Ersin@o-cise-F) on7ezt rans paced by KB. 2000@ 60°C 25 -C(a0.F OF) Stosss KB 174.0 21027 “0 7080") ower 16109 i600 12 eoses on fee @ 57 °C-£5°C 195 F297) 34 opens onrise @ 8-028°C (°F 29°F) z008 ar348s ‘RB doses one @ 57°C 5°C (95°F 29°F) EB: doses on rae @ 71-62 5°C(100-F 29°F) 0262 cd 01725600 Ds Goses on ne @71 "C= 5°C (180°F 29°F) a0e-4 16850 ‘AB i Oz4n @20°C27 °C (Se Fe36-F) BG Inns4n @20-C22°C(68 7 136-F) 2082 war 01725600 (Ds eoses on nse @ 71°C 5°C (180°F 29°F) zea aor ‘KB 11 OPEN @ =2°C(56-F) AB RIZIA@25°C(79-F) 08s ame ‘AB 1110240 @20°C27°C (68 F 236-7) BG iinsan @20-Ce2°C(68 F387) BE opera one @ 5-612 7) E-F opens onfso @ 15°C (6 Fj wih R= 23.0223. coo a0 AB.S9AN TK @25-C22°C UT FA) Cite pt Er closes onrse @ 71°05 (100°F 29°F) a0m087 a ‘AB doses on se @ 57704 5°C (195 F29°F) C5: coves one @ 71°C 5-0 (100°F #977) 02082 ‘66500 ‘18802600 ‘RB AO Kis 1% @25°C22°C (77-F 4°) B.C: 27010 S27 KG 25°C 22°CCT E24) oare2 WaT 010226000 ‘RB doses one @ 57 "C= 5°C (195°F 29°F) ED: doses one @ 71 -C25°C1100°F 29°F) aoarev4 “i386 ‘790-000 AB 174 23.0@ 21-27 0 7080"). 4B 20011300 57 63°C (135-48"F) So Imnssa@a2-C(r0-80"A, Gb: 200230 @57-65°C (1551457) oaret ‘273-500 “£8! opens ones @ 60°C +5°C (MOF 29°F) DG: opens en rae @ 65°C 25°C (149F 29°F) EF 206i 248K0@ 25°C +2°0(7°F 24°) 0soe.4 “10828 019756000 ACID: 10810 1110. @25:C22°C(7-F +4°F) BLCIEF 2510 MK 25°C 2°07 F 44°F) aosr63 o17698-600 BC: 3K @25°C#7°C(77-F ear) aosre.ra o17aaec00 AB AOTSKO@I CP COT FAA B.C: 27810327 HOG 25 "C22 CTF EAE) aoere.t o17aaec00 KB 4975KO@25°C+?°C (77 F24°A BC: 2r6wS2TKN@ 25 -C22-CCT FIAT) aoarea o2345-o00 ‘CONN doses on rie @ 60 “C5 °C (40°F +0°F) ECON closes on ise @ 7% “628°C (100-F 29°F) Er tkns70n@2s-C+2°C(77 F 24°F) aorret i338 ‘AB: closes on se 57°C 25°C (135° 29°F) 0: coses on ae @ 71 c= 5°C (60°F #9°F) ER v0 @25°C42°C07"F 24°F) osre.%0 o17aaec00 ‘RB MO7SKD@25-C22°C(7-F 24°F) Be 2ewsarKn@ 2 CaP COT FIA) sonore 079640000 ‘AG: doses one @ 71°G=5°C (160°F 29°F) 26054 “6278 ‘RB doses on se @71 "C= 5°C (60°F 29°F) Eb: doses on rae @ S7-C# 5°C1195°F 29°F) EF 7401506 2127 (080"F) EF 2001120511 50617 (198—142°F) [6908 SST ‘AB doses on se @ 57°01 5°C (195 F 29°F) Eb: covesonree@ 1-2 5-C1100-F 29°F) arson “a18808 ‘KC: opens on ise @ 7170 25° (160°F 29°F) Ae Disab 277 @ 227 C7080) Table 1 - Sonsor chock Page 5015 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart INSPECTION/CHECK Battery Fei77 PIN | V09052 PIN description Sensor Sensor Tae CE can snaear crs ceo Fae Check wee T ‘XB: doses once @71"025°C (160°F =9°F) Co: coses on ise @ 71°C $5°C (100 -F #0°F) Tae T ‘RB: doses on ree @Ti"C25°C (160°F +87) C:coses an ise @ 71 "C5 °C (160 -F 29°F) DE: short rout ro) T ‘RB: doses on ise @ 71°C #5°C (160°F +8°F) CO: closes on ise @ 71°C:45-C (160 -F £0°F) DE: short rout ro) 7X: doses on ioe @71-045°C (160°F 29°F) Co. eoses nie 71°C 45°C (100 -F 20°F) BE: shot creat TAB: opens on ise @ 73 -Ga5-C (160 FAO) mide point win 4.09 KA) 14 route Dez openson nse @ 8°C25 °C 6 F 29°F) DF opens on ise @ 8°C:25°C (45 F 29°F) wth 15.0resitor ‘RB: opens on se @71 "C570 (160°F 9°) mide port win 4.09 Kin 1% rotor Dz opens on ise @ 8°C'25 °C (a6 'F 20°F) DF opens on se @ 8°C 25°C (46 -F 89°F) wih 19.0resistor Table 1 - Sensor check 8-4, Vent valve test NOTE: The Vent Valve Test is not necessary ifthe full set of used vent valves is replaced by a brand +h year during the General Overhaul or when there is evidence of electrolyte over- ‘This test should be done while the battery is on charge. ‘Check the operation of the vent-valve assembly as follows: ~ Put the vent vaive (160) with its O-ring into the vent valve adapter (TOS) of the pressure test fixture, ~ Immerse the vent-valve in water and slowly raise the air pressure, = Test according to the table below, and change all vent valves if they do not pass the test ome Te asta aoranae apes <0 =) Ventas sed One pa) car pee evawoce «| aevoaonaeao | a0 | > | aswas | wawis | m | wo om aosmeen | owns | a area | Jemmaca ao] aeaaanaonezo | wo | 6] aswss | aaon | m | oamerao3y | (60) ehsied | drowns | we fares [evra «| atancoonaeea | aa | @ | aswas | awn | a | co Gesnasseans | (as) cased | drown | ws ravers —[m Jemnmaamn a0] asanaasoasao | asa | | aswss | waon | m | Gooey | 8) ebdeien | cowie | a raremn [a enwnaca [0] aaaaasaoasao | asa | 6] a5ess | awn | m | Giracoamases) | (80) eased | downy | oe jaraxs [> evawoce | « | aaaasanasao | ae | o | aswas | amis | a | wo Grencoore9) | (re) aosween | dows) | a arene | Jemnaca [0] assaasaoaeaa | asa | @ | aswss | aaon | m | foamy | 80) easwsen | dows | a jarowa [> evaoca | « | amanasanasao | ao | @ | aswas | twa | m | 70 tram) | Ge) eaeeien | wees | as pace fa ponuam —[u |aaonsnaroe | 0 | 6 | aswas | aon [a | @ ‘eomowesre) | ro) Savesen | caste) fare [> Jernenen [a] amancoomaeaa | ata | * | aseas | amu | w | a fostnenton | eo cabedin | (dete Table 2 - 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Battery fits and clearances Page 8003 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart FITS AND CLEARANCES < s| 2 4 E B 5 B) sig ig 8 2 2) 3 se (8 | 3 3 g| & gs |ecls- 4 g 8| 2 £2 |S8 Se & $ s| 3 se |e" le 5 2 2| 3 e? 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Battery fits and clearances Page 8004 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL FITS AND CLEARANCES < Ble A i 2 & g) s 368 3 2 3| ge se |§ [E 3 3 B| 5: ge lglg. : zg 8) £2 | 88 (£8 ge 3 8 3| BE se |e le § 3 Zz zz 3 = 3 3 a] § = \2 fe 2 3 & es g 3 = ia Toate ra Ea eaawaen | ereeo) aoe ao | wraioe we | moamoane | a0] 0 | aguas | —7wo | wm ] a ideas | etoto aaa [a0 | woamnae w | ewonmoais [aia | | asss | 10 | 0 | @ easwsen | eree woe fie [wrrasomna | 28 | atsontaoame | a0] 6 | aswss | 7wa | mw ] a ciated | rte area —}a0[wrraroaia | a7 | waoameoare | ae | 0} asmss | wu | | @ @abwser | stot amoai [a0 |wrraromia | a7 | wmoeaoaize | we | 0 | aswas | iw | m0 | eaawesen | cette wae ao [waromia | a7 | aanaweao | | | asess | wun | | @ @abwser | este aia [a0 [wrrarocis | ar | aeawacooane | ao | | aswss | wn | m0 | a aati) osawien | castor wea [ie |wiraromis | a7 | wawamoane | 2 | F | aswss | ou | w | % aaa)” | (ea aawser | ett) wes uo [weraroaes | a7 | eawammoane | a2] F) aswss | wou | | @ ‘oan eaawsen | cost ten Caan 89) oaaieser | (wot t2 aries [mo |wiraromis | 27 | aeaaamooane | aa | F | aswss | wu | 0 | idan to) @adtedsn | (dete) aes [a0 |wrarowis | ar | aeawawooane | aa | F | asses | wm | m0 | ‘oat eiaeaen | (cele wiem ae [wraroaes | a7 | maaamoane |e] | asess | ae | | ‘aaa 9) esawsen | coewtn voooar 20 | wou we | moaieoarso | sa | 0 | aswas | wu | 0 | a eaawsen | cost ten cova [20 | wou wo | aoaweoarso | ea | 0 | asmss | awn | 0 | 8) esawsen | (osm ten a wo | amoareoaTea | sa) 0 | aswss | ae | | @ ideas | (cere ien woos [a0 | vowooer x | waoaoawe | aa] | asas | wu | 0 | a Giaean | (dew ien soosnis fae | ween % | maoneoame | wa] 6 | as0s5 | won | mw] we cided | cece moar —[m[wirnomra as | seraneonarse | ava] 0 | asess | aon | m | idea | (cee ien coven [20 | evox wo | wmoaeoame | ur |< | aswss | aa | 20 | @ irazmaeotoes) | (63 eaawaen | crowns) | He ceascna ae ovo wo | asoasoase | m9) 6} asss | ason | | @ itso roros | @e) claws | downs | a woireni a0 | evox we | amano | a | | aswas | ame | 20 | @ ishogeecer) | an eiawien | drowns | a veirens [a0 evox % | mraassanro | ee | * | asus | awa | a | @ isteasecor) | (oa ctawa | downs | os cosas a0] wouone wo | aeaanooame | 368) € | asss | wa | 0 | @ idea | (cette Table 2 - Battery fits and clearances Page 8005 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart FITS AND CLEARANCES < s| 3 4 E B 5 B) sig ig 8 2 2) 3 se (8 | 3 3 g| & gs |ecls- 4 g 8| 2 £2 |S8 Se & $ s| 3 se |e" le — zz z z Zz 3 = s z = i g ia |g 5 a a wo [meramoane | me] P| sess] aon pe] eh asswten | caste ty pana [ao] voraer wo | mesamoaae | wo] F | sess | aon | |S ah easesen | ost ten pone [ao Yvon wo [mesamoams | 60) F | sess | aon | | = aasisen | (abt t2y fans [| vow | mesamoame | wa | | ess | aon |] eases | casei par [overs wo | mesomoaae | 7) F | sess | aon | | i eabesen | ost ten jae [a> wosaaie w | mesnmoame | we | F | ssess | aou | 0 | asswsen | (cet tn fore Jan] ves w | meacmomms | re] F | asess | aon |] = eS casesen | cts ten Cn % [maanona | are] F | asses | aon |] a eo eiaesen | tee ien a ve | meeaaoooae | 7 | F | aswss | aon | @ | 2 aatwten | (ce ten pares Jan] vemos w | mesamomms | a7) F | sess | aon |] easeeen | ose ten pares [ao wrenocn [mason | at] F | asess | en [ao] os esnwser | (eet ty area Ja] vrsnocn w | mesenomms | we] | sess | aon |] = as elses | ate iey a we | mesamoame | ae] F | asess | ou | | essween | cost ty Cr | mesamoams | we] | asess | aon |] = easton | (cen ares Jao] race wo | mexomoamo | we] | seuss | ou | | = casesen | coe ten pares [ao wren [mano | aT] F | ass | won |] a assween | cost tay a oT % | mamcom |e] F | asess | ven [a=] easwien | tet ten prea? faa wren x | mexomoamo | we | F | asess | ou | | = eabeeen | ose ten ree Jao Jwrmonsa [x |awanonane | we |) aseas | aon [= | @ essiten | aay a w [mesanomms | a7 | F | sess | aon | | = eaeeien | tet tn porear [a wren | mesamomms |e F | asess | ou | | = en aaswser | cost t2y ra ——[7ewrwnonnas [HY aeaanoomaeze | aes | 6 : qos] 0] i abiotey fore fan wanes [a | measmnane | es | | aswas | aon | w ] @ eabeten | tet tn aaa wens [a |aaawonae | ms | F | acess | aon [aw] @ essisen | cet t2y ares [ao wean [a | meacnnane | wa] | aswas | aon [a | @ asian) | (1080 124) Table 2 - Battery fits and clearances Page 8006 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL FITS AND CLEARANCES < s| 2 3 5 2 & g) s 368 : 2 lanes gz (8 js 3 3 B| 5: ge lglg. e a 8| s 82 /ZE |e 3 & s| Se BE |e" \e § 3 Zz zz 3 = 2 i &) 3 e | fg a FI q = ia Tass | wears | a | manawoame | oe | ) assess | aon | =] © easwsen | (ett ores a0 [wreaomis | @ | amaamoame | sea] ) asess | wen | | cided | cde ie voreo a0 |wrmaomis | «8 | wmacoooame | saa | F | aswas | wm | m0 | eaawesen | (tte vores fie [wrraoaea | we | eaamooaee | wea | F | aswss | ou | | én eases | cde ien worea ao [wraociasa | | maaamoame | aaa | F } asss | wen | % | a eiawien | caeotn wares [ie [vemos | a8 | aeaaeooase | ws | F | aswss | wou | w | @ eaawsen | cette ravens [a [wirmomra | a3 | aeancoooaeeo | sea | F | aswes | aon | m | @aawser | stot cores a0 |wrmasomis | «= | wmxaamooame | ss] | aswas | wm | m0 | easwaer | oot te) wares [ie |wrwomes | a8 | aeaamoaee | oe | F | aswss | wou | w | aawse7 | ett) rae [ao [wrnaocea | = | wnamoame | aaa] ) aswss | wun | | @ eh eaawsen | cost ten on 38.887 | (toe) javear —[m [wirwoma [a | aeascoooaeee | sea | F | a5w5s | ou | wm | 3 @aawser | cette vores [ao |wiraaomis | ae | wxwamooame | sea | F | aewas | wm | m0 | a esawsen | ost te fare wo |wrParoas | a7 | maaamoate | a3 | | aswss | ae | mw | @ caawsen | (wet te voroi [a0 |wearocaa | a7 | aeaaaoooame | aaa | F | aswas | wu | m0 | @ eaawsen | cost ten easwsen | (oem tan fea [> [wararoms [a7 | weancoooaeze | tea | * | aswss | ou | wm] @ @aawser | (ste vores a0 |wearoaa | ar | aeawacooame | aaa | F | aswas | wm | m0 | @ eaawsen | cost ten waraa ao [wears | 7 | waaamoaee | sa | | aswss | wen | = | © oiswien | «vet raves —|m | wirarous [a7 | aeascoooasee | sea | F | aswss | aon | m | cided | (dete ien waa [20 | wou wo | maeawean2 | a2 0 | amas | wn | m0 | easwesen | (tote vairem ae [oon we | smoamoases [a7] | asess | Tea | a | 7 ‘soca | caewsen | ete) waroons 20 evan | aonawoar | wa | F | aswas | wm | % | 3 eaawsen | costo seascre [iB oso w% | meoamoare | as] F | aswss | wou | | @ timnanve | 68) ciaieaen | costo 8 wo] vee < |aaecasaeis | 92 | 1] a3wss | 10 | @ | @ a) cided | bot Table 2 - Battery fits and clearances Page 8007 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart FITS AND CLEARANCES Z .| 3 g E 2 5 B| = sig ig 3 2 3) 3 sz |§ [5 3 3 s| & ge gee; 4 g 8| 2 £2 |S8 Se 3 8 s| 3 se |e" le 5 2 2| 3 e? 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[ao jwnows [a | meameniess | as fof 7 [= |= Senoas 0) mina [| wae | a | aeaamnness | we |e] 7 [au ]s Toate 0) mira |w [vomasa | & | wonmom | ws] 6 | asess | Tes] @ | a easwien | eto is [oro w | maaan | ar | F | asess | too | | a 2) aoswsen | rte a ao wm) maaan |e | F | asess | qos |] & asdinten | ett are Janno wm | mamma | 8 | 6 | aswss | two | 0 | caseien | eit man [| wemoms | | amoad | we] 6 | asess | we | @ | a assiien | rt are Jan wren w | mamma | Bs | 6 | awss | two | | caseien | otto Table 2 - Battery fits and clearances Page 8008 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL FITS AND CLEARANCES < s| 2 : i 2 & g) s 368 : 2 lanes gz (8 js 3 3 B| 5: ge lglg. e a 8| s 82 /ZE |e 3 é s| Se BE |e" \e § 3 Zz zz 3 = 2 i gl s fe 2g a FI q = ia Tare; wma | | moamoane | a] 6] asus | yes mw] easwesen | (2teeo) wean an [woe we | mmoamoane | ar] | amas | —7e0 | | a ah cided | oboe zewis a0 | woaaee w | mmoamoae | a7 | 6 | sas | 7w0 | 0 | ai a eaawesen | (eco) mara fo [vou wm | meoamoane | a8] 6 | aswss | yea | w | a ideas | etoeo wees a0 [wrrasomts | 28 | meoamoane | ma] | amas | —7we | wm ] a a casein | eres sre‘ fie | VPRO wm | monwoae | a5 | 6 | asuss | zea | mw | a easwadn | eres) wares ao | wramO we | maaawsams | a0] 6 | asess | yea | wa eaawsen | (een) wsrea [a0 | venom wz | masassans [ao] | seas | 7w0 | wa eaawsen | (eee) ere ie | vPaoR a | aeranueaae | aa | 6 | asws2 | swaa | wm Gea | owes mares ao |veao a atanueane | a0] 6 | aaese | —owoa | | Gaia) | ote) veerea a0 | vrnsoe we | aeranueao | m9 | @ | asms2 | soa | mo | a Gaay | owen ores [ao [wrrasomnasa | 2 | aaonwoae | a1 | 6 | aswss | 7wa | = | 8 eaaeain | eototo weerea [bo |wrwasomisea | 2 | aeoneaoazse | as] ¢ | amas | 7w0 | = |e iad | e2toco wares no [wreamomiasa | ze | maonmoane | m7 | 6 | asuss | yes | =] e esawsen | eee aioe [a0 | vaio w | woanzoane | ao] @ | aswas | 7w0 | 0 | ai ised | etoeo zeiosz [a0 | vrasocr wz | wsoczoane | mo] | amas | 7w0 | ma eaawesen | (2eeo) woes [ao [wreamomta | ze | sraaraoame | ms] 6 | aguas | yes | mw] ideas | etoto weioea [20 |woaeomia | 25 | wisdraoame | as | | aswas | 700 | mm | at (isan | etoeo woes [ie |wrrasomns | ae | woraaraoame | ms] 6 | aguas | yea | wm aaa | aioe weir ao |wrrasomns | 2 | wraaraoame | mas] 6} aswss | yes] mw] a is ised | etoeo eaoei [a0 |wrasomis | 25 | aatoneeoame | asa] ¢ | aswas | 70 | m0 | ai easweaen | (2eeo) wees [ao |wrrasomns | 28 | aaroneeoame | asa] ¢ | aguas | —7ws | mw] elses | oot eaves [a0 |wrasomis | 28 | aatoneeoaze | asa] @ | aswas | 7w0 | m0 | ai easier | (eeeo) esos [ie |wriasomna | 28 | aeocrooas2 | aa] | aswss | yea | w@ ] a ciaieae | e2toeo eos a0 [wrtasonts | 28 | aeonrooas2 | aa] | asmas | —7we | | a haan | etoeo Table 2 - Battery fits and clearances Page 8009 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart FITS AND CLEARANCES < Ale 3 E 2 5 B| = sig ig 3 2 3) 3 sz |§ [5 3 3 s| & ge gee; 4 g 8| 2 £2 |S8 Se 3 8 s| 3 se |e" le 5 2 2| 3 e? 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[a wrermas [a | aeons | ms | o | aseas | aon | @ | @ a, essiten | aay ra wo | mommozms | we | | sess | aon |] = eaeeien | tee tn roams [ao [Won ~ [eomeaans | ws [0 | sess | ou | | = aaswser | cost t2y raaez [a vrsnocn % | monmoame | wa] eo] ess | wen [=] @ estieten | cee ten mae fan wanes [ae | aooawaane | wo] | aswas | aon | w ] @ eabeten | tet tn meer fa wean [a | moawoame | wa) | aseas | aon [a] @ a essisen | caste ty maz fan wean [a | avoawoane | wa} 0 | aswas | aon [aw | @ a, eabeien | ost ten Table 2 - Battery fits and clearances Page 8010 Sep 23/2019sart OPERATING AND MAINTENANCE MANUAL FITS AND CLEARANCES < s| 2 : i 2 & g) s 368 : 2 lanes gz (8 js 3 3 B| 5: ge lglg. e a 8| s 82 /ZE |e 3 é s| Se BE |e" \e § 3 Zz zz 3 = 2 i gl s fe 2g a FI q = ia Tomes | wrasors | a | aooaeoaTees | sez | 0) sess | wen | =] © En easwesen | (ett weaoes [ao [wrocia | = | anoareoaree | a2] 0} aswss | wu | mo | oa cided | (dette veaes [a0 |wraomis | | anoaieoame | aaa | 0 | asmas | wm | m0 | a eaawesen | (stot wame7 [me [wrwomasa | @ | amoateoaree | sea | 0 | aswss | wu | % | eadean | cde ian weamea a0 [werarows | 7 | aaoamoawe | a0] 0} asess | wun | | @ @aawsen | stot eas «P| Waa m | maoneieams | me | 6 | aswss | won | | & eaawsen | cette area —|m [virmomrasa 3 | aanaaoaee | es | 6 | asnas | aon | @ | @aawsen | ost a esawien | castors ean | WOES we | maoneoavee | a0] 1 | aswss | ou | | aawser | (ett) wens [uo [wonaasa | 3 | waoaeoaree | avo] 0 | aswss | wun | = | @ eaawsen | (ost ten wear fro |voecmms | a0 | zieodeeoame | ies | asas | wm | m0 | 38.887) | (i062) pass [a vraaan wz | monsreans | ae | 6 | asess | wou | | @ @aawser | cette wea fao |woeomm [wo | amroaersawe | oo | | aswas | wu | m0 | esawsen | cost ten pare [mo [rao we | waoaraaae | a7 | 6 | assess | aon | @ ] caawesen | (ett ware [ao |wiraaomia | @ | rrearoasea | oa | | aswas | wm | m0 | eaawsen | cost ten wears a0 |wrwsromisea | sr | moamoane | sa] | asmss | wou | we | a easwsen | (oem tn ace | [wirnomis [as | sesaneooaroe | wa | 0 | aswss | ou | w] @aawser | stot wirei [oo |wirnomis | a8 | axoawsawe | oe | | ages | wu | m0 | a eaawsen | (ost ten wosee1 [ao [wreaaomnasa | | smaaeoasse | wa] 6 | aswss | eu | | osawien | ave ty fare [> [vrsomaens [00 | aernaasoaee | sea | 6 | a5wss | aon | m | chad | ocewien | os vwsres [a0 |vouoavac | 36 | aeoawoame | oa | | aswss | wm | a | a eaawaen | coer | mS waren io [vounans | 36 | aoawoase | ma | 6} asess | wen |= | @ eadean | ocewiey | oS wosrei foo |wrpaomis | 8 | aaoamoawe | ara | 6 | aswas | wie | m0 | eaawsen | costo were }ie | Woanonns | 36 | aeroaernasey | oa | 6 | aswss | wou | = | @ etawan | oats | oS were uo [wrtaaomis | = | aaoamoame | ae] 6} aswss | wu | m0 | @ idea | (cette Table 2 - Battery fits and clearances Page 8011 Sep 23/2019OPERATING AND MAINTENANCE MANUAL sart FITS AND CLEARANCES Number of cells Rated Capacity C1A, Type of Connector Lower Nut torque value N.m (Ibf.in) Electrolyte Level ‘mm Electrolyte water volume mi VAPORS Pa OaHe O20 e055 (a8i487) | (060 124) APIS AONE 2620 sess | aww asian) | (1080 124) VPADORHAC AGH ar2620 as0ss | ou (381487) | (10610 124) VAPORS 254 0aH8 02820 45055 | ow (‘0.00% 76%10.31) @8i04e.7) | (10610 124) VPADOKH 2206 2600 as0ss | ow asian) | (10810 124) ‘vPavoKt 252.0246 02600 45055 | ww (38%487) | (10610 124) PADDR AC AON BOS e055 | ww @a8ie4e7) | (10810 124) (2810487) | (0610 124) ‘ovniaoRsa 253.01197 01620 45055 Tw (0x7 864) @asie487 | e208) CvRaTIKA SO BAO 5200 5055 Tee aswaan | @21s0) ‘evnanoen Sa s000068 0280.0, as0ss | ews 8106x110) (asiesa7) | (1015) ‘ovnHoosa Pace 62056 45055 | Zemn (@.060 71<1050) (asie4a7 | (iow 15) Cvneni sa Pata D220 asses | wu (00087641031) @asweer | (1060 124) VaPTOHS SO 45055 Tos asiess7 | 2t0e0) VAPDEOS-SO 450s5 708 @aswaer | 621080) ‘veaDoRH SO) Pea a00 282 asess | aww (osextt8ts10331) (38i487) | (1080 124) VaPORHSSO 238 00082 5055 | aw sider) | (10600 124) VAPaTORS SO Bote DaTOO qsees | eu @aswear | (1060 120) VaPaTONS SO 365 ASU OTTO a50s5 | ow 88487) | (1080 124) CvnisRH TAOS HIIEO 5055 Tes (@aswsen | 2080) ‘CvnisRH Bote BED ‘aswes Two (swear | e208) KOT Blea TS 7a 7 (@9n6508063) (246) (25) Table 2 - Battery fits and clearances. MS : show bayonet type vent valves Page 8012 Sep 23/2019