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PAGE INTENTIONALLY LEFT BLANK BATTERY SERVICING 1. BATTERY MAINTENANCE A. Tools and consumable materials - Protection product (TB 05-918) - Petrolatum (TB 04-012) B. Procedure 1) Apart from periodical maintenance, the only precaution required for proper battery operation is the regular checking of its charge. a) Check the electrolyte level. Under all circumstances, the level should never fall below the plates, if, however, this occurs, restore it by adding distilled water only. b) Periodically check the electrolyte density : battery REBAT R.35 - 30°B. If these values are not reached, proceed to a regular charging, according to the type of battery : battery REBAT R.35, charge to 4 AH. c) For any information concerning GILL batteries, refer to GILL "Service Manual". ABAA Validity : S / N 1 - 9999 24-30-02 Page 301 (cA) OCT 02 PAGE INTENTIONALLY LEFT BLANK ABAA Validity : S / N 1 - 9999 24 30 02 _ Page 302 (CA) OCT 02 BATTERY SERVICING 1. BATTERY MAINTENANCE A. Tools and consumable materials - Protection product (TB 05-918) - Petrolatum (TB 04-012) B. Procedure NOTE : For any information concerning "CONCORDE" batteries, refer to the "CONCORDE AIRCRAFT BATTERY" Manual. CAUTION : NEVER LEAVE A BATTERY DISCHARGED, AS IT MAY DETERIORATE ITS COMPONENTS. NEVER CHARGE A BATTERY WITH A VOLTAGE HIGHER THAN 28.8 VOLTS. AN OVERVOLTAGE MAY DETERIORATE THE COMPONENTS OF THE BATTERY. WHEN A BATTERY IS NOT USED, COMPLETE THE CHARGE EVERY 90 DAYS. Charge the battery under a voltage of 28.2 volts. ACAB Validity : With front battery 24-30-02Page 301 (cG) OCT 02 PAGE INTENTIONALLY LEFT BLANK ACAB Validity : With front battery 24-30-02Page 302 (CG) OCT 02 BATTERY REMOVAL / INSTALLATION 1. REMOVAL OF THE BATTERY (Figures 401 and 401A) A. Tools and consumable materials - Battery strap B. Procedure WARNING : DISCONNECT ANY AUXILIARY POWER SUPPLY BEFORE DISCONNECTING THE BATTERY. 1) Open baggage compartment. 2) Remove carpet (7) behind rear bench. 3) Remove inspection door (9) 243. To do this, rotate 1/4 turn fasteners (10). 4) Disconnect lugs (1) and (4) from battery (6). 5) Using strap (2), remove battery from its tray (5). WARNING : IF AN AUXILIARY POWER SUPPLY IS USED, INSULATE BATTERY LUGS WITH RUBBER OR PLASTIC MATERIAL. 6) If necessary, remove tray (5). 2. INSTALLATION OF THE BATTERY (Figures 401 and 401A) A. Tools and consumable materials - Protection product (TB 05-918) - Battery strap - Adhesive (TB 08-006A) - Petrolatum (TB 04-012) 中国通航网 www.ga.cn 通航翻译 www.aviation.cn 本文链接地址：TB20 MAINTENANCE MANUAL 24 COMMUNICATIONS TB20飞机维护手册 电源(32) |
