R WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
R NOTE : This procedure is applicable to MICROBIOLOGICAL CONTAMIN. PROTECT.
____ R MATERIALS (Material No. 17-003) only. The material is Biobor. For R the equivalent procedure with the use of Kathon (Ref. TASK 28-11-R 00-600-009).
R (1) Put the safety barriers in position.
R (2) Make sure that the ground safety locks are installed on the landing R gear (Ref. TASK 32-00-00-481-001).
1EFF : ALL 1 28-11-00Page 345 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 28-11-00Page 346 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 28-11-00Page 347 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 28-11-00Page 348 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 28-11-00Page 349 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 28-11-00Page 350 1 1 May 01/05 1 1 1CES 1R C. Referenced Information
R (3) Obey the fuel safety procedures when you do work on the fuel system
R (Ref. TASK 28-00-00-910-001).
R (4) Put warning notices in the cockpit to tell persons not to operate:
R - the aircraft engines
R - the flap/slat system
R - the fuel system.
R Subtask 28-11-00-860-109
R B. Aircraft Maintenance Configuration
R WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED_______
R BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
R (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-
R 002).
R (2) Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001).
R (3) On panel 115VU, make sure that the ENG 1 and 2 switches are in the
R OFF position.
R Subtask 28-11-00-960-062
R C. Replace the Fuel Filter Elements
R (1) Replace the No. 1 and 2 engine fuel filter elements (Ref. TASK 73-11-
R 10-920-001).
R (2) Replace the APU fuel filter element:
R - for the 131-9(A) APU (Ref. TASK 49-32-41-920-001)
R - for the GTCP 36-300 APU (Ref. TASK 49-32-11-610-001)
R - for the APS 3200 APU (Ref. TASK 49-32-11-610-002).
R 4. Procedure_________
R Subtask 28-11-00-860-110
R A. Aircraft Maintenance Configuration
R (1) Drain the water from all of the fuel tanks (Ref. TASK 12-32-28-281-
R 001).
R (2) Defuel the aircraft (Ref. TASK 28-25-00-650-001).
R (3) Drain the remaining fuel from all of the tanks (Ref. TASK 28-25-00-
R 650-003).
R (4) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
R (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
R 002).
R Subtask 28-11-00-615-059
R B. Removal of the Microbiological Particles
R (1) Do the procedure for the removal of the microbiological particles
R (Ref. TASK 28-11-00-600-003).
R NOTE : Do this procedure as soon as possible to prevent corrosion of____
R the fuel tank structure.
R Subtask 28-11-00-670-066
R C. Biocidal Shock Treatment for Heavy Contamination - using Biobor Biocide
R with a Metered Injection Rig
R CAUTION : DO NOT USE A LARGE QUANTITY OF BIOBOR BIOCIDE IN THE FUEL:_______
R - MORE THAN 270 PPM IS NOT PERMITTED IN THE ENGINES
R - MORE THAN 1000 PPM CAN CAUSE SOLIDS IF THERE IS WATER IN THE
R FUEL.
R (1) Put MICROBIOLOGICAL CONTAMIN. PROTECT. MATERIALS (Material No. 17-
R 003) into the METERING EQUIPMENT - BIOCIDE, HAMMONDS FUEL ADDITIVES
R INC.(CAGE CODE 0U7J1).
R (2) Make sure that the METERING EQUIPMENT - BIOCIDE, HAMMONDS FUEL
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