Biocidal Shock Treatment for Heavy Contamination - With Fuel Mixed with Kathon Biocide
TASK 28-11-00-600-009-A-01
Biocidal Shock Treatment for Heavy Contamination - With Fuel Mixed with Kathon Biocide
Do this procedure not more than 10 days after the second fuel sample continues to show heavy contamination.
If you have to use KATHON after BIOBOR, you must make sure that the fuel quantity for all tanks is at low level.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Referenced Information
3. Job Set-up
Subtask 28-11-00-941-107-A
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(3) Make sure that the ground safety locks are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(4) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate:
Subtask 28-11-00-960-061-B ** ON A/C NOT FOR ALL
Subtask 28-11-00-860-108-A ** ON A/C NOT FOR ALL
Subtask 28-11-00-942-113-A
[Rev.9 from 2019]
2026.04.02 06:16:59 UTC
Biocidal Shock Treatment for Heavy Contamination - With Fuel Mixed with Kathon Biocide
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Do this procedure not more than 10 days after the second fuel sample continues to show heavy contamination.
If you have to use KATHON after BIOBOR, you must make sure that the fuel quantity for all tanks is at low level.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.11KBB1) | Antimicrobial Agent-Fuel System Liquid Additive - |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-11-28-650-003-A | Pressure Refuel with Automatic Control |
| TASK 12-32-28-281-001-A | Drain Water Content |
| TASK 12-32-28-281-003-A | Sample Fuel for Microbiological Contamination Analysis |
| TASK 12-32-28-281-005-A | Operate Water Drain Valves in Installed ACT(S) to Drain Accumulated Water |
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 28-00-00-910-001-A | Fuel Safety Procedures |
| TASK 28-11-00-600-003-A | Removal of Microbiological Particles |
| TASK 28-11-00-600-009-A | Biocidal Shock Treatment for Heavy Contamination - With Fuel Mixed with Biobor Biocide |
| TASK 28-11-00-600-009-A-01 | Biocidal Shock Treatment for Heavy Contamination - With Fuel Mixed with Kathon Biocide |
| TASK 28-11-00-600-009-A-02 | Biocidal Shock Treatment for Heavy Contamination - Using Biobor Biocide With a Metered Injection Rig |
| TASK 28-11-00-600-009-A-03 | Biocidal Shock Treatment for Heavy Contamination - Using Kathon Biocide With a Metered Injection Rig |
| TASK 28-25-00-650-001-A | Pressure Defuel |
| TASK 28-25-00-650-003-A | To Drain Remaining Fuel from the Wing Tanks and the Center Tank |
| TASK 28-25-00-650-003-A-01 | To Drain Remaining Fuel from the Wing Tanks and the Center Tank |
| TASK 28-25-00-650-005-A | To Drain the Remaining Fuel from the ACT |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TASK 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
| TASK 49-32-11-610-002-A | Fuel Filter Element - Removal/Installation (APS 3200) |
| TASK 49-32-41-920-001-A | Replacement of the Fuel Filter (131-9(A)) |
| TASK 73-11-06-000-801-A | Removal of the Fuel Filter Element |
| TASK 73-11-06-400-801-A | Installation of the Fuel Filter Element |
| TASK 73-11-10-920-001-A | Remove, Inspect and Replace Fuel Filter Element |
| TASK 73-11-10-920-001-B | Remove, Inspect and Replace Fuel Filter Element |
Subtask 28-11-00-941-107-A
WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
A. Safety PrecautionsNOTE: This procedure is applicable to Antimicrobial Agent-Fuel System Liquid Additive - (Material No.11KBB1) only. The material is Kathon. For the equivalent procedure with the use of Biobor (Ref. AMM TASK 28-11-00-600-009).
(1) You must obey the fuel safety procedures when you do work on the fuel system (Ref. AMM TASK 28-00-00-910-001). (2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(3) Make sure that the ground safety locks are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(4) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate:
- The aircraft engines
- The flap/slat system
- The fuel system.
B. Replace the Fuel Filter Elements
(1) You must replace the fuel filters for the engine and for the APU:
(b) Replace the APU fuel filter element:
Subtask 28-11-00-960-061-F ** ON A/C NOT FOR ALL (1) You must replace the fuel filters for the engine and for the APU:
- Before the first flight after the biocide treatment
- Then between the subsequent 50 to 75 flight hours.
NOTE: You can replace the filters before you do this procedure, during or after this procedure.
(a) Replace the No. 1 and 2 engine fuel filter elements (Ref. AMM TASK 73-11-10-920-001). (b) Replace the APU fuel filter element:
- for the 131-9(A) APU (Ref. AMM TASK 49-32-41-920-001)
- for the APS 3200 APU (Ref. AMM TASK 49-32-11-610-002).
B. Replace the Fuel Filter Elements
(1) You must replace the fuel filters for the engine and the APU:
(b) Replace the 131-9(A) APU fuel-filter element (Ref. AMM TASK 49-32-41-920-001).
Subtask 28-11-00-860-107-A (1) You must replace the fuel filters for the engine and the APU:
- Before the first flight after the biocide treatment, and
- Between the subsequent 50 to 75 flight hours.
NOTE: You can replace the filters before you do this procedure and during or after this procedure.
(a) Replace the No. 1 and 2 engine fuel-filter elements (Ref. AMM TASK 73-11-06-000-801) and (Ref. AMM TASK 73-11-06-400-801). (b) Replace the 131-9(A) APU fuel-filter element (Ref. AMM TASK 49-32-41-920-001).
C. Aircraft Maintenance Configuration
(2) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(3) On panel 115VU, make sure that the ENG 1 and 2 switches are in the OFF position.
4. ProcedureWARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002). (2) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(3) On panel 115VU, make sure that the ENG 1 and 2 switches are in the OFF position.
Subtask 28-11-00-860-108-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(2) Defuel the aircraft (Ref. AMM TASK 28-25-00-650-001).
(3) Drain the remaining fuel from all of the tanks (Ref. AMM TASK 28-25-00-650-003).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 28-11-00-860-108-B ** ON A/C NOT FOR ALL CAUTION:
DO NOT USE A LARGE QUANTITY OF KATHON BIOCIDE IN THE FUEL. MORE THAN 100 PPM IS NOT PERMITTED IN:
(1) Drain the water from all of the fuel tanks (Ref. AMM TASK 12-32-28-281-001). - THE ENGINES
- THE FUEL TANKS
- THE FUEL UPLIFTED TO THE AIRCRAFT.
(2) Defuel the aircraft (Ref. AMM TASK 28-25-00-650-001).
(3) Drain the remaining fuel from all of the tanks (Ref. AMM TASK 28-25-00-650-003).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
A. Aircraft Maintenance Configuration
(2) Defuel the aircraft (Ref. AMM TASK 28-25-00-650-001).
(3) Drain the remaining fuel from all of the tanks, (Ref. AMM TASK 28-25-00-650-003) and (Ref. AMM TASK 28-25-00-650-005).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 28-11-00-615-058-A CAUTION:
DO NOT USE A LARGE QUANTITY OF KATHON BIOCIDE IN THE FUEL. MORE THAN 100 PPM IS NOT PERMITTED IN:
(1) Drain the water from all of the fuel tanks, (Ref. AMM TASK 12-32-28-281-001) and (Ref. AMM TASK 12-32-28-281-005). - THE ENGINES
- THE FUEL TANKS
- THE FUEL UPLIFTED TO THE AIRCRAFT.
(2) Defuel the aircraft (Ref. AMM TASK 28-25-00-650-001).
(3) Drain the remaining fuel from all of the tanks, (Ref. AMM TASK 28-25-00-650-003) and (Ref. AMM TASK 28-25-00-650-005).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
B. Removal of the Microbiological Particles
(1) Do the procedure for the removal of microbiological particles (Ref. AMM TASK 28-11-00-600-003).
Subtask 28-11-00-670-064-A (1) Do the procedure for the removal of microbiological particles (Ref. AMM TASK 28-11-00-600-003).
NOTE: Do this procedure as soon as possible. This will prevent corrosion of the fuel tank structure.
C. Biocidal Shock Treatment for Heavy Contamination - with Fuel Mixed with Kathon Biocide
(1) In not more than 10 days, refuel all the fuel tanks to the maximum capacity. Refuel with fuel mixed with Antimicrobial Agent-Fuel System Liquid Additive - (Material No.11KBB1) , at a concentration of 100 ppm (by volume) (Ref. AMM TASK 12-11-28-650-003).
5. Close-up(1) In not more than 10 days, refuel all the fuel tanks to the maximum capacity. Refuel with fuel mixed with Antimicrobial Agent-Fuel System Liquid Additive - (Material No.11KBB1) , at a concentration of 100 ppm (by volume) (Ref. AMM TASK 12-11-28-650-003).
NOTE: AIRBUS recommends that you refuel the aircraft to the maximum capacity. If this is not done (for operational reasons) microbiological contamination can stay in the upper part of the tanks.
(2) Let the fuel stay in the tanks for between 12 and 24 hours. NOTE: In a high ambient temperature, the soak time must be a minimum of 12 hours. In a low ambient temperature, the soak time must be a minimum of 24 hours. AIRBUS recommends that you always let the fuel stay in the tanks for 24 hours.
(3) During the soak time: - Do not move the aircraft
- Do not operate the fuel pumps or APU
- Do not do water drain tests, a high concentration of biocide will be in the sample.
NOTE: Obey the engine manufacturers restrictions and guidelines for your aircraft.
Subtask 28-11-00-942-113-A
A. Removal of Equipment
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Subtask 28-11-00-281-058-A NOTE: For disposal of waste fuel, refer to the local regulations.
(1) Make sure that the work area is clean and clear of tools and other items.(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
B. Contamination Check
(1) Do the sampling procedure again in 10 days (but after a minimum of 5 flights) to check for contamination (Ref. AMM TASK 12-32-28-281-003).
(1) Do the sampling procedure again in 10 days (but after a minimum of 5 flights) to check for contamination (Ref. AMM TASK 12-32-28-281-003).
NOTE: AIRBUS recommends that if you get a negligible result, you do not continue to use the biocide treatment.