DOC AIRBUS | AMM A320FHealth Check Procedure - Temperature Control Function with the Bleed Test Set P/N 98L36103002000
TASK 36-11-00-720-802-A-01
Health Check Procedure - Temperature Control Function with the Bleed Test Set P/N 98L36103002000
The Bleed Health Check procedure has a set of steps to do in order to check preventively the three primary functions of the EBAS.
The temperature control function contains the Fan Air Valve (FAV) 9HA1 (9HA2), the FAV control thermostat 7170HM and the sense line that connects them.
The Bleed Health Check procedures contain a flow chart that should be used for guidance. This flow chart gives a visual idea of the procedure.
The operator can remove the components that have a drift, as given in the applicable flow chart, immediately or at the next maintenance unless there is an EWD message and the source of the CLASS1 failure is the component that has the drift. In this condition, you must refer to the MMEL/TSM for the aircraft dispatch.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 36-11-00-861-137-A ** ON A/C NOT FOR ALL Subtask 36-11-00-941-139-A ** ON A/C NOT FOR ALL
Subtask 36-11-00-720-093-B ** ON A/C NOT FOR ALL
Subtask 36-11-00-080-096-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 01:07:11 UTC
Health Check Procedure - Temperature Control Function with the Bleed Test Set P/N 98L36103002000
WARNING:
MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
WARNING:
BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.
NOTE: In the health check procedures the electrical harness is in correct operating condition.
1. Reason for the JobThe Bleed Health Check procedure has a set of steps to do in order to check preventively the three primary functions of the EBAS.
The temperature control function contains the Fan Air Valve (FAV) 9HA1 (9HA2), the FAV control thermostat 7170HM and the sense line that connects them.
The Bleed Health Check procedures contain a flow chart that should be used for guidance. This flow chart gives a visual idea of the procedure.
The operator can remove the components that have a drift, as given in the applicable flow chart, immediately or at the next maintenance unless there is an EWD message and the source of the CLASS1 failure is the component that has the drift. In this condition, you must refer to the MMEL/TSM for the aircraft dispatch.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 1M(3 FT) |
| No specific | 1 | AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY |
| No specific | 1 | GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY |
| No specific | 1 | PACKING |
| No specific | AR | WARNING NOTICE(S) |
| No specific | 1 | WRENCH 5/16 IN (8MM) - SPANNER |
| No specific | Torque wrench: range to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in )  | |
| No specific | Torque wrench: range to between 2.5 and 0.8 m.daN (221.24 and 70.80 lbf.in ) | |
| No specific | Torque wrench: range to between 1.1 and 0.9 m.daN (97.35 and 79.65 lbf.in ) | |
| 98L36103002000 | 1 | TEST SET - ENGINE BLEED |
| SBE2213 | 1 | KIT TOOL-TESTER SENSE LINE |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.14QFB1) | Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 191MB | |
| FOR [1000EM1] (ENGINE-1) | |
| 437AL, 438AR, 451AL, 452AR | |
| FOR [1000EM2] (ENGINE-2) | |
| 447AL, 448AR, 461AL, 462AR | |
| REFERENCE | DESIGNATION |
|---|---|
| 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 36-11-00-720-012-A | Functional Test of the Sense Line Connected between the Fan-Air Valve Control-Thermostat and the Fan Air Valve (FAV) with the Bleed Test Set P/N 99127B03 |
| TASK 36-11-00-720-012-A-01 | Functional Test of the Sense Line Connected between the Fan-Air Valve Control-Thermostat and the Fan Air Valve (FAV) with 98L36103002000 and SBE2213 |
| TASK 36-11-43-000-001-A | Removal of the Fan-Air Valve Control-Thermostat |
| TASK 36-11-43-400-001-A | Installation of the Fan-Air Valve Control-Thermostat |
| TASK 36-11-49-000-018-A | Removal of the Pneumatic Sense Lines in the Pylon |
| TASK 36-11-49-000-029-A | Removal of the Pneumatic Sense Lines in the Pylon |
| TASK 36-11-49-000-820-A | Removal of the Pneumatic Sense Lines in the Pylon |
| TASK 36-11-49-400-018-A | Installation of the Pneumatic Sense Lines in the Pylon |
| TASK 36-11-49-400-029-A | Installation of the Pneumatic Sense Lines in the Pylon |
| TASK 36-11-49-400-820-A | Installation of the Pneumatic Sense Lines in the Pylon |
| TASK 36-11-54-000-001-A | Removal of the Fan Air Valve |
| TASK 36-11-54-400-001-A | Installation of the Fan Air Valve |
| TASK 71-13-00-010-010-A | Opening of the Fan Cowls 437AL(447AL),438AR(448AR) |
| TASK 71-13-00-010-040-A | Opening of the Fan Cowl Doors |
| TASK 71-13-00-010-040-B | Opening of the Fan Cowl Doors |
| TASK 71-13-00-410-010-A | Closing of the Fan Cowls 437AL(447AL),438AR(448AR) |
| TASK 71-13-00-410-040-A | Closing of the Fan Cowl Doors |
| TASK 71-13-00-410-040-B | Closing of the Fan Cowl Doors |
| TASK 78-30-00-040-012-A | Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance |
| TASK 78-30-00-081-041-A | Make the Thrust Reverser Serviceable after Maintenance |
| TASK 78-30-00-081-041-B | Make the Thrust Reverser Serviceable after Maintenance |
| TASK 78-30-00-440-012-A | Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after Ground Maintenance |
| TASK 78-30-00-481-041-A | Make the Thrust Reverser Unserviceable for Maintenance |
| TASK 78-30-00-481-041-B | Make the Thrust Reverser Unserviceable for Maintenance |
| TASK 78-32-00-010-010-A | Opening of the Thrust Reverser Halves |
| TASK 78-32-00-410-010-A | Closing of the Thrust Reverser Halves |
| TASK 78-36-00-010-040-A | Opening of the Thrust Reverser Doors |
| TASK 78-36-00-010-040-B | Opening of the Thrust Reverser Doors |
| TASK 78-36-00-410-040-A | Closing of the Thrust Reverser Doors |
| TASK 78-36-00-410-040-B | Closing of the Thrust Reverser Doors |
 Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL | |
| Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL | |
Subtask 36-11-00-861-137-A ** ON A/C NOT FOR ALL Subtask 36-11-00-941-139-A ** ON A/C NOT FOR ALL
B. Safety Precautions
(1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(2) On the AIR COND panel 30VU:
Subtask 36-11-00-010-169-A ** ON A/C NOT FOR ALL (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(2) On the AIR COND panel 30VU:
- Make sure that the ENG 1(2) BLEED pushbutton switch is pushed (the OFF legend is off).
- Make sure that the APU BLEED pushbutton switch is released (the ON legend is off).
- Put a WARNING NOTICE(S) in position to tell persons not to operate the pneumatic system.
- Put a WARNING NOTICE(S) in position to tell persons not to start the engine 1(2).
- Put a WARNING NOTICE(S) in position to tell persons not to pressurize the pneumatic system.
- Make sure that the ON legend of the ENG/FADEC GND PWR 1(2) pushbutton switch is off.
- Put a WARNING NOTICE(S) in position to tell persons not to energize the FADEC 1(2).
C. Get Access
(1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Open the access door 191MB.
(3) Put the ACCESS PLATFORM 1M(3 FT) in position below the engine.
Subtask 36-11-00-040-113-A ** ON A/C NOT FOR ALL (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Open the access door 191MB.
(3) Put the ACCESS PLATFORM 1M(3 FT) in position below the engine.
D. Deactivation of the Thrust Reverser
Subtask 36-11-00-010-170-A ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE THRUST REVERSER HYDRAULIC CONTROL UNIT (HCU) IS DEACTIVATED BEFORE YOU DO WORK ON OR AROUND THE THRUST REVERSER. IF THE HCU IS NOT DEACTIVATED, THERE IS A RISK OF UNWANTED THRUST REVERSER OPERATION WHICH CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Make the thrust reverser unserviceable for maintenance (Ref. AMM TASK 78-30-00-481-041). E. Open the thrust reverser doors (Ref. AMM TASK 78-36-00-010-040):
(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 36-11-00-010-169-B ** ON A/C NOT FOR ALL (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
F. Get Access
(1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Open the access door 191MB.
(3) Put the ACCESS PLATFORM 1M(3 FT) in position below the engine.
Subtask 36-11-00-040-113-B ** ON A/C NOT FOR ALL (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Open the access door 191MB.
(3) Put the ACCESS PLATFORM 1M(3 FT) in position below the engine.
G. Deactivation of the Thrust Reverser
Subtask 36-11-00-010-170-B ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE THRUST REVERSER HYDRAULIC CONTROL UNIT (HCU) IS DEACTIVATED BEFORE YOU DO WORK ON OR AROUND THE THRUST REVERSER. IF THE HCU IS NOT DEACTIVATED, THERE IS A RISK OF UNWANTED THRUST REVERSER OPERATION WHICH CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Do the deactivation of the thrust reverser system for maintenance (Ref. AMM TASK 78-30-00-040-012). H. Open the thrust reverser halves (Ref. AMM TASK 78-32-00-010-010):
(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 36-11-00-010-169-C ** ON A/C NOT FOR ALL (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
I. Get Access
(1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Open the access door 191MB.
(3) Put the ACCESS PLATFORM 1M(3 FT) in position below the engine.
Subtask 36-11-00-040-113-C ** ON A/C NOT FOR ALL (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Open the access door 191MB.
(3) Put the ACCESS PLATFORM 1M(3 FT) in position below the engine.
J. Deactivation of the Thrust Reverser
Subtask 36-11-00-010-170-C ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE THRUST REVERSER HYDRAULIC CONTROL UNIT (HCU) IS DEACTIVATED BEFORE YOU DO WORK ON OR AROUND THE THRUST REVERSER. IF THE HCU IS NOT DEACTIVATED, THERE IS A RISK OF UNWANTED THRUST REVERSER OPERATION WHICH CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Make the thrust reverser unserviceable for maintenance (Ref. AMM TASK 78-30-00-481-041). K. Open the thrust reverser doors (Ref. AMM TASK 78-36-00-010-040):
(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 36-11-00-480-106-A ** ON A/C NOT FOR ALL (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
L. Preparation for installation
(1) Do a visual inspection of the FAV to find the position of the following features in the FAV actuator: sense line connection, test port and deactivation screw.
(a) For FAV standard 6730A and 6730B
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL
Subtask 36-11-00-480-109-A ** ON A/C NOT FOR ALL (1) Do a visual inspection of the FAV to find the position of the following features in the FAV actuator: sense line connection, test port and deactivation screw.
(a) For FAV standard 6730A and 6730B
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL - The test port is near the border of the FAV actuator.
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL - The test port is near the center of the FAV actuator.
Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL Sense Line Connected between the FAV Control-Thermostat and the FAV - Location ** ON A/C NOT FOR ALL - The test port is near the center of the FAV actuator.
M. Installation of the Tool (Fan Air Valve with the Orange Deactivation Screw).
Connection of the Fan Air Valve (Orange Deactivation Screw) with the Bleed Test Set 98L36103002000 and Sense Line Tester-Kit SBE2213 ** ON A/C NOT FOR ALL
(1) Close the shutoff valve, the purge valve and the pressure regulator valve on the 98L36103002000 TEST SET - ENGINE BLEED (Z01).
(2) Connect the AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to the 98L36103002000 TEST SET - ENGINE BLEED (Z01).
(4) Connect the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY 2 to the valve 2 port of the sense line tester (T01) with the adaptor (T04).
(5) TORQUE the adaptor (T04) to between 1.1 and 0.9 m.daN (97.35 and 79.65 lbf.in ).
(6) Removal of the deactivation screw lockwire:
(7) Remove the deactivation screw.
(c) Make sure the valve 1 and valve 2 are in the open position (valves aligned with the pneumatic ducts).
(9) Do a reset of GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY gages 1 and 2.
Subtask 36-11-00-480-110-A ** ON A/C NOT FOR ALL Connection of the Fan Air Valve (Orange Deactivation Screw) with the Bleed Test Set 98L36103002000 and Sense Line Tester-Kit SBE2213 ** ON A/C NOT FOR ALL (2) Connect the AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to the 98L36103002000 TEST SET - ENGINE BLEED (Z01).
NOTE: If the AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY has an own regulator valve it is not necessary to install the primary regulator valve supplied with the 98L36103002000 TEST SET - ENGINE BLEED (Z01).
(3) Connect the 98L36103002000 TEST SET - ENGINE BLEED (Z01) to the SBE2213 KIT TOOL-TESTER SENSE LINE (Z02). (4) Connect the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY 2 to the valve 2 port of the sense line tester (T01) with the adaptor (T04).
(5) TORQUE the adaptor (T04) to between 1.1 and 0.9 m.daN (97.35 and 79.65 lbf.in )
. (6) Removal of the deactivation screw lockwire:
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(a) Cut and discard the lockwire of the deactivation screw of the fan air valve. (7) Remove the deactivation screw.
NOTE: Use a WRENCH 5/16 IN (8MM) - SPANNER if necessary.
(8) Connection of the sense line tester (T01) to the fan air valve: CAUTION:
FIRST TRY TO INSTALL THE ADAPTOR WITH THE SHORTEST THREADED AREA (T02). IF YOU CANNOT INSTALL IT, INSTALL THE OTHER ADAPTOR (T03). MAKE SURE THAT THE ADAPTOR (T02 OR T03) IS CORRECTLY HAND TIGHTENED.
(a) Connect the sense line tester (T01) to the deactivation screw port with the adaptor (T02) or (T03). CAUTION:
MAKE SURE THAT THE ADAPTOR (T02 OR T03) IS CORRECTLY HAND TIGHTENED.
(b) Apply force when you tighten the adaptor (T02) or (T03) with your hand. (c) Make sure the valve 1 and valve 2 are in the open position (valves aligned with the pneumatic ducts).
(9) Do a reset of GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY gages 1 and 2.
NOTE: The pressure value shown on the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY must be equal to 0 psi (0.0000 bar).
(10) Make sure that the regulator valve of the test set is closed before pressurize the system. N. Installation of the Tool (Fan Air Valve with the Hexagonal Deactivation Screw).
Connection of the Fan Air Valve (Deactivation Screw with Hexagonal Head) with the Bleed Test Set 98L36103002000 and Sense Line Tester-Kit SBE2213 ** ON A/C NOT FOR ALL
(1) Close the shutoff valve, the purge valve and the pressure regulator valve on the 98L36103002000 TEST SET - ENGINE BLEED (Z01).
(2) Connect the AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to the 98L36103002000 TEST SET - ENGINE BLEED (Z01).
(3) Connect the 98L36103002000 TEST SET - ENGINE BLEED (Z01) to the SBE2213 KIT TOOL-TESTER SENSE LINE (Z02).
(4) Connect the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY 2 to the valve 2 port of the sense line tester (T01) with the adaptor (T04).
(5) TORQUE the adaptor (T04) to between 1.1 and 0.9 m.daN (97.35 and 79.65 lbf.in ).
(6) Removal of the deactivation screw lockwire:
(7) Remove the deactivation screw.
(c) Make sure the valve 1 and valve 2 are in the open position (valves aligned with the pneumatic ducts).
(9) Do a reset of GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY gages 1 and 2.
4. Procedure Connection of the Fan Air Valve (Deactivation Screw with Hexagonal Head) with the Bleed Test Set 98L36103002000 and Sense Line Tester-Kit SBE2213 ** ON A/C NOT FOR ALL (2) Connect the AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to the 98L36103002000 TEST SET - ENGINE BLEED (Z01).
(3) Connect the 98L36103002000 TEST SET - ENGINE BLEED (Z01) to the SBE2213 KIT TOOL-TESTER SENSE LINE (Z02).
(4) Connect the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY 2 to the valve 2 port of the sense line tester (T01) with the adaptor (T04).
(5) TORQUE the adaptor (T04) to between 1.1 and 0.9 m.daN (97.35 and 79.65 lbf.in )
. (6) Removal of the deactivation screw lockwire:
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(a) Cut and discard the lockwire of the deactivation screw of the fan air valve. (7) Remove the deactivation screw.
NOTE: Use a WRENCH 5/16 IN (8MM) - SPANNER if necessary.
(8) Connection of the sense line tester (T01) to the fan air valve: CAUTION:
FIRST TRY TO INSTALL THE ADAPTOR WITH THE SHORTEST THREADED AREA (T02). IF YOU CANNOT INSTALL IT, INSTALL THE OTHER ADAPTOR (T03). MAKE SURE THAT THE ADAPTOR (T02 OR T03) IS CORRECTLY HAND TIGHTENED.
(a) Connect the sense line tester (T01) to the deactivation screw port with the adaptor (T02) or (T03). CAUTION:
MAKE SURE THAT THE ADAPTOR (T02 OR T03) IS CORRECTLY HAND TIGHTENED.
(b) Apply force when you tighten the adaptor (T02) or (T03) with your hand. (c) Make sure the valve 1 and valve 2 are in the open position (valves aligned with the pneumatic ducts).
(9) Do a reset of GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY gages 1 and 2.
NOTE: The pressure value shown on the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY must be equal to 0 psi (0.0000 bar).
(10) Make sure that the regulator valve of the test set is closed before pressurize the system. Subtask 36-11-00-720-093-B ** ON A/C NOT FOR ALL
A. Health Check Test of the Temperature Control Function
(1) Do the minimum opening pressure-test of the FAV with the Bleed Test Set PN 98l36103002000 and the Sense Line Tester SBE2213:
(a) Pressurize the 98L36103002000 TEST SET - ENGINE BLEED:
1 Use the primary regulator valve on the 98L36103002000 TEST SET - ENGINE BLEED (Z01) or AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to pressurize the test set to 30 psi (2.0684 bar).
(b) If the minimum opening pressure-test of the FAV is OK:
1 Do the steps given in the Close-up paragraph.
(c) If the minimum opening pressure-test of the FAV is not OK:
1 Do the functional test of the sense line connected between the FAV control thermostat and the FAV with 98L36103002000 TEST SET - ENGINE BLEED and SBE2213 KIT TOOL-TESTER SENSE LINE (Ref. AMM TASK 36-11-00-720-012).
a If there is no leak:
Subtask 36-11-00-720-093-D ** ON A/C NOT FOR ALL (1) Do the minimum opening pressure-test of the FAV with the Bleed Test Set PN 98l36103002000 and the Sense Line Tester SBE2213:
(a) Pressurize the 98L36103002000 TEST SET - ENGINE BLEED:
1 Use the primary regulator valve on the 98L36103002000 TEST SET - ENGINE BLEED (Z01) or AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to pressurize the test set to 30 psi (2.0684 bar).
| ACTION | RESULT |
|---|---|
1.On the sense line tester (T01):
| On the sense line tester (T01):
|
2.On the test set (Z01):
NOTE: Read the pressure on the digital pressure gage. | On the FAV:
NOTE: Read the pressure on the digital pressure gage. |
3.On the test set (Z01):
| On the FAV:
|
(b) If the minimum opening pressure-test of the FAV is OK:
1 Do the steps given in the Close-up paragraph.
(c) If the minimum opening pressure-test of the FAV is not OK:
1 Do the functional test of the sense line connected between the FAV control thermostat and the FAV with 98L36103002000 TEST SET - ENGINE BLEED and SBE2213 KIT TOOL-TESTER SENSE LINE (Ref. AMM TASK 36-11-00-720-012).
a If there is no leak:
- Replace the FAV (Ref. AMM TASK 36-11-54-000-001) and (Ref. AMM TASK 36-11-54-400-001).
- Do the minimum opening pressure-test of the FAV.
- Do the steps given in the Close-up paragraph.
- Do a check of the unions and clamps of the sense line between the FAV control thermostat and the FAV.
* If the unions are loose:
** TORQUE the unions to between 2.5 and 0.8 m.daN (221.24 and 70.80 lbf.in ).
* If the unions are correctly tightened:
** Replace the pneumatic sense line connected between the FAV control thermostat and the FAV (Ref. AMM TASK 36-11-49-000-029) and (Ref. AMM TASK 36-11-49-400-029). - Do the minimum opening pressure-test of the FAV.
* If the test of the FAV is OK:
** Do the steps given in the Close-up paragraph.
* If the test of the FAV is not OK:
** Replace the FAV control thermostat (Ref. AMM TASK 36-11-43-000-001) and (Ref. AMM TASK 36-11-43-400-001).
** Do the minimum opening pressure-test of the FAV.
A. Health Check Test of the Temperature Control Function
(1) Do the minimum opening pressure-test of the FAV with the Bleed Test Set PN 98l36103002000 and the Sense Line Tester SBE2213:
(a) Pressurize the 98L36103002000 TEST SET - ENGINE BLEED:
1 Use the primary regulator valve on the 98L36103002000 TEST SET - ENGINE BLEED (Z01) or AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to pressurize the test set to 30 psi (2.0684 bar).
(b) If the minimum opening pressure-test of the FAV is OK:
1 Do the steps given in the Close-up paragraph.
(c) If the minimum opening pressure-test of the FAV is not OK:
1 Do the functional test of the sense line connected between the FAV control thermostat and the FAV with 98L36103002000 TEST SET - ENGINE BLEED and SBE2213 KIT TOOL-TESTER SENSE LINE (Ref. AMM TASK 36-11-00-720-012).
a If there is no leak:
Subtask 36-11-00-720-093-E ** ON A/C NOT FOR ALL (1) Do the minimum opening pressure-test of the FAV with the Bleed Test Set PN 98l36103002000 and the Sense Line Tester SBE2213:
(a) Pressurize the 98L36103002000 TEST SET - ENGINE BLEED:
1 Use the primary regulator valve on the 98L36103002000 TEST SET - ENGINE BLEED (Z01) or AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to pressurize the test set to 30 psi (2.0684 bar).
| ACTION | RESULT |
|---|---|
1.On the sense line tester (T01):
| On the sense line tester (T01):
|
2.On the test set (Z01):
NOTE: Read the pressure on the digital pressure gage. | On the FAV:
NOTE: Read the pressure on the digital pressure gage. |
3.On the test set (Z01):
| On the FAV:
|
(b) If the minimum opening pressure-test of the FAV is OK:
1 Do the steps given in the Close-up paragraph.
(c) If the minimum opening pressure-test of the FAV is not OK:
1 Do the functional test of the sense line connected between the FAV control thermostat and the FAV with 98L36103002000 TEST SET - ENGINE BLEED and SBE2213 KIT TOOL-TESTER SENSE LINE (Ref. AMM TASK 36-11-00-720-012).
a If there is no leak:
- Replace the FAV (Ref. AMM TASK 36-11-54-000-001) and (Ref. AMM TASK 36-11-54-400-001).
- Do the minimum opening pressure-test of the FAV.
- Do the steps given in the Close-up paragraph.
- Do a check of the unions and clamps of the sense line between the FAV control thermostat and the FAV.
* If the unions are loose:
** TORQUE the unions to between 2.5 and 0.8 m.daN (221.24 and 70.80 lbf.in ).
* If the unions are correctly tightened:
** Replace the pneumatic sense line connected between the FAV control thermostat and the FAV (Ref. AMM TASK 36-11-49-000-820) and (Ref. AMM TASK 36-11-49-400-820). - Do the minimum opening pressure-test of the FAV.
* If the test of the FAV is OK:
** Do the steps given in the Close-up paragraph.
* If the test of the FAV is not OK:
** Replace the FAV control thermostat (Ref. AMM TASK 36-11-43-000-001) and (Ref. AMM TASK 36-11-43-400-001).
** Do the minimum opening pressure-test of the FAV.
A. Health Check Test of the Temperature Control Function
(1) Do the minimum opening pressure-test of the FAV with the Bleed Test Set PN 98l36103002000 and the Sense Line Tester SBE2213:
(a) Pressurize the 98L36103002000 TEST SET - ENGINE BLEED:
1 Use the primary regulator valve on the 98L36103002000 TEST SET - ENGINE BLEED (Z01) or AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to pressurize the test set to 30 psi (2.0684 bar).
(b) If the minimum opening pressure-test of the FAV is OK:
1 Do the steps given in the Close-up paragraph.
(c) If the minimum opening pressure-test of the FAV is not OK:
1 Do the functional test of the sense line connected between the FAV control thermostat and the FAV with 98L36103002000 TEST SET - ENGINE BLEED and SBE2213 KIT TOOL-TESTER SENSE LINE (Ref. AMM TASK 36-11-00-720-012).
a If there is no leak:
5. Close-up(1) Do the minimum opening pressure-test of the FAV with the Bleed Test Set PN 98l36103002000 and the Sense Line Tester SBE2213:
(a) Pressurize the 98L36103002000 TEST SET - ENGINE BLEED:
1 Use the primary regulator valve on the 98L36103002000 TEST SET - ENGINE BLEED (Z01) or AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) to pressurize the test set to 30 psi (2.0684 bar).
| ACTION | RESULT |
|---|---|
1.On the sense line tester (T01):
| On the sense line tester (T01):
|
2.On the test set (Z01):
NOTE: Read the pressure on the digital pressure gage. | On the FAV:
NOTE: Read the pressure on the digital pressure gage. |
3.On the test set (Z01):
| On the FAV:
|
(b) If the minimum opening pressure-test of the FAV is OK:
1 Do the steps given in the Close-up paragraph.
(c) If the minimum opening pressure-test of the FAV is not OK:
1 Do the functional test of the sense line connected between the FAV control thermostat and the FAV with 98L36103002000 TEST SET - ENGINE BLEED and SBE2213 KIT TOOL-TESTER SENSE LINE (Ref. AMM TASK 36-11-00-720-012).
a If there is no leak:
- Replace the FAV (Ref. AMM TASK 36-11-54-000-001) and (Ref. AMM TASK 36-11-54-400-001).
- Do the minimum opening pressure-test of the FAV.
- Do the steps given in the Close-up paragraph.
- Do a check of the unions and clamps of the sense line between the FAV control thermostat and the FAV.
* If the unions are loose:
** TORQUE the unions to between 2.5 and 0.8 m.daN (221.24 and 70.80 lbf.in ).
* If the unions are correctly tightened:
** Replace the pneumatic sense line connected between the FAV control thermostat and the FAV (Ref. AMM TASK 36-11-49-000-018) and (Ref. AMM TASK 36-11-49-400-018). - Do the minimum opening pressure-test of the FAV.
* If the test of the FAV is OK:
** Do the steps given in the Close-up paragraph.
* If the test of the FAV is not OK:
** Replace the FAV control thermostat (Ref. AMM TASK 36-11-43-000-001) and (Ref. AMM TASK 36-11-43-400-001).
** Do the minimum opening pressure-test of the FAV.
Subtask 36-11-00-080-096-A ** ON A/C NOT FOR ALL
A. Removal of the Tool (Fan Air Valve with the Orange Deactivation Screw)
Connection of the Fan Air Valve (Orange Deactivation Screw) with the Bleed Test Set 98L36103002000 and Sense Line Tester-Kit SBE2213 ** ON A/C NOT FOR ALL
(1) Disconnect the adaptor (T02) or (T03) from the fan air valve.
(2) Remove the SBE2213 KIT TOOL-TESTER SENSE LINE (Z02), 98L36103002000 TEST SET - ENGINE BLEED (Z01) and AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) from the engine.
(b) Install the deactivation screw on the fan air valve.
(c) TORQUE the deactivation screw to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in ).
14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
Subtask 36-11-00-080-097-A ** ON A/C NOT FOR ALL Connection of the Fan Air Valve (Orange Deactivation Screw) with the Bleed Test Set 98L36103002000 and Sense Line Tester-Kit SBE2213 ** ON A/C NOT FOR ALL (2) Remove the SBE2213 KIT TOOL-TESTER SENSE LINE (Z02), 98L36103002000 TEST SET - ENGINE BLEED (Z01) and AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) from the engine.
CAUTION:
WHEN YOU INSTALL THE DEACTIVATION SCREW ON THE VALVE, TIGHTEN THE SCREW WITH YOUR HAND BEFORE YOU TORQUE IT. IF YOU DO NOT OBEY THIS PRECAUTION, YOU CAN CAUSE DAMAGE TO THE SCREW AND THE VALVE.
CAUTION:
BEFORE YOU INSTALL THE DEACTIVATION SCREW, MAKE SURE THAT THE PREFORMED PACKING IS INSTALLED ON THE DEACTIVATION SCREW.
(3) Installation of the deactivation screw: NOTE: If the adaptor (T03) is installed, the deactivation screw is equipped with a preformed PACKING.
(a) Make sure you install a new preformed PACKING on the deactivation screw if you have removed the adaptor (T03). (b) Install the deactivation screw on the fan air valve.
(c) TORQUE the deactivation screw to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in )
. WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(d) Safety the deactivation screw on its support with lockwire B. Removal of the Tool (Fan Air Valve with the Hexagonal Head Deactivation Screw)
Connection of the Fan Air Valve (Deactivation Screw with Hexagonal Head) with the Bleed Test Set 98L36103002000 and Sense Line Tester-Kit SBE2213 ** ON A/C NOT FOR ALL
(1) Disconnect the adaptor (T02) or (T03) from the fan air valve.
(2) Remove the SBE2213 KIT TOOL-TESTER SENSE LINE (Z02), 98L36103002000 TEST SET - ENGINE BLEED (Z01) and AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) from the engine.
(b) Install the deactivation screw on the fan air valve.
(c) TORQUE the deactivation screw to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in ).
14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
Subtask 36-11-00-410-159-A ** ON A/C NOT FOR ALL Connection of the Fan Air Valve (Deactivation Screw with Hexagonal Head) with the Bleed Test Set 98L36103002000 and Sense Line Tester-Kit SBE2213 ** ON A/C NOT FOR ALL (2) Remove the SBE2213 KIT TOOL-TESTER SENSE LINE (Z02), 98L36103002000 TEST SET - ENGINE BLEED (Z01) and AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03) from the engine.
CAUTION:
WHEN YOU INSTALL THE DEACTIVATION SCREW ON THE VALVE, TIGHTEN THE SCREW WITH YOUR HAND BEFORE YOU TORQUE IT. IF YOU DO NOT OBEY THIS PRECAUTION, YOU CAN CAUSE DAMAGE TO THE SCREW AND THE VALVE.
CAUTION:
BEFORE YOU INSTALL THE DEACTIVATION SCREW, MAKE SURE THAT THE PREFORMED PACKING IS INSTALLED ON THE DEACTIVATION SCREW.
(3) Installation of the deactivation screw: NOTE: If the adaptor (T03) is installed, the deactivation screw is equipped with a preformed PACKING.
(a) Make sure you install a new preformed PACKING on the deactivation screw if you have removed the adaptor (T03). (b) Install the deactivation screw on the fan air valve.
(c) TORQUE the deactivation screw to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in )
. WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(d) Safety the deactivation screw on its support with lockwire C. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser doors (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 36-11-00-440-101-A ** ON A/C NOT FOR ALL Subtask 36-11-00-410-160-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser doors (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
E. Close Access
(1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Close the access door 191MB.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
Subtask 36-11-00-410-159-B ** ON A/C NOT FOR ALL (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Close the access door 191MB.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
F. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser halves (Ref. AMM TASK 78-32-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 36-11-00-440-101-B ** ON A/C NOT FOR ALL Subtask 36-11-00-410-160-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser halves (Ref. AMM TASK 78-32-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
H. Close Access
(1) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Close the access door 191MB.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
Subtask 36-11-00-410-159-C ** ON A/C NOT FOR ALL (1) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Close the access door 191MB.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
I. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser doors (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 36-11-00-440-101-C ** ON A/C NOT FOR ALL Subtask 36-11-00-410-160-C ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the thrust reverser doors (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
K. Close Access
(1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Close the access door 191MB.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
Subtask 36-11-00-862-121-A ** ON A/C NOT FOR ALL (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Close the access door 191MB.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).