Functional Test of the Sense Line between the Pressure Regulator Valve (PRV) and the PRV Control Solenoid with the 98L36103002000 and SBE2213

TASK 36-11-00-720-010-A-01
Functional Test of the Sense Line between the Pressure Regulator Valve (PRV) and the PRV Control Solenoid with the 98L36103002000 and SBE2213

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.

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

FIN: 10HA1 ** ON A/C NOT FOR ALL
FIN: 10HA2 ** ON A/C NOT FOR ALL
FIN: 4001HA ** ON A/C NOT FOR ALL

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	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 145 and 135 lbf.in (1.64 and 1.53 m.daN )
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 1.1 and 0.9 m.daN (97.35 and 79.65 lbf.in )
98L36103002000	1	TEST SET - ENGINE BLEED
SBE2213	2	KIT TOOL-TESTER SENSE LINE

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.14QFB1)	Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
191MB
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR

D. Referenced Information

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 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
Connection of the Bleed-Pressure Regulator Valve (with Deactivation Screw on Regulator) with the Test Set 98L36103002000 and Tester Kit SBE2213
Connection of the Bleed-Pressure Regulator Valve (without Deactivation Screw on Regulator) with the Test Set 98L36103002000 and Tester Kit SBE2213

3. Job Set-up
Subtask 36-11-00-861-102-A ** ON A/C NOT FOR ALL

A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).

Subtask 36-11-00-941-106-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:

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.

(3) On the ENG panel 115VU:

Put a WARNING NOTICE(S) in position to tell persons not to start the engine 1(2).

(4) On the HP ground connector:

Put a WARNING NOTICE(S) in position to tell persons not to pressurize the pneumatic system.

(5) On the ENG section of the maintenance panel 50VU:

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).

Subtask 36-11-00-010-106-A ** ON A/C NOT FOR ALL

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 36-11-00-040-073-A ** ON A/C NOT FOR ALL

D. Deactivation of the Thrust Reverser

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).

Subtask 36-11-00-010-107-A ** ON A/C NOT FOR ALL

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 36-11-00-010-106-B ** ON A/C NOT FOR ALL

F. Get Access
(1) Open the fan cowls (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 36-11-00-040-073-B ** ON A/C NOT FOR ALL

G. Deactivation of the Thrust Reverser

(1) Do the deactivation of the Thrust-Reverser Hydraulic Control-Unit (HCU) (Ref. AMM TASK 78-30-00-040-012).

Subtask 36-11-00-010-107-B ** ON A/C NOT FOR ALL

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 36-11-00-010-106-C ** ON A/C NOT FOR ALL

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 36-11-00-040-073-C ** ON A/C NOT FOR ALL

J. Deactivation of the Thrust Reverser

(1) Make the thrust reverser unserviceable for maintenance (Ref. AMM TASK 78-30-00-481-041).

Subtask 36-11-00-010-107-C ** ON A/C NOT FOR ALL

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.

4. Procedure
Subtask 36-11-00-480-063-A ** ON A/C NOT FOR ALL

A. Installation of the Tool (Bleed-Pressure Regulator Valve with the Deactivation Screw on the Regulator)

Connection of the Bleed-Pressure Regulator Valve (with Deactivation Screw on Regulator) with the Test Set 98L36103002000 and 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) Connection of the test set.

WARNING: MAKE SURE THAT THE PRESSURE SUPPLIED TO BLEED TEST SET 98L36103002000 NEVER EXCEEDS 217 PSI (15 BAR). IF THE PRESSURE SUPPLIED TO THE BLEED TEST SET EXCEEDS THIS VALUE, THERE IS A RISK OF INJURY TO PERSONNEL AND DAMAGE TO EQUIPMENT. IF THE AIR CYLINDER DOES NOT HAVE A MANOMETER INSTALLED, YOU MUST INSTALL THE PRIMARY REGULATOR VALVE BETWEEN THE AIR BOTTLE AND BLEED TEST SET 98L36103002000. THE PRIMARY REGULATOR VALVE WILL LIMIT THE PRESSURE IN THE BLEED TEST SET TO 217 PSI (15 BAR).

CAUTION: BE CAREFUL WHEN YOU CONNECT/DISCONNECT THE TEST SET TO/FROM THE EQUIPMENT. THE PRESSURE REGULATING VALVE AND THE PRESSURE GAGE ASSEMBLY OF THE TEST SET ARE HEAVY AND CAN CAUSE DAMAGE TO THE ENGINE.

(a) 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 bleed-pressure regulator 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 bleed-pressure regulator 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 bleed-pressure regulator valve 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 gauges 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 36-11-00-480-064-A ** ON A/C NOT FOR ALL

B. Installation of the Tool (PRV without the Deactivation Screw on the Regulator)

Connection of the Bleed-Pressure Regulator Valve (without Deactivation Screw on Regulator) with the Test Set 98L36103002000 and Tester Kit SBE2213 ** ON A/C NOT FOR ALL

(1) Close the shutoff valve, the purge valve and the PRV 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 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) Disconnect the sense line (connected between the HPV (4000HA) and the PRV (4001HA)) from the PRV.
(7) Connect the sense line tester (T01) to the PRV as follows:
(a) Connect the sense line tester (T01) to the PRV with the adaptor (T07) and hose (T06).
(b) TORQUE the union of the adaptor (T07) to between 1.1 and 0.9 m.daN (97.35 and 79.65 lbf.in )

.
(8) Make sure that valve 1 and valve 2 are in the open position (the valves are aligned with the pneumatic ducts).
(9) Do a reset of all the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY:
(a) 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 you pressurize the system.

Subtask 36-11-00-720-066-A ** ON A/C NOT FOR ALL

CAUTION: DO NOT APPLY A PRESSURE OF MORE THAN 145 PSI (10 BAR). A HIGHER PRESSURE WILL CAUSE DAMAGE TO THE SENSE LINE.

C. Test

ACTION	RESULT
1.Pressurize the test set: If there is a manometer on the air cylinder then installation of the primary regulator valve is not necessary. Use the air cylinder shut off valve and the manometer to slowly pressurize the test set to 100 psi (6.8948 bar). If there is no manometer in the air cylinder then installation of primary regulator valve is mandatory. In this case the primary regulator valve will limit the pressure in the test set to 217 psi (14.9616 bar).
2.On the test set (Z01): Open the shutoff valve.
3.On the test set (Z01): Use the pressure regulator valve of the test set increase the pressure to 21.75 +0.75 psi or -0.75 psi (1.4996 +0.0517 bar or -0.0517 bar).	On the test set (Z01): The pressure value shows on the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY 1.
4.On the sense line tester (T01): Close the valve 1.	On the sense line tester (T01): The valve 1 is not aligned with the pneumatic duct.
5.On the sense line tester (T01): Do a check of the pressure value shown on the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY 2.	On the GAGE - ABSOLUTE PRESSURE, DIGITAL, 0.001 BAR ACCURACY 2: The pressure is more or equal to 9.6 psi (0.6619 bar).
6.On the AIR SOURCE 6.9 BAR (100 PSI) - REGULATED,FILTERED, DRY (Z03): Close the shutoff valve.
7.On the test set (Z01): Slowly open the purge valve to depressurize the test set.

Subtask 36-11-00-080-061-A ** ON A/C NOT FOR ALL

D. Removal of the Tool (Bleed-Pressure Regulator Valve with the Deactivation Screw on the Regulator)

Connection of the Bleed-Pressure Regulator Valve (with Deactivation Screw on Regulator) with the Test Set 98L36103002000 and Tester Kit SBE2213 ** ON A/C NOT FOR ALL

WARNING: BEFORE YOU START TO REMOVE THE TOOLING, MAKE SURE THAT THERE IS NO PRESSURIZED GAS LEFT INSIDE THE DUCTS. IT CAN CAUSE AN INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT.

(1) Make sure that the duct is not pressurized before removal of the tool.
(2) Disconnect the adaptor (T02) or (T03) from the bleed-pressure regulator valve.
(3) 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.

(4) 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 bleed-pressure regulator valve.
(c) TORQUE the deactivation screw to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in )

(d) Safety the deactivation screw on its support with lockwire 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.

Subtask 36-11-00-080-062-A ** ON A/C NOT FOR ALL

E. Removal of the Tool (PRV without the Deactivation Screw on the Regulator)

Connection of the Bleed-Pressure Regulator Valve (without Deactivation Screw on Regulator) with the Test Set 98L36103002000 and Tester Kit SBE2213 ** ON A/C NOT FOR ALL

WARNING: BEFORE YOU START TO REMOVE THE TOOLING, MAKE SURE THAT THERE IS NO PRESSURIZED GAS LEFT INSIDE THE DUCTS. IT CAN CAUSE AN INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT.

(1) Make sure that the duct is not pressurized before you remove the tool.
(2) Disconnect the adaptor (T07), adaptor (T04), hose (T06), 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 PRV.
(3) Connect the sense line to the PRV.
(4) TORQUE the union of the sense line to between 145 and 135 lbf.in (1.64 and 1.53 m.daN )

5. Close-up
Subtask 36-11-00-410-105-A ** ON A/C NOT FOR ALL

A. 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 36-11-00-440-073-A ** ON A/C NOT FOR ALL

B. Make the thrust reverser serviceable after maintenance (Ref. AMM TASK 78-30-00-081-041).

Subtask 36-11-00-410-106-A ** ON A/C NOT FOR ALL

C. 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 36-11-00-410-105-B ** ON A/C NOT FOR ALL

D. 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 36-11-00-440-073-B ** ON A/C NOT FOR ALL

E. Do the re-activation of the thrust reverser HCU (Ref. AMM TASK 78-30-00-440-012).

Subtask 36-11-00-410-106-B ** ON A/C NOT FOR ALL

F. 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 WARNING NOTICE(S).
(4) Remove the access platform(s).

Subtask 36-11-00-410-105-C ** ON A/C NOT FOR ALL

G. 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 36-11-00-440-073-C ** ON A/C NOT FOR ALL

H. Make the thrust reverser serviceable after maintenance (Ref. AMM TASK 78-30-00-081-041).

Subtask 36-11-00-410-106-C ** ON A/C NOT FOR ALL

I. 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 36-11-00-862-088-A ** ON A/C NOT FOR ALL

J. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.01 01:07:02 UTC