Reactivation of the HP Bleed Valve to Make serviceable the IP Bleed Check-Valve

TASK 36-11-00-440-002-A
Reactivation of the HP Bleed Valve to Make serviceable the IP Bleed Check-Valve

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: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL
FIN: 4000HA ** ON A/C NOT FOR ALL
FIN: 7110HM ** ON A/C NOT FOR ALL

1. Reason for the Job
MMEL 36-11-06B
ENGINE BLEED IP CHECK VALVE
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 0.6 and 0.5 m.daN (53.10 and 44.25 lbf.in )
No specific	Torque wrench: range to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in )

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.14QEB1)	Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -

C. Work Zones and Access Panels

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

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
2	PACKING	AIPC 36-11-51-01-130
3	PACKING	AIPC 36-11-51-01-150

E. 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
HP Bleed Valve P/N 6773B02 ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6773B02 ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6713D01-07 ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6713D01-07 ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6773B03 ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6773B03 ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6713D08 ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6713D08 ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6773E ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6773E ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6773F and 6773G ** ON A/C NOT FOR ALL
HP Bleed Valve P/N 6773F and 6773G ** ON A/C NOT FOR ALL

3. Job Set-up
Subtask 36-11-00-861-069-A ** ON A/C NOT FOR ALL

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

Subtask 36-11-00-941-066-A ** ON A/C NOT FOR ALL

B. Safety Precautions
(1) Make sure that the engine 1(2) is shut down occurred not less than 5 minutes.
(2) On the AIR COND panel 30VU:

make sure that the ENG 1(2) BLEED pushbutton switch is released (the OFF legend is on)
make sure that the APU BLEED pushbutton switch is released (the ON legend is off)
put a WARNING NOTICE(S) to tell persons not to operate the pneumatic system.

(3) On the ENG panel 115VU:

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

(4) On the HP ground connector:

put a WARNING NOTICE(S) to tell persons not to pressurize the pneumatic system.

(5) On 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) to tell persons not to energize the FADEC 1(2).

Subtask 36-11-00-865-069-A ** ON A/C NOT FOR ALL

C. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	AIR BLEED/ENG 1/CTL	3HA1	D12
49VU	AIR BLEED/ENG 1/MONG	2HA1	D11
122VU	AIR BLEED/ENG 2/CTL	3HA2	Z23
122VU	AIR BLEED/ENG 2/MONG	2HA2	Z22

Subtask 36-11-00-010-055-A ** ON A/C NOT FOR ALL

D. 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) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position below the engine.

Subtask 36-11-00-040-053-A ** ON A/C NOT FOR ALL

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

Subtask 36-11-00-010-074-A ** ON A/C NOT FOR ALL

F. Open the left thrust-reverser cowl door (Ref. AMM TASK 78-36-00-010-040):
(1) FOR [1000EM1] (ENGINE-1)
451AL
(2) FOR [1000EM2] (ENGINE-2)
461AL

Subtask 36-11-00-010-055-B ** ON A/C NOT FOR ALL

G. 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) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in to position below the engine.

Subtask 36-11-00-040-053-B ** ON A/C NOT FOR ALL

H. Deactivate 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) Deactivate the thrust reverser Hydraulic Control Unit (HCU) (Ref. AMM TASK 78-30-00-040-012).

Subtask 36-11-00-010-074-B ** ON A/C NOT FOR ALL

I. 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 36-11-00-010-055-C ** ON A/C NOT FOR ALL

J. 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) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position below the engine.

Subtask 36-11-00-040-053-C ** ON A/C NOT FOR ALL

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

Subtask 36-11-00-010-074-C ** ON A/C NOT FOR ALL

L. Open the left thrust-reverser cowl door (Ref. AMM TASK 78-36-00-010-040):
(1) FOR [1000EM1] (ENGINE-1)
451AL
(2) FOR [1000EM2] (ENGINE-2)
461AL.

4. Procedure
Subtask 36-11-00-440-058-A ** ON A/C NOT FOR ALL

A. Reactivation of the HP Bleed Valve
(1) On the HP bleed valve P/N 6773B02 and P/N 6713D01 to P/N 6713D07:

HP Bleed Valve P/N 6773B02 ** ON A/C NOT FOR ALL

HP Bleed Valve P/N 6713D01-07 ** ON A/C NOT FOR ALL

(a) Remove the knurled screw (1) from the override control to unlock the valve.
(b) Install the knurled screw (1) with the washer (2) in the storage port.
(c) Tighten the knurled screw (1) with your hand.
(d) Installation of the 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.

1 Safety the knurled screw (1) with 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.
(2) On the HP bleed valve P/N 6773B03 and P/N 6713D08:

HP Bleed Valve P/N 6773B03 ** ON A/C NOT FOR ALL

HP Bleed Valve P/N 6713D08 ** ON A/C NOT FOR ALL

(a) Remove the safety screw (1) from the override control to unlock the valve.
(b) Install the safety screw (1) with the washer (2) in the storage port.
(c) TORQUE the safety screw (1) to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in )

.
(d) Installation of the lockwire:

1 Safety the safety screw (1) with 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.
(3) On the HP bleed valve P/N 6773E:

HP Bleed Valve P/N 6773E ** ON A/C NOT FOR ALL

CAUTION: MAKE SURE THAT THE PACKING IS IN POSITION WHEN YOU INSTALL THE LOCKING PIN ON ITS SUPPORT. THIS WILL PREVENT VENTING OF THE VALVE REGULATOR.

(a) Remove the special screw (1) from the override control to unlock the valve.
(b) Install a new AIPC 36-11-51-01-150 PACKING (3).
(c) Install the special screw (1) with the washer (2) in the storage port.
(d) Tighten the special screw (1) with your hand.
(e) Installation of the lockwire:

1 Safety the special screw (1) with 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.
(4) On the HP bleed valve P/N 6773F and P/N 6774G:

HP Bleed Valve P/N 6773F and 6773G ** ON A/C NOT FOR ALL

CAUTION: MAKE SURE THAT THE PACKING IS IN POSITION WHEN YOU INSTALL THE LOCKING PIN ON ITS SUPPORT. THIS WILL PREVENT VENTING OF THE VALVE REGULATOR.

(a) Remove the safety screw (1) from the override control to unlock the valve.
(b) Install a new AIPC 36-11-51-01-130 PACKING (2).
(c) Install the safety screw (1) in the storage port.
(d) TORQUE the safety screw (1) to between 0.6 and 0.5 m.daN (53.10 and 44.25 lbf.in )

.
(e) Installation of the lockwire:

1 Safety the safety screw (1) with 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.

5. Close-up
Subtask 36-11-00-410-055-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 left thrust-reverser cowl door (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL
(b) FOR [1000EM2] (ENGINE-2)
461AL

Subtask 36-11-00-440-054-A ** ON A/C NOT FOR ALL

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

Subtask 36-11-00-410-074-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) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).

Subtask 36-11-00-410-055-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 36-11-00-440-054-B ** ON A/C NOT FOR ALL

E. Activate the thrust reverser HCU (Ref. AMM TASK 78-30-00-440-012).

Subtask 36-11-00-410-074-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) Remove the WARNING NOTICE(S).
(3) Remove the access platform(s).

Subtask 36-11-00-410-055-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 left thrust-reverser cowl door (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL
(b) FOR [1000EM2] (ENGINE-2)
461AL.

Subtask 36-11-00-440-054-C ** ON A/C NOT FOR ALL

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

Subtask 36-11-00-410-074-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) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).

Subtask 36-11-00-865-070-A ** ON A/C NOT FOR ALL

J. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	AIR BLEED/ENG 1/CTL	3HA1	D12
49VU	AIR BLEED/ENG 1/MONG	2HA1	D11
122VU	AIR BLEED/ENG 2/CTL	3HA2	Z23
122VU	AIR BLEED/ENG 2/MONG	2HA2	Z22

Subtask 36-11-00-869-114-A ** ON A/C NOT FOR ALL

K. On the AIR COND panel 30VU:

push the ENG 1(2) BLEED pushbutton switch (the OFF legend is off).

Subtask 36-11-00-862-069-A ** ON A/C NOT FOR ALL

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

[Rev.10 from 2021] 2026.04.01 01:06:22 UTC