Adjustment Procedure to Install the Lock pin in the Regulator Valve Assembly of the Inflation Reservoir - Offwing Escape-Slide

TASK 25-62-00-820-001-A
Adjustment Procedure to Install the Lock pin in the Regulator Valve Assembly of the Inflation Reservoir - Offwing Escape-Slide

ZONE: 150
FIN: 7506MM ** ON A/C NOT FOR ALL
FIN: 7507MM ** ON A/C NOT FOR ALL
FIN: 7685MM ** ON A/C NOT FOR ALL
FIN: 7686MM ** 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 5M (16 FT)- ADJUSTABLE
No specific	AR	ALLEN KEY 3/16 IN
No specific	AR	SAFETY BARRIER(S)
No specific	AR	SHEET - PLASTIC
No specific	AR	WARNING NOTICE(S)
98D27803000000	1	LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
FOR [7507MM] (RESERVOIR ASSY OWS R)
No specific	1	ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific	1	MIRROR - INSPECTION, FLEXIBLE

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.13XCA4)	Laminate Repair Patch-Fire compliant - Cargo
(Material No.14JEA1)	Sealing Profile-Vaccum Bag Sealant - -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
150	AFT CARGO COMPARTMENT FWD PRESS BULKHEAD TO AFT BULKHEAD OF AFT CARGO COMPARTMENT

D. Referenced Information

REFERENCE	DESIGNATION
TASK 27-50-00-866-009-A	Retraction of the Flaps on the Ground
TASK 27-50-00-866-009-A-01	Retraction of the Flaps/Slats on the Ground
Inflation Reservoir - Adjustment Procedure to Install the Lock Pin Assembly ** ON A/C NOT FOR ALL
Inflation Reservoir ** ON A/C NOT FOR ALL
FOR [7507MM] (RESERVOIR ASSY OWS R)
TASK 52-30-00-860-001-A	Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
TASK 52-30-00-860-002-A	Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump

3. Job Set-up
Subtask 25-62-00-941-059-A ** ON A/C NOT FOR ALL

WARNING: MAKE SURE THAT THE LOCK PIN IS CORRECTLY INSTALLED IN THE REGULATOR VALVE ASSEMBLY OF THE INFLATION RESERVOIR. THIS SAFETIES ALL COMPONENTS OF THE INFLATION SYSTEM IN OPERATION AND PREVENTS ACCIDENTAL:

DISCHARGE OF THE INFLATION RESERVOIR
DEPLOYMENT OF THE ESCAPE SLIDE

WHICH CAN CAUSE INJURY AND/OR DAMAGE.

A. Safety Precautions and Wing Protection

NOTE: We recommended that only personnel who know the system do this procedure.

(1) Wing Protection Procedure:

CAUTION: MAKE SURE THAT THE PROTECTION IS IN POSITION ON THE UPPER SURFACE OF THE WING. DEPLOYMENT OF THE OFFWING ESCAPE-SLIDE CAN CAUSE DAMAGE TO THIS AREA.

(a) Do not use bubble wrap as protection for the aircraft wing.

NOTE: The protection is a lamination of fiberglass-reinforced polyester which has a minimum thickness of 1.2 mm (0.05 in.). It is thin, resistant to impact and applies the load equally to prevent damage to the wing.

(b) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position adjacent to the applicable wing.
(c) Attach the protection in position:

CAUTION: MAKE SURE THAT THE PROTECTION IS CORRECLTY ATTACHED WITH TAPE TO THE AIRCRAFT STRUCTURE. THIS PREVENTS THE SUCTION OF LOOSE MATERIAL INTO THE ASPIRATOR DURING DEPLOYMENT. LOOSE MATERIAL CAN CAUSE DAMAGE TO THE ASPIRATOR.

(d) Refer to the FIGURE for the approximate dimensions and position of the protection.
(e) Use Sealing Profile-Vaccum Bag Sealant - - (Material No.14JEA1) and attach Laminate Repair Patch-Fire compliant - Cargo (Material No.13XCA4) on to the upper surface of the wing.
(2) Ground safety procedure:

WARNING: PUT SAFETY BARRIERS IN POSITION TO KEEP THE TRAVEL RANGE OF THE ESCAPE-SLIDE CLEAR. IF YOU DO NOT, INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT CAN OCCUR.

(a) Below the related offwing escape-slide, make sure that an area with a radius of approximately 12.0 m (39.37 ft.) is clear of all miscellaneous equipment.
(b) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(c) Put SHEET - PLASTIC in position where the offwing escape-slide hits the ground.
(d) Put the WARNING NOTICE(S) in position to tell persons not to go into the area behind the safety barriers.
(3) Cockpit safety procedure:

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:

THE FLIGHT CONTROLS
THE FLIGHT CONTROL SURFACES
THE LANDING GEAR AND THE RELATED DOORS
COMPONENTS THAT MOVE.

MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.

(a) Set the slat/flap control lever to the 0 position (Ref. AMM TASK 27-50-00-866-009).
(b) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the slat/flap control lever when working near the slats/flaps.
(c) Put the WARNING NOTICE(S) on the slat/flap control lever to tell persons not to operate the flaps.

4. Procedure
Subtask 25-62-00-820-050-A ** ON A/C NOT FOR ALL

A. Adjustment Procedure

Inflation Reservoir - Adjustment Procedure to Install the Lock Pin Assembly ** ON A/C NOT FOR ALL

(1) FOR [7507MM] (RESERVOIR ASSY OWS R)

CAUTION: MAKE SURE THAT THE AFT CARGO-COMPARTMENT DOOR IS CLOSED BEFORE THE RIGHT OFFWING ESCAPE-SLIDE DEPLOYS. IF THE DOOR IS NOT CLOSED, YOU CAN CAUSE DAMAGE TO:

THE INFLATABLE ASSEMBLY
THE AFT CARGO-COMPARTMENT DOOR.

(a) Remove the access platform(s).
(b) Close the aft cargo-compartment door (Ref. AMM TASK 52-30-00-860-002).
(c) Use a MIRROR - INSPECTION, FLEXIBLE to let you see the pulley stop-pin (6) on the right-regulator valve assembly (5).
(2) Remove the lock pin (3) from the pocket (1).
(3) Do the adjustment procedure of the regulator valve assembly:

WARNING: MAKE SURE THAT YOU TURN THE REGULATOR ASSEMBLY IN A CLOCKWISE DIRECTION OR IN THE DIRECTION OF THE BLACK MARK. WHEN YOU TURN THE REGULATOR ASSEMBLY IN THIS DIRECTION, THE VALVE CLOSES. IF YOU DO NOT OBEY THIS INSTRUCTION, YOU WILL START AN UNWANTED DEPLOYMENT SEQUENCE. THIS CAN CAUSE INJURY TO PERSONNEL AND DAMAGE TO EQUIPMENT.

(a) Put an ALLEN KEY 3/16 IN (8) into the hexagonal socket (9).
(b) Turn the Allen key (8) in the SAFE direction, to move the pulley stop-pin (6) in the direction of the BLACK mark (7) (closed position).

NOTE: When the pulley stop-pin (6) is in the fully closed position, the internal hole aligns with the installation hole (4).

(4) Install the lock pin (3) in the installation hole (4).
(5) FOR [7507MM] (RESERVOIR ASSY OWS R)
(a) Open the aft cargo-compartment door (Ref. AMM TASK 52-30-00-860-001).
(b) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE back in position, adjacent to the aft cargo-compartment exit.

Subtask 25-62-00-820-050-F ** ON A/C NOT FOR ALL

A. Adjustment Procedure

Inflation Reservoir ** ON A/C NOT FOR ALL

Inflation Reservoir - Adjustment Procedure to Install the Lock Pin Assembly ** ON A/C NOT FOR ALL

(1) If necessary, get access to the inflation reservoir (4):
(a) Open the applicable overhead stowage-compartment door.
(b) Remove the screws (2) and the washers (12).
(c) Carefully remove the inspection wall (1) from the overhead stowage compartment.
(2) Remove the lock pin (5) from the pocket (3).
(3) Adjust the regulator valve assembly (7):

(a) Put the ALLEN KEY 3/16 IN (10) into the hexagonal socket (11).
(b) Turn the ALLEN KEY 3/16 IN (10) to the SAFE direction and move the pulley stop-pin (8) to the direction of the black mark (9) (closed position).
(c) Make sure that the pulley stop-pin (8) is in the fully closed position and the internal hole aligns with the installation hole (6).
(4) Install the lock pin (5) in the installation hole (6).

5. Close-up
Subtask 25-62-00-942-062-A ** ON A/C NOT FOR ALL

A. Removal of the Safety Precautions and Wing Protection
(1) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the slat/flap control lever.
(2) Remove the WARNING NOTICE(S).
(3) Remove the safety barriers.
(4) Remove the plastic sheet from the ground.
(5) Remove the tacky tape and protection from the upper surface of the wing.
(6) Remove the access platform(s).

[Rev.10 from 2021] 2026.04.01 06:30:56 UTC