Restoration of the Aircraft after Flight with One MLG Door Assembly Missing or One MLG Fixed Fairing Assembly Missing or One Secondary Hinged Fairing Missing

TASK 32-12-00-440-001-A
Restoration of the Aircraft after Flight with One MLG Door Assembly Missing or One MLG Fixed Fairing Assembly Missing or One Secondary Hinged Fairing Missing

WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR:

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

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

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

1. Reason for the Job
CDL 52-14
Main Landing Gear Door (732, 742) (Flight with gear down)
CDL 52-15
Main Landing Gear Door (733, 743) (Flight with gear down)
CDL 52-16
Main Landing Gear Door (734, 744) (Flight with gear down)
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 2M (6 FT)
No specific	AR	ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific	1	PLUG - BLANKING
No specific	AR	SAFETY BARRIER(S)
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 1.8 and 0.9 m.daN (159.29 and 79.65 lbf.in )
No specific	Torque wrench: range to between 2.9 and 2.7 m.daN (21.39 and 19.91 lbf.ft )
No specific	Torque wrench: range to between 3.2 and 2.9 m.daN (23.60 and 21.39 lbf.ft )

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.02ABA1)	Phosphate Ester Hydraulic Fluid-General Power - -
(Material No.04JMD9)	Top Coat Polyurethane-- Decorative Furnishing
(Material No.06AAB1)	Polysulfide Sealant-General Purpose Fillet -
(Material No.06AAC5)	Polysulfide Sealant-General Purpose Interfay Landing Gear
(Material No.06LDG6)	Non Hardening Jointing Putty-High Temp. Area - Hydraulic
(Material No.14QFB1)	Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
824

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
51	COTTER PIN	AIPC 32-11-11-80-090
51	COTTER PIN	AIPC 32-11-85-80-090
1	COTTER PIN	AIPC 32-12-03-01-130
1	COTTER PIN	AIPC 32-12-83-01-130
69	COTTER PIN	AIPC 57-26-05-36-030
69	COTTER PIN	AIPC 57-26-85-36-120

E. Referenced Information

REFERENCE	DESIGNATION
TASK 12-22-32-640-001-A	Lubrication of Main Landing Gear and Doors
TASK 20-28-00-912-802-A	Electrical Bonding - General Maintenance Procedure
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 29-00-00-910-002-A	Safety Procedures of the Hydraulic System
TASK 29-10-00-864-001-A	Depressurize the Green Hydraulic System
TASK 32-00-00-481-001-A	Installation of the Safety Devices on the Landing Gears
TASK 32-00-00-860-001-A	Flight Configuration Precautions with Electrical Power
TASK 32-00-00-860-001-A-01	Flight Configuration Precautions without Electrical Power
TASK 32-00-00-860-002-A	Ground Configuration after Flight Configuration with Electrical Power
TASK 32-00-00-860-002-A-01	Ground Configuration after Flight Configuration without Electrical Power
TASK 32-12-11-400-001-A	Installation of the Door Assembly - Main
TASK 32-12-13-400-001-A	Installation of a Replacement Secondary Hinged Fairing
TASK 32-12-14-000-001-A	Removal of the MLG Fixed Fairing Assembly
TASK 32-12-14-400-002-A	Installation of a Replacement MLG Fixed-Fairing Assembly
TASK 32-31-00-710-002-A	Operational Test of the Landing Gear Doors (With False Targets)
TASK 32-31-00-710-002-A-01	Operational Test of the Landing Gear Doors (Without False Targets)
TASK 32-31-35-400-001-A	Installation of the MLG Door Actuating-Cylinder
TASK 32-31-38-400-001-A	Installation of the MLG Door Swivel-Joint Assembly
TASK 51-75-13-916-002-A	Repair to a layer of Corrosion Preventive Compound
TASK 57-26-21-400-001-A	Installation of the Secondary-Hinged-Fairing Attachment
Bonding Straps to MLG Door Hinge Attachment Points - Removal/Installation
MLG Actuator Flexible Hoses - Removal/Installation
Attaching Parts for the Secondary Hinged Fairing - Removal/Installation
Bonding Straps to MLG Leg - Removal/Installation ** ON A/C NOT FOR ALL
Bonding Straps to MLG Leg - Removal/Installation ** ON A/C NOT FOR ALL

3. Job Set-up
Subtask 32-12-00-941-064-A

WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.

A. Safety Precautions
(Ref. AMM TASK 29-00-00-910-002)
(1) Put the SAFETY BARRIER(S) in position.
(2) On the panel 400VU:

Make sure that the landing-gear control-lever 6GA is in the DOWN position
Put a WARNING NOTICE(S) in position to tell persons not to operate the landing gear.

(3) On the panel 110VU, make sure that the GRAVITY GEAR EXTN handle is folded into the center console.
(4) Make sure that the safety device is installed on the applicable MLG (Ref. AMM TASK 32-00-00-481-001).

Subtask 32-12-00-860-063-A

B. Aircraft Maintenance Configuration

WARNING: 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) Depressurize the Green hydraulic system
(Ref. AMM TASK 29-10-00-864-001).

Subtask 32-12-00-869-060-A

C. Flight Configuration Precautions
(1) Do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.

Subtask 32-12-00-865-063-A

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

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
49VU	L/G/LGCIU/SYS1/NORM	1GA	C09
** ON A/C NOT FOR ALL
49VU	HYDRAULIC/G HYD/PUMP ENG1/CTL	1701GK	H12
** ON A/C NOT FOR ALL
121VU	HYDRAULIC/G HYD/PUMP ENG1/CTL	1701GK	R35
** ON A/C NOT FOR ALL
121VU	HYDRAULIC/G HYD/PUMP ENG1/MONG	1702GK	R34
121VU	LGCIU/BAT SPLY/SYS2	59GA	R33
121VU	LGCIU/BAT SPLY/SYS1	58GA	R32
** ON A/C ALL
121VU	HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY	4GG	M36
121VU	HYDRAULIC/BRAKING AND STEERING/SYS2/CTL	3GG	M35
121VU	HYDRAULIC/BRAKING AND STEERING/SYS1/CTL	1GG	M34
121VU	HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY	2GG	M33
121VU	HYDRAULIC/Y HYD/PUMP ENG2/MONG	3700GD	Q37
121VU	HYDRAULIC/Y HYD/PUMP ENG2/CTL	3701GD	Q36
121VU	HYDRAULIC/LGCIU/SYS2	2GA	Q35
121VU	HYDRAULIC/LGCIU/SYS1/GRND SPLY	52GA	Q34
** ON A/C NOT FOR ALL
121VU	HYDRAULIC/G HYD/PUMP ENG1/MONG	1702GK	R33
121VU	LGCIU/BAT SPLY/SYS2	59GA	R32
121VU	LGCIU/BAT SPLY/SYS1	58GA	R31

Subtask 32-12-00-010-058-A

E. Get Access
(1) Put the ACCESS PLATFORM 2M (6 FT) in position below the applicable zone 128.
(2) Open the access door 824.
(3) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable zone 733(743).

4. Procedure
Subtask 32-12-00-420-065-A

A. Installation of the MLG Door Assembly and Attaching Parts

Bonding Straps to MLG Door Hinge Attachment Points - Removal/Installation

MLG Actuator Flexible Hoses - Removal/Installation

CAUTION: DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.

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

(5) Apply Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) to the threads of the elbow connectors (18).
(6) Put the flexible hoses (13) in position and connect the connectors (18) to the elbow connectors (19).
(7) Tighten the connectors (18) and TORQUE to between 3.2 and 2.9 m.daN (23.60 and 21.39 lbf.ft )

.
(8) Apply corrosion protection to the connectors (18) and (19) and the adjacent areas (Ref. AMM TASK 51-75-13-916-002).
(9) Make a mark on the connectors (18) and (19) with Top Coat Polyurethane-- Decorative Furnishing (Material No.04JMD9) .
(10) Put the clamps (16) in position on the flexible hoses (13) and install the bolts (14), the washers (15) and the nuts (17).

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

(11) Apply Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the heads of the bolts (14) and the nuts (17).
(12) Install the applicable MLG door swivel-joint assembly (Ref. AMM TASK 32-31-38-400-001).
(13) Install the applicable MLG door actuating cylinder (Ref. AMM TASK 32-31-35-400-001).
(14) Install the bonding straps (5), the bolts (6), the washers (3) and the nuts (2) to the hinge attachment points (4) (Ref. AMM TASK 20-28-00-912-802).
(15) Safety the nuts (2) with the new AIPC 32-12-03-01-130 COTTER PIN (1) or the new AIPC 32-12-83-01-130 COTTER PIN (1).

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

(16) Apply Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the heads of the bolts (6) and the nuts (2).
(17) Install the applicable MLG door assembly (Ref. AMM TASK 32-12-11-400-001).

Subtask 32-12-00-640-050-A

B. Lubrication
(1) Lubricate the applicable door hinge connection points (Ref. AMM TASK 12-22-32-640-001).

Subtask 32-12-00-710-054-A

C. Operational Test
(1) Do an operational test of the main landing gear doors (Ref. AMM TASK 32-31-00-710-002).

Subtask 32-12-00-420-062-A

D. Installation of the Secondary Hinged Fairing and Attachments

Attaching Parts for the Secondary Hinged Fairing - Removal/Installation

CAUTION: DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.

(1) Remove the applicable fixed fairing assembly (Ref. AMM TASK 32-12-14-000-001).
(2) Clean the component interfaces and/or the adjacent area.
(3) Do an inspection of the component interfaces and/or the adjacent area.
(4) Make sure that the parts retained from the removed components are clean and in the correct condition.
(5) Put the actuating rod (74) between the lugs of the transfer block (80).
(6) Install the threaded insert (81), the spacer (76), the pin (77), the washer (78) and the bolt (79) to the transfer block (80).
(7) Install the nut (75), the bonding strap (84), the washer (82) and the bolt (83) to the transfer block (80) (Ref. AMM TASK 20-28-00-912-802).

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

(8) Apply Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the heads of the bolts (79) and (83) and the nut (75).
(9) Install the packer (72), the shim (71), the hinged fairing mounting plate (66), the washer (70) and loosely install the nut (68).
(10) Install the screws (67) and loosely install the nuts (73).
(11) Hold the mounting plate (66) in the position identified before removal.
(12) Tighten the nuts (73) and the nut (68).
(13) Safety the nut (68) with a new AIPC 57-26-05-36-030 COTTER PIN (69) or AIPC 57-26-85-36-120 COTTER PIN (69).

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

(14) Apply Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the heads of the screws (67) and the nuts (68) and (73).
(15) Install the applicable secondary-hinged-fairing attachment (Ref. AMM TASK 57-26-21-400-001).
(16) Install the applicable secondary hinged fairing (Ref. AMM TASK 32-12-13-400-001).

Subtask 32-12-00-420-063-A ** ON A/C NOT FOR ALL

E. Installation of the MLG Fixed Fairing Assembly and Attachments

Bonding Straps to MLG Leg - Removal/Installation ** ON A/C NOT FOR ALL

CAUTION: DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.

(1) Clean the component interfaces and/or the adjacent area.
(2) Do an inspection of the component interfaces and/or the adjacent area.
(3) Make sure that the parts retained from the removed components are clean and in the correct condition.
(4) Remove and discard the cotter pin (51) from the nut (50).
(5) Remove the nut (50), the washer (49) and the bolt (48) from the bracket (46).
(6) Install the bonding strap (47), the bolt (48), the washer (49) and the nut (50) (Ref. AMM TASK 20-28-00-912-802).
(7) Safety the nut (50) with a new AIPC 32-11-11-80-090 COTTER PIN (51).

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

(8) Apply Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the head of the bolt (48) and the nut (50).

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.

(9) Remove and discard the lockwire from the bolts (53) and (56).
(10) Remove the bolt (56) and the washer (55) from the bracket (52).
(11) Install the bonding strap (54), the washer (55) and the bolt (56) (Ref. AMM TASK 20-28-00-912-802).
(12) Safety the bolts (53) and (56) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.

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

(13) Apply Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the heads of the bolts (53) and (56).
(14) Install the fixed fairing assembly (Ref. AMM TASK 32-12-14-400-002).

Subtask 32-12-00-420-063-B ** ON A/C NOT FOR ALL

E. Installation of the MLG Fixed Fairing Assembly and Attachments

Bonding Straps to MLG Leg - Removal/Installation ** ON A/C NOT FOR ALL

CAUTION: DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.

(1) Clean the component interfaces and/or the adjacent area.
(2) Do an inspection of the component interfaces and/or the adjacent area.
(3) Make sure that the parts retained from the removed components are clean and in the correct condition.
(4) Remove and discard the cotter pin (51) from the nut (50).
(5) Remove the nut (50), the washer (49) and the bolt (48) from the bracket (46).
(6) Apply Non Hardening Jointing Putty-High Temp. Area - Hydraulic (Material No.06LDG6) to the shank and the threads of the bolt (48).
(7) Install the bonding strap (47), the bolt (48), the washer (49) and the nut (50) (Ref. AMM TASK 20-28-00-912-802).
(8) TORQUE the nut (50) to between 1.8 and 0.9 m.daN (159.29 and 79.65 lbf.in )

.
(9) Safety the nut (50) with a new AIPC 32-11-11-80-090 COTTER PIN (51) or AIPC 32-11-85-80-090 COTTER PIN (51).
(10) Apply Polysulfide Sealant-General Purpose Interfay Landing Gear (Material No.06AAC5) to the nut (50), the washer (49) and the head of the bolt (48).
(11) Remove and discard the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - from the bolts (53) and (56).
(12) Remove the bolt (56) and the washer (55) from the bracket (52).
(13) Apply Non Hardening Jointing Putty-High Temp. Area - Hydraulic (Material No.06LDG6) to the shank and the threads of the bolt (56).
(14) Install the bonding strap (54), the washer (55) and the bolt (56) (Ref. AMM TASK 20-28-00-912-802).
(15) TORQUE the bolt (56) to between 2.9 and 2.7 m.daN (21.39 and 19.91 lbf.ft )

.
(16) Safety the bolts (53) and (56) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
(17) Apply Polysulfide Sealant-General Purpose Interfay Landing Gear (Material No.06AAC5) to:

The head of the bolts (53) and (56)
The washer (55).

(18) Install the fixed fairing assembly (Ref. AMM TASK 32-12-14-400-002).

Subtask 32-12-00-420-063-C ** ON A/C NOT FOR ALL

E. Installation of the MLG Fixed Fairing Assembly and Attachments

Bonding Straps to MLG Leg - Removal/Installation ** ON A/C NOT FOR ALL

CAUTION: DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.

(1) Clean the component interfaces and/or the adjacent area.
(2) Do an inspection of the component interfaces and/or the adjacent area.
(3) Make sure that the parts retained from the removed components are clean and in the correct condition.
(4) Remove and discard the cotter pin (51) from the nut (50).
(5) Remove the nut (50), the washer (49) and the bolt (48) from the bracket (46).
(6) Apply Non Hardening Jointing Putty-High Temp. Area - Hydraulic (Material No.06LDG6) to the shank and the threads of the bolt (48).
(7) Install the bonding strap (47), the bolt (48), the washer (49) and the nut (50) (Ref. AMM TASK 20-28-00-912-802).
(8) TORQUE the nut (50) to between 1.8 and 0.9 m.daN (159.29 and 79.65 lbf.in )

.
(16) Safety the bolts (53) and (56) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
(17) Apply Polysulfide Sealant-General Purpose Interfay Landing Gear (Material No.06AAC5) to:

The head of the bolts (53) and (56)
The washer (55).

(18) Install the fixed fairing assembly (Ref. AMM TASK 32-12-14-400-002).

Subtask 32-12-00-980-051-A

F. Manual Operation

(1) In the avionics compartment on the panel 188VU:
(a) Set the L/G DOWN VMO/MMO SELECTION switch 22FP to NORM.
(b) Lock the safety cover and secure it with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.

Subtask 32-12-00-865-065-A

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

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
49VU	L/G/LGCIU/SYS1/NORM	1GA	C09
** ON A/C NOT FOR ALL
49VU	HYDRAULIC/G HYD/PUMP ENG1/CTL	1701GK	H12
** ON A/C NOT FOR ALL
121VU	HYDRAULIC/G HYD/PUMP ENG1/CTL	1701GK	R35
** ON A/C NOT FOR ALL
121VU	HYDRAULIC/G HYD/PUMP ENG1/MONG	1702GK	R34
121VU	LGCIU/BAT SPLY/SYS2	59GA	R33
121VU	LGCIU/BAT SPLY/SYS1	58GA	R32
** ON A/C ALL
121VU	HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY	4GG	M36
121VU	HYDRAULIC/BRAKING AND STEERING/SYS2/CTL	3GG	M35
121VU	HYDRAULIC/BRAKING AND STEERING/SYS1/CTL	1GG	M34
121VU	HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY	2GG	M33
121VU	HYDRAULIC/Y HYD/PUMP ENG2/MONG	3700GD	Q37
121VU	HYDRAULIC/Y HYD/PUMP ENG2/CTL	3701GD	Q36
121VU	HYDRAULIC/LGCIU/SYS2	2GA	Q35
121VU	HYDRAULIC/LGCIU/SYS1/GRND SPLY	52GA	Q34
** ON A/C NOT FOR ALL
121VU	HYDRAULIC/G HYD/PUMP ENG1/MONG	1702GK	R33
121VU	LGCIU/BAT SPLY/SYS2	59GA	R32
121VU	LGCIU/BAT SPLY/SYS1	58GA	R31

5. Close-up
Subtask 32-12-00-860-064-A

A. Aircraft Maintenance Configuration
(1) Close the access door 824.
(2) Put the aircraft back to the ground configuration (Ref. AMM TASK 32-00-00-860-002).
(3) Depressurize the Green hydraulic system
(Ref. AMM TASK 29-10-00-864-001).
(4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).

Subtask 32-12-00-942-060-A

B. Removal of Equipment
(1) Remove the access platform(s).
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.04.01 00:41:08 UTC