Preparation of the Aircraft for Flight with One MLG Door Assembly Missing or One MLG Fixed Fairing Assembly Missing or One Secondary Hinged Fairing Missing

TASK 32-12-00-040-001-A
Preparation of the Aircraft for 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	1	ACCESS PLATFORM 2M (6 FT)
No specific	1	ACCESS PLATFORM 3M (10 FT)
No specific	AR	PLUG - BLANKING
No specific	AR	SAFETY BARRIER(S)
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	1	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 1.808 and 0.904 m.daN (160.00 and 80.00 lbf.in )
No specific	Torque wrench: range to between 2.9 and 2.7 m.daN (21.39 and 19.91 lbf.ft )

B. Consumable Materials

REFERENCE	DESIGNATION
(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

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 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 32-12-00-010-001-A	Open the Main Gear Doors for Access
TASK 32-12-11-000-001-A	Removal of the Door Assembly - Main
TASK 32-12-13-000-001-A	Removal of the Secondary Hinged Fairing
TASK 32-12-14-000-001-A	Removal of the MLG Fixed Fairing Assembly
TASK 32-12-14-400-001-A	Installation of the MLG Fixed Fairing Assembly (That was Removed For Access Only)
TASK 32-31-35-000-001-A	Removal of the MLG Door Actuating-Cylinder
TASK 32-31-38-000-001-A	Removal of the MLG Door Swivel-Joint Assembly
TASK 57-26-21-000-001-A	Removal of the Secondary-Hinged-Fairing Attachment
Bonding Straps to MLG Door Hinge Attachment Points - Removal/Installation
MLG Actuator Flexible Hoses - 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
Attaching Parts for the Secondary Hinged Fairing - Removal/Installation

3. Job Set-up
Subtask 32-12-00-941-063-A

WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.

A. Safety Precautions
(Ref. AMM TASK 29-00-00-910-002)
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(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 the safety device is installed on the applicable MLG (Ref. AMM TASK 32-00-00-481-001).

Subtask 32-12-00-860-056-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 32-12-00-869-059-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 32-12-00-865-062-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 32-12-00-010-057-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) in position below the applicable zone 733(743).

4. Procedure
Subtask 32-12-00-980-050-A

A. Manual Operation

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) In the avionics compartment on the panel 188VU:
(a) Remove the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - from the safety cover of the L/G DOWN VMO/MMO SELECTION switch 22FP.
(b) Set the L/G DOWN VMO/MMO SELECTION switch 22FP to L/G DOWN.

Subtask 32-12-00-020-060-A

B. Removal 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.

(1) Open the applicable MLG door (Ref. AMM TASK 32-12-00-010-001).
(2) Remove the applicable MLG door assembly (Ref. AMM TASK 32-12-11-000-001).
(3) Remove and retain all the nuts and bolts from the MLG door hinge attachment points (4).
(4) Remove and discard the cotter pins (1) from the nuts (2).
(5) Remove and retain the:

nuts (2)
washers (3)
bolts (6)
bonding straps (5)
from the door hinge attachment points (4).

(6) Remove the applicable MLG door-actuating cylinder (Ref. AMM TASK 32-31-35-000-001).
(7) Remove the applicable MLG door swivel-joint assembly (Ref. AMM TASK 32-31-38-000-001).
(8) Remove and retain the nuts (17), the bolts (14), the washers (15) and the clamps (16) from the flexible hoses (13).
(9) Disconnect the connectors (18) from the elbow connectors (19) and remove and retain the flexible hoses (13).
(10) Put a PLUG - BLANKING on the elbow connectors (19).

NOTE: Make sure that the blanking plugs are correctly installed before each flight if subsequent flights in this configuration are necessary.

Subtask 32-12-00-860-058-C

C. ECAM Display During Flight with One MLG Door Assembly Missing

NOTE: The MLG and the NLG must be extended at all times during flight with one MLG door missing (control lever 6GA in the DOWN position).

(1) The ECAM displays (for the applicable missing MLG door) are as follows:
(a) ECAM indications:

door position hinge bar - DOOR IN TRANSIT (amber)
landing gear locked down triangles (green).

(b) ECAM warnings:

L/G DOORS NOT CLOSED (amber) - in flight phases 1, 3, 4, 5, 8, 9 and 10.

NOTE: The warning(s) that follow will only show if LGCIU 1 and/or 2 are reset above 70 knots (or a power interrupt occurs above 70 knots).

L/G RECYCLE, MAX SPEED 250 KNOTS, INCREASED FUEL CONSUMPTION.

L/G DOOR.

Subtask 32-12-00-020-063-A ** ON A/C NOT FOR ALL

D. Removal of the MLG Fixed Fairing Assembly and Attaching Parts

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) Remove the applicable fixed fairing assembly (Ref. AMM TASK 32-12-14-000-001).
(2) Remove and retain all the nuts and bolts that attach the fixed fairing assembly from the MLG.
(3) Remove and discard the cotter pin (51) from the nut (50).
(4) Remove the nut (50), the washer (49) and the bolt (48). Remove and retain the bonding strap (47) from the bracket (46).
(5) Install the bolt (48), the washer (49) and the nut (50).
(6) Safety the nut (50) with a new AIPC 32-11-11-80-090 COTTER PIN (51).
(7) Apply Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the head of the bolt (48) and the nut (50).
(8) Remove and discard the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - from the bolts (53) and (56).
(9) Remove the bolt (56), the washer (55) and the bonding strap (54) from the bracket (52). Retain the bonding strap (54).
(10) Install the washer (55) and the bolt (56).
(11) TORQUE the bolt (56) to between 1.808 and 0.904 m.daN (160.00 and 80.00 lbf.in )

.
(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).

Subtask 32-12-00-020-063-B ** ON A/C NOT FOR ALL

D. Removal of the MLG Fixed Fairing Assembly and Attaching Parts

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.

.
(8) 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).
(9) 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).
(10) Remove and discard the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - from the bolts (53) and (56).
(11) Remove the bolt (56), the washer (55) and the bonding strap (54) from the bracket (52). Retain the bonding strap (54).
(12) Apply Non Hardening Jointing Putty-High Temp. Area - Hydraulic (Material No.06LDG6) to the shank and the threads of the bolt (56).
(13) Install the washer (55) and the bolt (56).
(14) TORQUE the bolt (56) to between 2.9 and 2.7 m.daN (21.39 and 19.91 lbf.ft )

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

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

Subtask 32-12-00-020-063-C ** ON A/C NOT FOR ALL

D. Removal of the MLG Fixed Fairing Assembly and Attaching Parts

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) Remove the applicable fixed fairing assembly (Ref. AMM TASK 32-12-14-000-001).
(2) Remove and keep all the nuts and bolts that attach the fixed fairing assembly from the MLG.
(3) Remove and discard the cotter pin (51) from the nut (50).
(4) Remove the nut (50), the washer (49) and the bolt (48). Remove and keep the bonding strap (47) from the bracket (46).
(5) Apply Non Hardening Jointing Putty-High Temp. Area - Hydraulic (Material No.06LDG6) to the shank and the threads of the bolt (48).
(6) Install the bolt (48), the washer (49) and the nut (50).
(7) TORQUE the nut (50) to between 1.8 and 0.9 m.daN (159.29 and 79.65 lbf.in )

.
(8) 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).
(9) 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).
(10) Remove and discard the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - from the bolts (53) and (56).
(11) Remove the bolt (56), the washer (55) and the bonding strap (54) from the bracket (52). Keep the bonding strap (54).
(12) Apply Non Hardening Jointing Putty-High Temp. Area - Hydraulic (Material No.06LDG6) to the shank and the threads of the bolt (56).
(13) Install the washer (55) and the bolt (56).
(14) TORQUE the bolt (56) to between 2.9 and 2.7 m.daN (21.39 and 19.91 lbf.ft )

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

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

Subtask 32-12-00-020-064-A

E. Removal of the Secondary Hinged Fairing and Attaching Parts

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 MLG fixed fairing assembly (Ref. AMM TASK 32-12-14-000-001).
(2) Remove the secondary hinged fairing (Ref. AMM TASK 32-12-13-000-001).
(3) Remove and retain all the nuts and bolts that attach the secondary hinged fairing from the MLG.
(4) Remove the secondary hinged fairing attachment (Ref. AMM TASK 57-26-21-000-001).
(5) Remove and retain all the nuts and bolts that attach the secondary hinged fairing attachment from the MLG.
(6) Identify the position of the hinged fairing mounting plate (66) before you remove it.
(7) Remove and discard the cotter pin (69) from the nut (68).
(8) Remove and retain the nut (68) and the washer (70).
(9) Remove and retain the:

nuts (73)
bolts (67)
hinged fairing mounting plate (66)
shim (71)
packer (72).

(10) Remove and retain the:

bolt (83)
washer (82)
bonding strap (84)
nut (75)
from the transfer block (80).

(11) Remove and retain the:

bolt (79)
washer (78)
pin (77)
spacer (76)
threaded insert (81)
from the transfer block (80).

(12) Remove and retain the actuating rod (74) from the transfer block (80).
(13) Install the MLG fixed fairing assembly (Ref. AMM TASK 32-12-14-400-001).

Subtask 32-12-00-865-058-A

F. 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 32-12-00-860-057-A

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

Subtask 32-12-00-942-057-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 00:41:05 UTC