Air-Bus A318 User manual

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-000-001-A - Removal of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 1 of 6
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
** ON A/C ALL
TASK 29-11-52-000-001-A
Removal of the Engine Pump Fire-Valve
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.
WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS
POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
FIN : 1046GK
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 3M (10 FT)
No specific AR CAP - BLANKING
No specific 1 CONTAINER 1 L (1/4 USGAL)
No specific AR PLUG - BLANKING
No specific AR SAFETY BARRIER(S)
No specific AR SAFETY CLIP - CIRCUIT BREAKER
No specific 1 WARNING NOTICE(S)
B. Consumable Materials
REFERENCE DESIGNATION
(Material No. 14SBA1) Textile-Lint free Cotton -
C. Work Zones and Access Panels
ZONE/ACCESS ZONE DESCRIPTION
574AB, 574BB
D. Referenced Information
REFERENCE DESIGNATION
(Ref. 29-00-00-864-001-A). Put the Related Hydraulic System in the Depressurized Configuration
before Maintenance Action

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-000-001-A - Removal of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 2 of 6
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
REFERENCE DESIGNATION
(Ref. 29-00-00-910-002-A). Safety Procedures of the Hydraulic System
(Ref. 29-14-00-614-001-A). Depressurization of the Hydraulic Reservoirs
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-
0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749
Engine Pump Fire-Valve (1046GK)

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-000-001-A - Removal of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 3 of 6
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
1
2
3
6
5
4
COMPENSATED
SLIDE
1010GM
PRE MOD 22155 K 2261
STA2508/RIB 5
574AB
574BB
1
1
A
A
N_MM_291152_4_AAM0_01_00
Figure 29-11-52-991-00100-00-A / SHEET 1/2 - Engine Pump Fire-Valve (1046GK)
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-
0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-000-001-A - Removal of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 4 of 6
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
RIB 5
574AB
574BB
A
A
4
COMPENSATED
SLIDE
1010 GM
6
1
1
POST MOD 22155 K 2261
5
3
2
1
N_MM_291152_4_AAM0_02_00
Figure 29-11-52-991-00100-00-A / SHEET 2/2 - Engine Pump Fire-Valve (1046GK)
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-
0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-000-001-A - Removal of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 5 of 6
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
3. Job Set-up
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-0249, 0251-
0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749
(Ref. Fig. Engine Pump Fire-Valve (1046GK))
** ON A/C ALL
Subtask 29-11-52-941-050-A
A. Safety Precautions
WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
(1) You must obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002) when you do
work on the hydraulic system.
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and
your local regulations.
(3) Put a WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system.
Subtask 29-11-52-864-050-A
B. Depressurize the Applicable Hydraulic System
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
(1) Depressurize the Green Hydraulic system (Ref. AMM TASK 29-00-00-864-001) .
(2) Depressurize the Green Hydraulic system reservoir (Ref. AMM TASK 29-14-00-614-001) .
Subtask 29-11-52-865-050-A
C. Open, safety and tag this(these) circuit breaker(s):
PANEL DESIGNATION FIN LOCATION
49VU HYD/FIRE VALVE/G/ENG1 1703GK C13
121VU HYDRAULIC/G HYD/PUMP ENG1/
MONG 1702GK R34
** ON A/C 0051-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-0249, 0251-0299, 0301-
0399, 0401-0449, 0451-0499, 0501-0549, 0551-0599, 0601-0749, 0751-0799, 0801-0830, 0832-0899, 0901-0999,
1001-1050, 1053-1151, 1153-1153, 1155-1200
Subtask 29-11-52-010-050-B
D. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT) below zone 574.
(2) Remove the access panels 574AB, 574BB.
(3) Put clean Textile-Lint free Cotton - (Material No. 14SBA1) below the engine pump fire valve (5).
(4) Put a CONTAINER 1 L (1/4 USGAL) below the access door opening, to collect the hydraulic fluid.
** ON A/C ALL
4. Procedure

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-000-001-A - Removal of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 6 of 6
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-0249, 0251-
0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749
(Ref. Fig. Engine Pump Fire-Valve (1046GK))
** ON A/C ALL
Subtask 29-11-52-020-050-A
A. Removal of the Engine Fire Pump-Valve
(1) Disconnect the cable connector (1) from the electrical connector (2).
(2) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(3) Hold the engine pump fire-valve (5) and disconnect the coupling-nuts (6) and (3).
(4) Compress the compensated slide (4) to decrease its length. Remove the engine pump fire-valve (5).
(5) Put the PLUG-BLANKING in each disconnected line end.
End of document

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-400-001-A - Installation of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 1 of 7
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
** ON A/C ALL
TASK 29-11-52-400-001-A
Installation of the Engine Pump Fire-Valve
WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES
ARE IN POSITION.
WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS
POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL
MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
FIN : 1046GK
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 3M (10 FT)
** ON A/C 0051-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-0249, 0251-
0299, 0301-0399, 0401-0449, 0451-0499, 0501-0549, 0551-0599, 0601-0749, 0751-0799, 0801-0830,
0832-0899, 0901-0999, 1001-1050, 1053-1151, 1153-1153, 1155-1200
No specific 1 CONTAINER 1 L (1/4 USGAL)
** ON A/C ALL
No specific AR SAFETY BARRIER(S)
No specific 1 WARNING NOTICE(S)
No specific Torque wrench: range to between 8.5 and 9.5 m.daN
(62.68 and 70.06 lbf.ft)
B. Consumable Materials
REFERENCE DESIGNATION
(Material No. 08BAA9) Non Aqueous Cleaner-General - -
(Material No. 14SBA1) Textile-Lint free Cotton -
C. Work Zones and Access Panels
ZONE/ACCESS ZONE DESCRIPTION
574AB, 574BB
D. Referenced Information

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-400-001-A - Installation of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 2 of 7
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
REFERENCE DESIGNATION
(Ref. 29-00-00-864-001-A). Put the Related Hydraulic System in the Depressurized Configuration
before Maintenance Action
(Ref. 29-00-00-910-002-A). Safety Procedures of the Hydraulic System
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-
0249, 0251-0299, 0301-0399, 0401-0449, 0451-0499, 0501-0549, 0551-0599, 0601-0749, 0751-0799,
0801-0830, 0832-0899, 0901-0970
(Ref. 29-10-00-720-001-A). Functional Check of Hydraulic Fire Shut-Off Valves
** ON A/C ALL
(Ref. 29-10-00-863-001-A). Pressurize the Green Hydraulic System with a Hydraulic Ground
Power-Cart
(Ref. 29-10-00-864-001-A). Depressurize the Green Hydraulic System
(Ref. 29-14-00-614-001-A). Depressurization of the Hydraulic Reservoirs
** ON A/C 0051-0099, 0151-0199, 0251-0299, 0351-0399, 0451-0499, 0551-0599, 0601-0650, 0801-
0830, 0832-0899
(Ref. 71-00-00-710-001-B). Dry Motoring Check
** ON A/C ALL
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-
0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749
Engine Pump Fire-Valve (1046GK)

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-400-001-A - Installation of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 3 of 7
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
1
2
3
6
5
4
COMPENSATED
SLIDE
1010GM
PRE MOD 22155 K 2261
STA2508/RIB 5
574AB
574BB
1
1
A
A
N_MM_291152_4_AAM0_01_00
Figure 29-11-52-991-00100-00-A / SHEET 1/2 - Engine Pump Fire-Valve (1046GK)
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-
0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749

Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
Manual : AMM
Selected applicability : 0053-0053
29-11-52-400-001-A - Installation of the Engine Pump Fire-Valve
Print Date: August 16, 2018 Page 4 of 7
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
RIB 5
574AB
574BB
A
A
4
COMPENSATED
SLIDE
1010 GM
6
1
1
POST MOD 22155 K 2261
5
3
2
1
N_MM_291152_4_AAM0_02_00
Figure 29-11-52-991-00100-00-A / SHEET 2/2 - Engine Pump Fire-Valve (1046GK)
** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209-
0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749