W DOC AIRBUS | AMM A320F

Installation of the PS13 Line [CFMB]

TASK 72-23-00-400-029-A
Installation of the PS13 Line

FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** 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
AR
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 150 and 135 lbf.in (1.70 and 1.53 m.daN ) T
No specific
Torque wrench: range to between 200 and 180 lbf.in (2.26 and 2.03 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2101)
graphite grease
(Material No.CP8001)
lockwire 0.032 in. (0.8 mm) dia.
(Material No.CP8002)
lockwire 0.032 in. (0.8 mm) dia
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
TASK 71-13-00-410-040-B
Closing of the Fan Cowl Doors
F Removal/Installation of the PS13 Line
3. Job Set-up
Subtask 72-23-00-860-064-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) On the center pedestal, on the ENG panel 115VU, make sure that a WARNING NOTICE(S) is in position to tell persons not to start the engine.
   (2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) is off. Make sure that a WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).
   (3) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position.
Subtask 72-23-00-010-105-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that the fan cowl doors are open: (Ref. AMM TASK 71-13-00-010-040)
   (2) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (3) FOR [1000EM2] (ENGINE-2)
447AL 448AR
4. Procedure
Subtask 72-23-00-420-065-A ** ON A/C NOT FOR ALL
A. Installation of the PS13 Line
CAUTION: USE 2 WRENCHES TO REMOVE/INSTALL THE TUBE UNION NUT: ONE TO HOLD THE FITTING, THE OTHER TO LOOSE/TORQUE THE NUT. OTHERWISE, DAMAGE TO THE HARDWARE CAN OCCUR.
   (1) Lubricate the ECU and the fan frame boss nipples with engine fuel.
   (2) Connect the PS13 line to the ECU and to the fan frame boss by hand.
   (3) Lubricate the threads of the bolts (40), (50), (90), (130), (170), (210) with graphite grease (Material No.CP2101) .
   (4) Install the parts which attach the PS13 line as follows:
INSTALL
ON
NOTE
Nut (10)
Bolt (40)
Bracket (20) on flange F
At the 4:45 o'clock
position (Detail B)
Nut (80)
Bolt (50)
Clamp (70)
Bracket (60) on flange F
At the 4:30 o'clock
position (Detail C)
Nut (120)
Bolt (90)
Clamp (100)
Bracket (110) on flange F
At the 4 o'clock
position (Detail D)
Nut (140)
Bolt (130)
Clamp (160)
Bracket (150) on flange F
At the 3:45 o'clock
position (Detail E)
Nuts (200)
Bolts (170)
Clamps (190)
Brackets (180) on flange G
At the 3 o'clock,
2 o'clock and 1:30 o'clock
positions (3 locations)
(Detail F)
Nut (240)
Bolt (210)
Clamp (230)
Bracket (220) on flange G
At the 2:30 o'clock
position (Detail G)
   (5) TORQUE the PS13 connection to the ECU to between 200 and 180 lbf.in (2.26 and 2.03 m.daN ) T.
   (6) Safety with CP8001lockwire 0.032 in. (0.8 mm) dia. or CP8002lockwire 0.032 in. (0.8 mm) dia.
   (7) TORQUE the PS13 connection to the fan frame boss to between 150 and 135 lbf.in (1.70 and 1.53 m.daN ) T.
   (8) Safety with CP8001lockwire 0.032 in. (0.8 mm) dia. or CP8002lockwire 0.032 in. (0.8 mm) dia.
5. Close-up
Subtask 72-23-00-410-095-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 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
   (3) Remove the WARNING NOTICE(S).
   (4) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.01 02:41:40 UTC
"Aviabrain" 2025