W DOC AIRBUS | AMM A320F

Visual Inspection of the Fuel Filter Differential Pressure (FFDP) Sensor (Transducer) [CFML]


TASK 73-34-05-210-801-A
Visual Inspection of the Fuel Filter Differential Pressure (FFDP) Sensor (Transducer)


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.
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 1M(3 FT)
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL, 438AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL, 448AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 70-70-00-910-804-A
Electrical Standard Practices
TASK 71-00-00-700-805-A
Dry-Motoring Check
TASK 71-13-00-010-803-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-803-A
Closing of the Fan Cowl Doors
TASK 73-34-05-000-801-A
Removal of the Fuel Filter Differential Pressure Sensor
TASK 73-34-05-400-801-A
Installation of the Fuel Filter Differential Pressure Sensor
3. Job Set-up
Subtask 73-34-05-941-052-A
A. Safety Precautions
   (1) On the center pedestal, on ENG panel 115VU:
     (a) Make sure that the ENG/MODE selector switch is in the NORM position.
     (b) Make sure that the ENG/MASTER 1(2) control switch was in the OFF position not less than five minutes before you do this procedure.
     (c) Put WARNING NOTICE(S) in position to tell persons not to operate:
  • The ENG/MODE selector switch, and
  • The ENG/MASTER 1(2) control switch.
   (2) On the ENG section of maintenance panel 50VU:
     (a) Make sure that the ON legend of the FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) in position to tell persons not to energize FADEC 1(2).
Subtask 73-34-05-010-052-A
B. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL 448AR
   (2) Put an ACCESS PLATFORM 1M(3 FT) in position.
4. Procedure
Subtask 73-34-05-210-050-A
A. Examine the Fuel Filter Differential Pressure (FFDP) Sensor (Transducer) as follows:
Inspection/Check
Maximum Serviceable Limits
Remarks
1.Examine the FFDP sensor for:


(a) Signs of fuel leaks
Not permitted
Replace the FFDP sensor O-ring (Ref. AMM TASK 73-34-05-000-801) and (Ref. AMM TASK 73-34-05-400-801).
(b) Looseness
Not permitted
Tighten the bolts that attach the FFDP sensor to the fuel filter (Ref. AMM TASK 73-34-05-400-801).
(c) Loose electrical connectors
Not permitted
Tighten the electrical connector on the FFDP sensor (Ref. AMM TASK 70-70-00-910-804).
5. Close-up
Subtask 73-34-05-710-051-A
A. Test
   (1) If you found leaks in Step 4.A.(1)(a), do the task that follows after you repair the leaks.
     (a) Do a dry-motoring check (Ref. AMM TASK 71-00-00-700-805).
     (b) Repair the leaks you find.
     (c) Examine the location for the leaks again.
Subtask 73-34-05-410-051-A
B. 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 71-13-00-410-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL 448AR
   (3) Remove the access platform(s).
   (4) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 03:06:40 UTC