W DOC AIRBUS | AMM A320F

Visual Inspection of the Fuel Metering Unit (FMU) [CFML]


TASK 73-21-05-210-801-A
Visual Inspection of the Fuel Metering Unit (FMU)


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
AR
WARNING NOTICE(S)
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 70-70-00-910-804-A
Electrical Standard Practices
TASK 73-21-05-000-802-A
Removal of the Fuel Metering Unit (FMU)
TASK 73-21-05-400-802-A
Installation of the Fuel Metering Unit (FMU)
3. Job Set-up
Subtask 73-21-05-941-054-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 a WARNING NOTICE(S) in position to tell persons not to operate:
  • The ENG/MODE selector switch
  • 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).
4. Procedure
Subtask 73-21-05-210-050-A
A. Do the visual inspection of the Fuel Metering Unit (FMU).
INSPECTION/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
1.Examine the FMU for:


A.Signs of fuel leaks
Not permitted.
If you see signs of fuel leaks, replace the FMU gasket seals (Ref. AMM TASK 73-21-05-000-802) and (Ref. AMM TASK 73-21-05-400-802).
B.Make sure that the FMU is not loose
Not permitted.
If the FMU is loose, tighten the mounting bolts (Ref. AMM TASK 73-21-05-400-802).
C.Nick, dents or scratches
Permitted, if they are less than 0.010 in. (0.25 mm) in depth after removal of high metal.


Not permitted on an edge, on small radius or corners of the assembly.


Not permitted across mating joints, sealing surfaces or seal grooves.

D.Cracks
Not permitted.
If you see cracks, replace the FMU (Ref. AMM TASK 73-21-05-000-802) and (Ref. AMM TASK 73-21-05-400-802).
E.Loose FMU electrical connectors
Not permitted.
Tighten the electrical connectors (Ref. AMM TASK 70-70-00-910-804).
5. Close-up
Subtask 73-21-05-942-050-A
A. Put the aircraft back to its initial configuration.
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 03:04:25 UTC