DOC AIRBUS | AMM A320FGeneral Visual Inspection of the Air Intake Cowl (MPD) [CFML]
TASK 71-60-41-210-801-A
General Visual Inspection of the Air Intake Cowl (MPD)
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 71-60-41-941-050-A
Subtask 71-60-41-210-050-A
Subtask 71-60-41-942-050-A
[Rev.10 from 2021]
2026.04.01 13:03:35 UTC
General Visual Inspection of the Air Intake Cowl (MPD)
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 JobSelf 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) |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 71-60-41-960-801-A | Replacement of the Air Intake Aerofiller |
Resin Impregnation at Panel EdgeSubtask 71-60-41-941-050-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:
(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).
(3) Put a ACCESS PLATFORM 1M(3 FT).
4. Procedure(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
- The ENG/MASTER 1(2) control switch.
(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).
(3) Put a ACCESS PLATFORM 1M(3 FT).
Subtask 71-60-41-210-050-A
A. General Visual Inspection (GVI) of the Nose-Lip Aero Filler and the Inner and Outer Barrel Aero-Filler of the Air Inlet Cowl
(1) Do a GVI of the nose-lip aero filler and the inner and outer barrel aero-filler of the air inlet cowl for sealant damage.
(a) If there is sealant damage, replace the applicable air-inlet-cowl aero filler (Ref. AMM TASK 71-60-41-960-801).
5. Close-up(1) Do a GVI of the nose-lip aero filler and the inner and outer barrel aero-filler of the air inlet cowl for sealant damage.
(a) If there is sealant damage, replace the applicable air-inlet-cowl aero filler (Ref. AMM TASK 71-60-41-960-801).
NOTE: On the rear and forward panel edges, you can have resin impregnation (brown) due to curing production cycle. This is acceptable.
Subtask 71-60-41-942-050-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 access platform(s).
(3) Remove the WARNING NOTICE(S).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).