DOC AIRBUS | AMM A320FReactivation of the Cascade [CFML]
TASK 78-30-00-440-811-A
Reactivation of the Cascade
CDL 78-71
Thrust Reverser Cascade
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 78-30-00-941-099-A
[Rev.10 from 2021]
2026.04.01 03:34:51 UTC
Reactivation of the Cascade
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.
ZONE: 400
1. Reason for the JobCDL 78-71
Thrust Reverser Cascade
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 400 | POWER PLANT, NACELLES AND PYLONS |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 78-30-00-440-808-A | Reactivation of the Thrust Reverser System after Flight |
| TASK 78-32-43-400-806-A | Installation of the Thrust Reverser Cascades |
Deactivation/Reactivation of the CascadeSubtask 78-30-00-941-099-A
A. Not Applicable
4. ProcedureCAUTION:
ONLY ONE OF THE CASCADES CAN BE MISSING AT THE SAME TIME FROM EACH THRUST REVERSER COWL.
Subtask 78-30-00-420-058-A A. Installation of the Thrust Reverser Cascade
(1) Install the thrust reverser cascade no.1, no.2 and no.10 (Ref. AMM TASK 78-32-43-400-806).
Subtask 78-30-00-440-078-A (1) Install the thrust reverser cascade no.1, no.2 and no.10 (Ref. AMM TASK 78-32-43-400-806).
B. Reactivation of the Thrust Reverser after Flight
(1) Reactivate the thrust reverser after flight (Ref. AMM TASK 78-30-00-440-808).
(1) Reactivate the thrust reverser after flight (Ref. AMM TASK 78-30-00-440-808).