W DOC AIRBUS | TSM A320F

Impact on Engine Cowls


TASK 05-50-00-810-812-A
Impact on Engine Cowls


1. Possible Causes

2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 05-51-27-200-001
Inspection after an Impact on the Nacelle or the Engine Equipment
3. Fault Confirmation
Subtask 05-50-00-710-061-A
A. Not Applicable
4. Fault Isolation
Subtask 05-50-00-810-061-A
A. After an engine side loads:
   (1) Do the procedure: Inspection after Impact on Engine Cowls AMM 05-51-27-200-001.
[Rev.8 from Aug 2018] 2026.04.04 04:24:34 UTC