W DOC AIRBUS | AMM A320F

General Visual Inspection of Lower Half of Fuselage


TASK 05-21-00-200-002-A
General Visual Inspection of Lower Half of Fuselage


WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND RELATED DOORS - THE CARGO DOORS - THE ENGINES - OTHER COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
ZONE: 100
1. Reason for the Job
Refer to the MPD TASK: ZL-100-02
GENERAL VISUAL INSPECTION OF LOWER HALF OF FUSELAGE
NOTE: This task can contribute to fuel savings.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
100
LOWER HALF FUSELAGE INCLUDING RADOME
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 53-35-00-200-002-A
Inspection of the Wing-to-Fuselage Fairings and the Belly-Fairing Access Panels for Missing Fasteners
F Lower Half of the Fuselage ** ON A/C NOT FOR ALL
F Lower Half of the Fuselage ** ON A/C NOT FOR ALL
F Lower Half of the Fuselage ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 05-21-00-010-050-A
A. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) in position at zone 100.
WARNING: BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS AND ATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
   (2) Put on and attach a safety harness before you start work in the work area.
4. Procedure
Subtask 05-21-00-210-051-A
A. Inspection
F Lower Half of the Fuselage ** ON A/C NOT FOR ALL
F Lower Half of the Fuselage ** ON A/C NOT FOR ALL
F Lower Half of the Fuselage ** ON A/C NOT FOR ALL
   (1) Do a general visual inspection of the external lower half of the fuselage up to STGR23LH and STGR23RH and the areas around the doors (zone 100).
   (2) Make sure that there is no deterioration (damage, corrosion, leakage, cracks or chafing) on all the parts of the components and the structure you can see.
   (3) Examine the wing-to-fuselage fairings and the belly-fairing access panels for missing fasteners (Ref. AMM TASK 53-35-00-200-002).
5. Close-up
Subtask 05-21-00-410-050-A
A. Close Access
   (1) Remove the access platform(s).
   (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
[Rev.10 from 2021] 2026.03.31 22:48:27 UTC