W DOC AIRBUS | AMM A320F

Visual Inspection of the Drain Mast


TASK 30-71-51-200-001-A
Visual Inspection of the Drain Mast


1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 30-71-00-710-001-A
Operational Test of the Drainmast Ice Protection
TASK 30-71-51-000-001-A
Removal of the Drain Mast
TASK 30-71-51-400-001-A
Installation of the Drain Mast
3. Job Set-up
Subtask 30-71-51-860-051-A
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 30-71-51-865-062-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VUWASTE WIP-DRAINMAST-FWD1DUB06
** ON A/C NOT FOR ALL
2000VUDRAINMAST-FWD1DUB03
** ON A/C NOT FOR ALL
2000VUWASTE WIP-DRAINMAST-FWD1DUB03
** ON A/C ALL
2001VUWASTE WIP-DRAINMAST-AFT11DUE01
** ON A/C NOT FOR ALL
2001VUWASTE WIP-DRAINMAST-MID21DUE02
Subtask 30-71-51-010-053-A
C. Get Access
   (1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the related Drain Mast.
4. Procedure
Subtask 30-71-51-210-050-A
A. General
The drain mast cover is an aerodynamic cover made of aluminum. It has a wall thickness of 1.2 mm (0.0472 in.) (without corrosion-paint and lacquer).
   (1) General requirements:
A serviceable drain mast must have:
  • No lateral deformation
  • No cracks
  • No scratches and abrasions with a depth of more than max. 50% of the cover material thickness 0.6 mm (0.0236 in.).
If the corrosion protection is damaged, make the scratches smooth.
Repair the surface protection and paint coating after repair of scratches and abrasion.
   (2) Damage limits:
NOTE: If the dents depth in Zone 2 is less than 3.0 mm (0.1181 in.), no maintenance action (replacement) is necessary.
The drain mast cover is divided into 4 Zones with special zone-limits:
  • Zone 1: max. dent depth 0.0 mm (0.0000 in.)
  • Zone 2: max. dent depth 3.0 mm (0.1181 in.)
  • Zone 3: max. dent depth 0.0 mm (0.0000 in.)
  • Zone 4: max. dent depth 0.0 mm (0.0000 in.).
   (3) Visual inspection of the drain mast:
Do a visual inspection of the drain mast for cracks, scratches, dents, deformation and abrasion.
Make sure that the bolts, which connect the drain mast to the fuselage, are tight.
Do a check of the adjacent area for damage.
     (a) If you find scratches and abrasion with a depth less than 50% of the material thickness, 0.6 mm (0.0236 in.):
       1 If the operational test is correct and the corrosion protection is not damaged:
  • No additional test or replacement is necessary.
       2 If the operational test is correct but the corrosion protection is damaged:
       3 If the operational test is not correct:
     (b) If you find cracks, scratches, dents, deformation and abrasion which are not in the given limits and zone-limits:
5. Close-up
Subtask 30-71-51-865-063-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VUWASTE WIP-DRAINMAST-FWD1DUB06
** ON A/C NOT FOR ALL
2000VUDRAINMAST-FWD1DUB03
** ON A/C NOT FOR ALL
2000VUWASTE WIP-DRAINMAST-FWD1DUB03
** ON A/C ALL
2001VUWASTE WIP-DRAINMAST-AFT11DUE01
** ON A/C NOT FOR ALL
2001VUWASTE WIP-DRAINMAST-MID21DUE02
Subtask 30-71-51-860-052-A
B. Aircraft Maintenance Configuration
   (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
Subtask 30-71-51-410-054-A
C. Close Access
   (1) Remove the access platform.
[Rev.10 from 2021] 2026.04.01 00:32:02 UTC