W DOC AIRBUS | AMM A320F

Detailed Inspection of Vertical Stabilizer, Center Box, Internal Structure as far as Visible, Front Spar Forward Face and Upper Closing Rib, Upper Surface

TASK 55-30-00-200-001-A
Detailed Inspection of Vertical Stabilizer, Center Box, Internal Structure as far as Visible, Front Spar Forward Face and Upper Closing Rib, Upper Surface

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
ZONE: 321
ZONE: 322
ZONE: 323
ZONE: 324
1. Reason for the Job
Refer to the MPD TASK: 553003-01
DETAILED INSPECTION OF VERTICAL STABILIZER, CENTER BOX, INTERNAL STRUCTURE AS FAR AS VISIBLE, FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB, UPPER SURFACE
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.05RAB9)
Adhesive Film Tape-- Aluminium Foil -
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
321
DORSAL FIN
322
VERTICAL STABILIZER LEADING EDGE
323
VERTICAL STABILIZER SPAR BOX
324
VERTICAL STABILIZER TIP
325BL, 325BR, 325CL, 325CR, 325DL, 325EL, 325ER
321AL, 325AL, 325AR, 325FR, 325GR
325DR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 53-45-11-000-001-A
Removal of the Dorsal Fin
TASK 53-45-11-400-001-A
Installation of the Dorsal Fin
TASK 53-55-12-000-001-A
Removal of the Rudder Fairings
TASK 53-55-12-400-001-A
Installation of the Rudder Fairings
TASK 55-32-11-000-001-A
Removal of the Vertical Stabilizer Leading-Edge
TASK 55-32-11-400-001-A
Installation of the Vertical Stabilizer Leading-Edge
TASK 55-33-13-010-002-A
Opening/Removal of the Trailing Edge Access-Panels of the Vertical Stabilizer
TASK 55-33-13-410-002-A
Closing/Installation of the Trailing Edge Access-Panels of the Vertical Stabilizer
TASK 55-34-11-000-001-A
Removal of the Vertical Stabilizer Tip
TASK 55-34-11-400-001-A
Installation of the Vertical Stabilizer Tip
SRM 553100
F Vertical-Stabilizer Spar-Box - Inspection Area
3. Job Set-up
Subtask 55-30-00-860-055-A
A. Aircraft Maintenance Configuration
   (1) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. AMM TASK 29-00-00-864-001).
   (2) Put the WARNING NOTICE(S) in the cockpit to tell persons not to operate the flight controls.
   (3) Put the ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE in position at Zone 320.
Subtask 55-30-00-865-050-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUAUTO FLT/RUDDER/TRIM/IND15CCM20
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
Subtask 55-30-00-010-052-B ** ON A/C NOT FOR ALL
C. Get Access
   (1) Remove the vertical stabilizer tip (Ref. AMM TASK 55-34-11-000-001).
   (2) Remove the leading edge of the vertical stabilizer (Ref. AMM TASK 55-32-11-000-001).
   (3) Remove the dorsal fin 321AL (Ref. AMM TASK 53-45-11-000-001).
   (4) Remove the fairings 325AL and 325AR (Ref. AMM TASK 53-55-12-000-001).
   (5) Open and safety the access panels 325BL 325CL 325DL 325BR 325CR (Ref. AMM TASK 55-33-13-010-002).
   (6) Remove the access panels 325EL 325ER 325DR (Ref. AMM TASK 55-33-13-010-002).
   (7) Remove the peelable hole covers from the lighting holes at the spars.
Subtask 55-30-00-010-052-C ** ON A/C NOT FOR ALL
C. Get Access
   (1) Remove the vertical stabilizer tip (Ref. AMM TASK 55-34-11-000-001).
   (2) Remove the leading edge of the vertical stabilizer (Ref. AMM TASK 55-32-11-000-001).
   (3) Remove dorsal fin 321AL (Ref. AMM TASK 53-45-11-000-001).
   (4) Remove rudder fairings 325AL and 325AR (Ref. AMM TASK 53-55-12-000-001).
   (5) Open and safety access panels 325BL, 325CL, 325DL, 325BR and 325CR (Ref. AMM TASK 55-33-13-010-002).
   (6) Remove access panels 325EL, 325ER, 325FR and 325GR (Ref. AMM TASK 55-33-13-010-002).
   (7) Remove the peelable hole covers from the lighting holes at the spars.
4. Procedure
Subtask 55-30-00-210-050-A
A. Inspection
   (1) Do a visual inspection of the vertical stabilizer center box internal structure as far as visible, the front spar FWD face and the upper closing rib upper structure.
   (2) If you find damage, look for the limits SRM 553100.
5. Close-up
Subtask 55-30-00-865-051-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
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUAUTO FLT/RUDDER/TRIM/IND15CCM20
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
Subtask 55-30-00-410-054-B ** ON A/C NOT FOR ALL
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the peelable hole covers as follows:
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
     (a) For each lightening hole, cut a piece of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with 20 mm (0.7874 in.) of excess of the hole dimension to make the peelable hole covers.
     (b) Clean the adjacent area of the lightening holes with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) until contamination is removed. Do not let cleaning agent dry on the surfaces.
     (c) Install the peelable hole covers on the lightening holes.
   (3) Close the access panels 325BL 325CL 325DL 325BR 325CR (Ref. AMM TASK 55-33-13-410-002).
   (4) Install the access panels 325EL 325ER 325DR (Ref. AMM TASK 55-33-13-410-002).
   (5) Install the fairings 325AL and 325AR (Ref. AMM TASK 53-55-12-400-001).
   (6) Install the vertical stabilizer tip (Ref. AMM TASK 55-34-11-400-001).
   (7) Install the leading edge (Ref. AMM TASK 55-32-11-400-001).
   (8) Install the dorsal fin 321AL (Ref. AMM TASK 53-45-11-400-001).
   (9) Remove the access platform(s).
   (10) Remove the WARNING NOTICE(S).
   (11) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Subtask 55-30-00-410-054-C ** ON A/C NOT FOR ALL
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the new peelable hole covers as follows:
     (a) Clean the adjacent area of the lightening holes with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) . Do not let cleaning agent dry on the surfaces.
     (b) For each lightening hole, cut a piece of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with a diameter of 20 mm (0.7874 in.) larger than the diameter of the lightening hole.
     (c) Install the new peelable hole covers on the lightening holes.
   (3) Close access panels 325BL, 325CL, 325DL, 325BR and 325CR (Ref. AMM TASK 55-33-13-410-002).
   (4) Install access panels 325EL, 325ER, 325FR and 325GR (Ref. AMM TASK 55-33-13-410-002).
   (5) Install rudder fairings 325AL and 325AR (Ref. AMM TASK 53-55-12-400-001).
   (6) Install dorsal fin 321AL (Ref. AMM TASK 53-45-11-400-001).
   (7) Install the leading edge of the vertical stabilizer (Ref. AMM TASK 55-32-11-400-001).
   (8) Install the vertical stabilizer tip (Ref. AMM TASK 55-34-11-400-001).
   (9) Remove the access platform(s).
   (10) Remove the WARNING NOTICE(S).
   (11) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 02:05:43 UTC
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