W DOC AIRBUS | AMM A320F

Removal of the Access Panel

TASK 57-27-11-000-001-A
Removal of the Access Panel

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.
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 5M (16 FT)- ADJUSTABLE
No specific
1
LABEL - IDENTIFICATION
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WARNING NOTICE(S)
98A53003500000
1
REMOVAL TOOL OF PHILLIPS TORQUE
98A57304002000
1
EXTRACTION, MANHOLE BOLT
98D27803500001
1
LOCKING TOOL ZERO POS
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 28-10-00-910-001-A
Safety Procedures When You Do Work in a Fuel Tank
TASK 28-10-00-910-002-A
Access to the Fuel Tanks and the Work Areas
TASK 28-25-00-650-001-A
Pressure Defuel
TASK 28-25-00-650-003-A
To Drain Remaining Fuel from the Wing Tanks and the Center Tank
TASK 28-25-00-650-003-A-01
To Drain Remaining Fuel from the Wing Tanks and the Center Tank
TASK 57-27-11-300-001-A
Repair of the Outer Wing - SPF Access Panels
TASK 57-55-11-000-001-A
Removal of the Flap Track Fairings Nos. 2, 3 and 4
TASK 57-55-11-000-004-A
Removal of the Flap Track Fairings Nos. 2, 3 and 4
F Access Panels - Rib 2 to Rib 13
F Access Panels - Rib 2 to Rib 13 Bolt Removal/Tightening Sequence ** ON A/C NOT FOR ALL
F Access Panels - Rib 2 to Rib 13 Bolt Removal/Tightening Sequence ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 57-27-11-941-050-A
A. Safety Precautions
WARNING: BEFORE YOU DO WORK IN OR NEAR A FUEL TANK, MAKE SURE THAT YOU OBEY ALL THE SAFETY PROCEDURES. THIS WILL PREVENT INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
   (1) You must obey the fuel safety procedures when you do work in a fuel tank, (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-002).
   (2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
   (3) Put the WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
   (4) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
Subtask 57-27-11-860-054-A
B. Aircraft Maintenance Configuration
   (1) Defuel the applicable fuel tank (Ref. AMM TASK 28-25-00-650-001).
   (2) Drain the remaining fuel from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
Subtask 57-27-11-865-050-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFUEL/XFR VALVE1/WING/R2QPA11
49VUFUEL/XFR VALVE1/WING/L1QPA10
** ON A/C ALL
49VUFUEL/X FEED/VALVE/MOT12QEA12
** ON A/C NOT FOR ALL
121VUFUEL/CTR TK/PUMP2 SPLY30QAP26
121VUFUEL/CTR TK/PUMP1 SPLY29QAP23
** ON A/C NOT FOR ALL
121VUFUEL/RFL/DFL/SPLY2QUL24
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL23
** ON A/C ALL
121VUFUEL/L WING TK/PUMP2 SPLY7QAN26
121VUFUEL/L WING TK/PUMP1 SPLY1QAN23
121VUFUEL/R WING TK/PUMP2 SPLY8QAQ26
121VUFUEL/R WING TK/PUMP1 SPLY2QAQ23
** ON A/C NOT FOR ALL
121VUFUEL/RFL/DFL/SPLY2QUL23
121VUFUEL/RFL/DFL/XFR/DEFUEL/VALVE1QUL22
Subtask 57-27-11-010-054-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the applicable access panel:
   (2) Remove the forward and aft fixed fairings of the No. 3 flap track (Ref. AMM TASK 57-55-11-000-001):
Subtask 57-27-11-010-054-B ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the applicable access panel:
   (2) Remove the forward and aft fixed fairings of the No. 3 flap track (Ref. AMM TASK 57-55-11-000-004):
4. Procedure
Subtask 57-27-11-020-050-A
A. Removal of the Access Panel
CAUTION: YOU MUST REMOVE AND INSTALL THE BOLTS IN THE SPECIFIED SEQUENCE. THIS WILL PREVENT DAMAGE TO THE ACCESS PANEL.
   (1) To remove the PRE modification 30100J2130 panels:
     (a) If you cannot remove the applicable bolt(s) (6), (17) and (28) easily, use the 98A53003500000 REMOVAL TOOL OF PHILLIPS TORQUE or the 98A57304002000 EXTRACTION, MANHOLE BOLT.
     (b) Remove the applicable bolt(s) (6), (17) and (28) in the sequence AF thru A.
     (c) Remove the applicable clamp ring(s) (5), (16) and (27) and the applicable knitted gasket(s) (4), (15) and (26).
     (d) Remove the applicable access panel(s) (1), (12) and (23).
     (e) Identify the applicable removed access panel(s) (1), (12) and (23) with a LABEL - IDENTIFICATION.
   (2) To remove the POST modification 30100J2130 panels:
     (a) If you cannot remove the applicable bolt(s) (11), (22) and (33) easily, use the 98A53003500000 REMOVAL TOOL OF PHILLIPS TORQUE or the 98A57304002000 EXTRACTION, MANHOLE BOLT.
     (b) Remove the applicable bolt(s) (11), (22) and (33) in the sequence AF thru A.
     (c) Remove the applicable outer access panel(s) (10), (21) and (32) and the applicable knitted gasket(s) (9), (20) and (31).
     (d) Remove the applicable access panel(s) (7), (18) and (29).
     (e) Identify the applicable removed access panel(s) (7), (18) and (29) with a LABEL - IDENTIFICATION.
Subtask 57-27-11-210-069-A ** ON A/C NOT FOR ALL
B. Inspection of the Lower Wing Tank Access Panels for Fluid Ingress
   (1) Examine the lower wing tank access panels:
     (a) Look for signs of:
  • fluid leakage at the panel side plug
  • fluid leakage at the panel rivnuts.
     (b) Weigh the panel to make sure that it is not heavier than its nominal weight. The nominal weights of the panels are given in the table that follows:
PANEL TYPE
PART NUMBER
NOMINAL WEIGHT (kg) +/- 0.100kg
Type 23R
D572 51360 000
D572 51360 002
1.58
Type 24
D572 51306 000
D572 51306 002
1.10
NOTE: If a panel weighs more than the value given in the table, repair the panels that have fluid ingress (Ref. AMM TASK 57-27-11-300-001).
[Rev.10 from 2021] 2026.04.01 02:11:49 UTC
"Aviabrain" 2025