W DOC AIRBUS | AMM A320F

Installation of the Wingrip


TASK 12-00-00-481-002-A
Installation of the Wingrip


WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
WARNING: YOU MUST PUT ON AND ATTACH A SAFETY HARNESS BEFORE YOU START WORK:
  • ON THE THS OR IN THE REAR FUSELAGE
  • ON TOP OF THE WINGS OR PYLONS.
WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
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
WARNING NOTICE(S)
15318-00
2
WINGRIP
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
98D27803500001
1
LOCKING TOOL ZERO POS
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 27-00-00-080-002-A
Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 27-00-00-480-002-A
Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 27-50-00-866-009-A
Retraction of the Flaps on the Ground
TASK 27-50-00-866-009-A-01
Retraction of the Flaps/Slats on the Ground
TASK 27-80-00-866-005-A
Retracting the Slats on the Ground
F Installation of the Wingrip ** ON A/C NOT FOR ALL
F Installation of the Wingrip ** ON A/C NOT FOR ALL
F Installation of the Wingrip ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 12-00-00-866-051-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the flaps and the slats are retracted (Ref. AMM TASK 27-50-00-866-009) (Ref. AMM TASK 27-80-00-866-005).
Subtask 12-00-00-941-061-A
B. Safety Precautions
   (1) Put a WARNING NOTICE(S) in the cockpit to tell persons not to operate the flap and slat control lever.
   (2) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (Ref. AMM TASK 27-00-00-480-002) or 98D27803500001 LOCKING TOOL ZERO POS on the flap and slat control lever.
Subtask 12-00-00-010-052-A
C. Get Access
   (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the wing.
4. Procedure
Subtask 12-00-00-481-052-A
A. Installation of the 15318-00 WINGRIP
F Installation of the Wingrip ** ON A/C NOT FOR ALL
F Installation of the Wingrip ** ON A/C NOT FOR ALL
F Installation of the Wingrip ** ON A/C NOT FOR ALL
WARNING: INSTALL THE VACUUM PADS OF THE WINGRIP SYSTEM ON THE AREA OF THE WING WHERE YOU CAN WALK. BEFORE YOU PUT THE VACUUM PAD IN POSITION, MAKE SURE THAT THERE IS NO DIRT, OIL, SHARP OBJECTS, WATER OR OTHER CONTAMINATION. PUT THE VACUUM PAD IN POSITION AS FAR AS POSSIBLE FROM THE EDGES OF THE WORK AREA (NOT ADJACENT TO JOINTS AND/OR PROUD-HEADED RIVETS/SCREWS). IF THE VACUUM PADS ARE NOT INSTALLED CORRECTLY, YOU CAN FALL FROM THE WING, WHICH CAN CAUSE YOU INJURY OR KILL YOU.
   (1) Refer to the Wingrip manufacturer's instructions for the installation of the Wingrip system.
NOTE: Only personnel with special training are permitted to install/use the Wingrip system.
     (a) The Wingrip system includes the individual pad system or the multi-pad system:
       1 Individual pad system
The individual pad system contains a Wingrip single-point anchor (5) installed on the wing in an area near the work area. A primary hose (2) connects the Wingrip single-point anchor (5) to the vacuum module (1). The body harness (3) is attached to the Wingrip single-point anchor with the double lanyard (4).
       2 Multi-pad system
The multi-pad system contains two Wingrip end anchors (8). A primary hose (7) connects the anchor (8) to the vacuum module (6). The multi-pad system also contains Wingrip intermediate anchors (9) and secondary hoses (13) (the quantity is related to the system length). The body harness (10) (one for each user) is attached to the Wingrip shuttle (12) with the double lanyard (11).
5. Close-up
Subtask 12-00-00-081-053-A
A. Removal of the 15318-00 WINGRIP
F Installation of the Wingrip ** ON A/C NOT FOR ALL
F Installation of the Wingrip ** ON A/C NOT FOR ALL
F Installation of the Wingrip ** ON A/C NOT FOR ALL
   (1) Refer to the Wingrip manufacturer's instructions for removal of the Wingrip individual pad system or the Wingrip multi-pad system.
Subtask 12-00-00-942-056-A
B. Put the aircraft back to its initial configuration.
   (1) Remove the access platform(s).
   (2) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (Ref. AMM TASK 27-00-00-080-002) or 98D27803500001 LOCKING TOOL ZERO POS.
   (3) Remove the WARNING NOTICE(S).
   (4) Make sure that the work area is clean and clear of tools and other items.
[Rev.10 from 2021] 2026.04.01 12:38:22 UTC