W DOC AIRBUS | AMM A320F

Removal of the Free-Fall Control-Handle Assembly


TASK 32-33-11-000-001-A
Removal of the Free-Fall Control-Handle Assembly


1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98A27801001000
1
RIGGING PIN
98A27901002000
1
PIN-RIGGING,RUDDER CONTROL
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
822
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 31-35-22-000-001-A
Removal of the Printer
TASK 32-00-00-481-001-A
Installation of the Safety Devices on the Landing Gears
TASK 32-22-00-010-001-A
Nose Gear Doors - Ground Doors Opening
3. Job Set-up
Subtask 32-33-11-941-050-A
A. Safety Precautions
   (1) In the cockpit, on the panel 400VU put WARNING NOTICE(S) in position to tell persons not to operate the landing gear control lever.
   (2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
Subtask 32-33-11-865-050-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C NOT FOR ALL
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
121VUAUTO FLT/RUDDER/TRIM/IND15CCM20
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
122VULIGHTING/INSTL LT/MAIN INST/PNL AND/PED4LFY04
Subtask 32-33-11-010-050-A
C. Get access to the NLG free-fall extension mechanical system
   (1) Open the nose landing-gear doors (Ref. AMM TASK 32-22-00-010-001).
   (2) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position in zone 123.
   (3) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position below the lateral avionics-compartment door 822.
   (4) Open the lateral avionics-compartment door 822.
Subtask 32-33-11-480-050-A
D. Installation of Rigging Pins
   (1) Put the 98A27901002000 PIN-RIGGING,RUDDER CONTROL (26) in position on the lower bellcrank (27).
   (2) Put the 98A27801001000 RIGGING PIN (20) in position on the cable quadrant (21).
Subtask 32-33-11-010-052-B
E. Get access to the control handle
   (1) In the cockpit, turn by a quarter turn the fasteners (2) of the panels (1) and (3).
   (2) Remove the panels (1) and (3) from their housings.
   (3) Remove the printer (5) (Ref. AMM TASK 31-35-22-000-001).
   (4) Remove the screws (7), the nuts (4), the washers (11) and the bushes (10).
   (5) Loosen the screws (9) and move the casing (8) at an angle.
4. Procedure
Subtask 32-33-11-020-050-A
A. Removal of the Control Handle
   (1) Remove the screws (6) and (12).
   (2) Lift the panel (13), disconnect the plugs (14) and remove the panel (13).
   (3) Remove the handle assembly (15) from its housing.
[Rev.10 from 2021] 2026.04.01 00:46:25 UTC