Removal of the Control Handle
TASK 38-14-49-000-005-A
Removal of the Control Handle
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 38-14-49-861-053-A Subtask 38-14-49-680-057-A Subtask 38-14-49-010-059-A
Subtask 38-14-49-020-053-A
[Rev.10 from 2021]
2026.04.02 06:25:46 UTC
Removal of the Control Handle
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 1M(3 FT) |
| No specific | AR | ACCESS PLATFORM 2M (6 FT) |
| No specific | AR | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | AR | ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 131EF, 131FF, 131GF, 133AL, 171AL, 825, 832, 842 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-42-00-861-001-A | Energize the Ground Service Network from the External Power |
| TASK 38-10-00-614-002-A | Depressurization of the Potable Water System |
| TASK 52-10-00-010-001-A | Opening of the Passenger/Crew Door |
| TASK 52-30-00-860-001-A | Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
Subtask 38-14-49-861-053-A Subtask 38-14-49-680-057-A Subtask 38-14-49-010-059-A
C. Get Access
(1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position in front of the applicable passenger/crew door 832 or 842.
(2) Open passenger/crew door 832 or 842 (Ref. AMM TASK 52-10-00-010-001).
(3) Put an ACCESS PLATFORM 1M(3 FT) in position at drain panel 133AL.
(4) Open drain panel 133AL.
(5) Put the WARNING NOTICE(S) in position in the drain panel to tell persons not to turn the control handle.
(6) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at service panel 2023VU.
(7) Open access door 171AL of service panel 2023VU.
(8) Put the WARNING NOTICE(S) in position in service panel 2023VU to tell persons not to turn the control handle.
(9) Put an ACCESS PLATFORM 2M (6 FT) in position at forward cargo-compartment door 825.
(10) Open forward cargo-compartment door 825 (Ref. AMM TASK 52-30-00-860-001).
(11) Set cargo-compartment light switch 6LU to ON.
(12) In the forward cargo-compartment, remove floor panels 131EF 131FF 131GF.
Subtask 38-14-49-865-059-A (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position in front of the applicable passenger/crew door 832 or 842.
(2) Open passenger/crew door 832 or 842 (Ref. AMM TASK 52-10-00-010-001).
(3) Put an ACCESS PLATFORM 1M(3 FT) in position at drain panel 133AL.
(4) Open drain panel 133AL.
(5) Put the WARNING NOTICE(S) in position in the drain panel to tell persons not to turn the control handle.
(6) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at service panel 2023VU.
(7) Open access door 171AL of service panel 2023VU.
(8) Put the WARNING NOTICE(S) in position in service panel 2023VU to tell persons not to turn the control handle.
(9) Put an ACCESS PLATFORM 2M (6 FT) in position at forward cargo-compartment door 825.
(10) Open forward cargo-compartment door 825 (Ref. AMM TASK 52-30-00-860-001).
(11) Set cargo-compartment light switch 6LU to ON.
(12) In the forward cargo-compartment, remove floor panels 131EF 131FF 131GF.
D. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 124VU | SVCE/601PP/602PP/SPLY | 1PX | BB01 |
Subtask 38-14-49-020-053-A
A. Remove the Control Rod
(2) Remove the pin (1) and disengage the clevis (2).
(3) Remove the nut (10), the lever (9) and at the same time from the outside of the aircraft hold the bolt (5) and the handle (6).
(4) Remove the bolt (5), the handle (6) and the bush (8) from the bearing assy (7).
NOTE: Two mechanics are necessary to do these operations.
(1) Remove the washer (3) and remove and discard the cotter pin (4). - One mechanic in the FWD cargo compartment.
- One mechanic outside the aircraft.
(2) Remove the pin (1) and disengage the clevis (2).
(3) Remove the nut (10), the lever (9) and at the same time from the outside of the aircraft hold the bolt (5) and the handle (6).
(4) Remove the bolt (5), the handle (6) and the bush (8) from the bearing assy (7).
Control Handle