Removal of the Pedal Position Transducer Unit
TASK 27-92-15-000-001-A
Removal of the Pedal Position Transducer Unit
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 27-92-15-860-050-A
Subtask 27-92-15-020-050-A
[Rev.10 from 2021]
2026.03.31 23:58:35 UTC
Removal of the Pedal Position Transducer Unit
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 | CAP - BLANKING |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| 98A27901002000 | 1 | PIN-RIGGING,RUDDER CONTROL |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 121 | AVIONICS COMPARTMENT |
| 122 | AVIONICS COMPARTMENT |
| 811, 822 |
| REFERENCE | DESIGNATION |
|---|---|
Subtask 27-92-15-860-050-A
A. Aircraft Maintenance Configuration
(1) Put a WARNING NOTICE(S) to tell persons not to operate the pedals.
(2) On the panel 110VU, put a WARNING NOTICE(S) to tell persons not to use the rudder trim.
(3) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 811.
(4) Open the access door 811.
(5) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
(6) Open the access door 822.
(7) On the battery power center 105VU:
Subtask 27-92-15-865-050-A (1) Put a WARNING NOTICE(S) to tell persons not to operate the pedals.
(2) On the panel 110VU, put a WARNING NOTICE(S) to tell persons not to use the rudder trim.
(3) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 811.
(4) Open the access door 811.
(5) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
(6) Open the access door 822.
(7) On the battery power center 105VU:
- loosen the two screws and remove the protective cover.
B. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| ** ON A/C ALL | |||
| 105VU | FLIGHT CONTROLS/ELAC2/STBY SPLY | 16CE2 | A02 |
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
Subtask 27-92-15-020-050-A
A. Removal of the Transducer Unit
(1) Disconnect the electrical connectors (13) and (14) from the transducer unit (12).
(2) Put CAP - BLANKING on the electrical connectors (13) and (14) and on the electrical connectors of the transducer unit (12).
(3) Remove and discard the cotter pin (8) remove the nut (7) and the washer (6).
(4) Remove the bolt (2) and disconnect the rod (5).
(5) Remove and discard the cotter pins (16) remove the nuts (15) and the washers (17).
(6) Remove the bolts (1) and remove the transducer unit (12).
(1) Disconnect the electrical connectors (13) and (14) from the transducer unit (12).
(2) Put CAP - BLANKING on the electrical connectors (13) and (14) and on the electrical connectors of the transducer unit (12).
(3) Remove and discard the cotter pin (8) remove the nut (7) and the washer (6).
(4) Remove the bolt (2) and disconnect the rod (5).
(5) Remove and discard the cotter pins (16) remove the nuts (15) and the washers (17).
(6) Remove the bolts (1) and remove the transducer unit (12).
Pedal Position Transducer Unit