Removal of the Secondary Hinged Fairing
TASK 32-12-13-000-001-A
Removal of the Secondary Hinged Fairing
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 32-12-13-941-050-A
Subtask 32-12-13-020-050-A
(2) Remove the nut (5), the bolt (7) and the bonding tag (6).
(3) Remove the nuts (9) and the bolts (10).
(4) Carefully remove the secondary hinged fairing (2). If necessary, use a WEDGE - NON METALLIC to loosen the seal to release the secondary hinged fairing.
(5) Loosely attach the nuts (5) and (9) and the bolts (7) and (10) to the secondary hinged fairing (2).
[Rev.10 from 2021]
2026.04.01 12:29:59 UTC
Removal of the Secondary Hinged Fairing
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT) |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| No specific | 1 | WEDGE - NON METALLIC |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
| TASK 32-00-00-860-001-A | Flight Configuration Precautions with Electrical Power |
| TASK 32-00-00-860-001-A-01 | Flight Configuration Precautions without Electrical Power |
| TASK 32-12-14-000-001-A | Removal of the MLG Fixed Fairing Assembly |
Subtask 32-12-13-941-050-A
A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Make sure that the ground safety locks are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
(5) Put a WARNING NOTICE(S) at the ground door opening panel, to tell persons not to operate the landing gear doors.
Subtask 32-12-13-869-052-A (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Make sure that the ground safety locks are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
- Make sure that the landing-gear control-lever is in the DOWN position
- Put a WARNING NOTICE(S) in the cockpit to tell persons not to operate the landing gear.
(5) Put a WARNING NOTICE(S) at the ground door opening panel, to tell persons not to operate the landing gear doors.
B. Flight Configuration Precautions
(1) If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.
(2) If the electrical power is necessary, do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.
Subtask 32-12-13-865-050-A (1) If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.
(2) If the electrical power is necessary, do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.
C. Open, safety and tag this(these) circuit breaker(s):
Subtask 32-12-13-010-053-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
D. Get Access
(1) Put an ACCESS PLATFORM 3M (10 FT) below the applicable zone:
4. Procedure(1) Put an ACCESS PLATFORM 3M (10 FT) below the applicable zone:
- For the left wing, below zone 733
- For the right wing, below zone 743.
- If a replacement secondary hinged-fairing is installed
- If an adjustment of the secondary hinged fairing is necessary.
NOTE: If you remove the secondary hinged fairing for access only, it is not necessary to remove the fixed fairing.
Subtask 32-12-13-020-050-A
CAUTION:
HOLD THE SECONDARY HINGED FAIRING OR IT WILL BECOME DAMAGED.
A. Removal of the Secondary Hinged Fairing NOTE: If the same hinged fairing is installed, you must not move the actuating rod (3) locknuts. If you move the actuating rod, the hinged fairing adjustment will change.
(1) Remove and discard the cotter pins (4) and (8). (2) Remove the nut (5), the bolt (7) and the bonding tag (6).
(3) Remove the nuts (9) and the bolts (10).
(4) Carefully remove the secondary hinged fairing (2). If necessary, use a WEDGE - NON METALLIC to loosen the seal to release the secondary hinged fairing.
(5) Loosely attach the nuts (5) and (9) and the bolts (7) and (10) to the secondary hinged fairing (2).
Secondary Hinged Fairing