Removal of the Flap and Slat Control Lever
TASK 27-51-43-000-001-A
Removal of the Flap and Slat Control Lever
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 27-51-43-860-050-A
Subtask 27-51-43-020-050-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 06:03:14 UTC
Removal of the Flap and Slat Control Lever
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
ZONE: 210
1. Reason for the JobSelf Explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | CAP - BLANKING |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| REFERENCE | DESIGNATION |
|---|---|
| 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 31-35-22-000-001-A | Removal of the Printer |
Subtask 27-51-43-860-050-A
A. Aircraft Maintenance Configuration
(1) Make sure that the flaps and slats are in the fully retracted position (Ref. AMM TASK 27-50-00-866-009).
(2) Make sure that the hydraulic systems are depressurized.
Subtask 27-51-43-865-050-A (1) Make sure that the flaps and slats are in the fully retracted position (Ref. AMM TASK 27-50-00-866-009).
(2) Make sure that the hydraulic systems are depressurized.
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/SLT FLP/POS/IND 1 | 1CN | B12 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SLT FLP/POS/IND 1 | 1CN | B07 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 105VU | ELEC/HOT BUS/702PP SPLY | 5PB2 | D02 |
| 105VU | ELEC/HOT BUS/701PP SPLY | 5PB1 | D01 |
| 105VU | ELEC/HOT BUS/702PP SPLY | 12PB2 | E02 |
| 105VU | ELEC/HOT BUS/701PP SPLY | 12PB1 | E01 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FLIGHT CONTROLS/SLT FLP/2POS/IND | 2CN | P16 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FLIGHT CONTROLS/SLT FLP/2POS/IND | 2CN | P21 |
| ** ON A/C ALL | |||
| 122VU | LIGHTING/INSTL LT/MAIN INST/PNL AND/PED | 4LF | Y04 |
Subtask 27-51-43-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the Flap and Slat Control Lever
(1) Remove the screws (1) and the washers (2).
(2) Lift the control lever assembly (9).
(3) Disconnect the electrical connector (8) from the control lever assembly (9).
(a) If necessary, remove the printer (Ref. AMM TASK 31-35-22-000-001).
(5) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(6) Cut and discard the lockwire from the screws (3).
(7) Remove the screws (3) and the washers (4).
(8) Remove the control lever assembly (9).
Subtask 27-51-43-020-050-B ** ON A/C NOT FOR ALL (1) Remove the screws (1) and the washers (2).
(2) Lift the control lever assembly (9).
(3) Disconnect the electrical connector (8) from the control lever assembly (9).
(a) If necessary, remove the printer (Ref. AMM TASK 31-35-22-000-001).
NOTE: If you need more space to disconnect the electrical connector(s) from the control lever assembly or the CSU, you can remove the printer.
(4) Disconnect the electrical connector (7) and (6) from the Command Sensor Unit (CSU) (5). (5) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(6) Cut and discard the lockwire from the screws (3).
(7) Remove the screws (3) and the washers (4).
(8) Remove the control lever assembly (9).
A. Removal of the Flap and Slat Control Lever
(1) Remove the screws (1) and the washers (2).
(2) Lift the control lever assembly (9).
(3) Disconnect the electrical connector (8) from the control lever assembly (9).
(a) If necessary, remove the printer (Ref. AMM TASK 31-35-22-000-001).
(5) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(6) Cut and discard the lockwire from the screws (3),(10).
(7) Remove the screws (3), (10) and the washers (4).
(8) Remove the control lever assembly (9).
(1) Remove the screws (1) and the washers (2).
(2) Lift the control lever assembly (9).
(3) Disconnect the electrical connector (8) from the control lever assembly (9).
(a) If necessary, remove the printer (Ref. AMM TASK 31-35-22-000-001).
NOTE: If you need more space to disconnect the electrical connector(s) from the control lever assembly or the CSU, you can remove the printer.
(4) Disconnect the electrical connector (7) and (6) from the CSU (5). (5) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(6) Cut and discard the lockwire from the screws (3),(10).
(7) Remove the screws (3), (10) and the washers (4).
(8) Remove the control lever assembly (9).
Flap and Slat Control - Lever