Installation of the Throttle Control Lever Assembly [PW11]
TASK 76-11-41-400-802-A
Installation of the Throttle Control Lever Assembly
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 76-11-41-860-053-A ** ON A/C NOT FOR ALL
Subtask 76-11-41-420-060-A ** ON A/C NOT FOR ALL
Subtask 76-11-41-410-058-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 12:32:47 UTC
Installation of the Throttle Control Lever Assembly
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | AR | WARNING NOTICE(S) |
| No specific | Torque wrench: range to between 4 and 3 m.daN (29.50 and 22.12 lbf.ft ) ![]() | |
| 98DNSA20208120 | 1 | RIGGING PIN |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.05ABF1) | Retaining adhesive-Cylindrical fitting Medium strength Low viscosity - |
| (Material No.05BAE1) | Threadlocking Adhesive-- Medium strength - |
| (Material No.14QFB1) | Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 811 |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 86 | LIGHTED LABEL | AIPC 33-13-88-03-110 |
| 30 | COTTER PINS | AIPC 76-11-81-01-010 |
| 49 | ADJUSTMENT BUSHING | AIPC 76-11-81-01-130 |
| 43 | COTTER PINS | AIPC 76-11-81-01-230 |
| 72 | COTTER PINS | AIPC 76-11-81-01-230 |
| 40 | BEARING | AIPC 76-11-81-01-300 |
| 48 | BEARING | AIPC 76-11-81-01-300 |
| 50 | BEARING | AIPC 76-11-81-01-300 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 22-82-12-000-001-A | Removal of the Multipurpose Control & Display Unit (MCDU) |
| TASK 22-82-12-400-002-A | Installation of the Multipurpose Control & Display Unit (MCDU) |
| TASK 22-96-00-710-001-A | Operational Test of the AFS |
| TASK 22-97-00-710-001-A | Operational Test of the LAND CAT III Capability |
| TASK 23-13-13-000-001-A | Removal of the Radio Management Panel (RMP) |
| TASK 23-13-13-400-001-A | Installation of the Radio Management Panel (RMP) |
| TASK 23-51-12-000-001-A | Removal of the Audio Control Panel (ACP) |
| TASK 23-51-12-400-001-A | Installation of the Audio Control Panel (ACP) |
| TASK 27-41-41-400-001-A | Installation of the Control Mechanism-Pitch Trim |
| TASK 34-41-12-000-001-A | Removal of the Weather-Radar Control Unit |
| TASK 34-41-12-400-001-A | Installation of the Weather-Radar Control Unit |
| TASK 34-52-12-000-001-A | Removal of the ATC/TCAS Control Unit |
| TASK 34-52-12-400-001-A | Installation of the ATC/TCAS Control Unit |
| TASK 71-00-00-860-832-A | Procedure to Prevent Engine Motoring and to Stop the Electrical Supply to the EEC |
| TASK 73-25-34-400-802-A | Installation of the Engine Interface Unit (EIU) |
Subtask 76-11-41-860-053-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) Make sure that the WARNING NOTICE(S) is in position in the cockpit to tell persons not to move the slat and flap control lever.
(2) Make sure that you did the procedure to prevent engine motoring and to stop the electrical supply to the Electronic Engine Control (EEC)
(Ref. AMM TASK 71-00-00-860-832)
(3) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position.
(4) Make sure that access door 811 is open.
(5) Make sure that the Multipurpose Control and Display Units (MCDUs) (3CA1, 3CA2) (Ref. AMM TASK 22-82-12-000-001) are removed.
(6) Make sure that the Radio Management Panels (RMPs) (1RG1, 1RG2) (Ref. AMM TASK 23-13-13-000-001) are removed.
(7) Make sure that the Audio Control Panels (ACPs) (2RN1, 2RN2) (Ref. AMM TASK 23-51-12-000-001) are removed.
(8) Make sure that the weather radar control unit (3SQ) (Ref. AMM TASK 34-41-12-000-001) is removed.
(9) Make sure that the ATC/TCAS control unit (3SH) (Ref. AMM TASK 34-52-12-000-001) is removed.
(10) Make sure that the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU are removed.
(11) Make sure that the throttle control levers are at idle (0 deg. TLA).
(12) Make sure that the 98DNSA20208120 RIGGING PIN (11) is installed in the artificial feel unit.
Subtask 76-11-41-865-063-A ** ON A/C NOT FOR ALL (1) Make sure that the WARNING NOTICE(S) is in position in the cockpit to tell persons not to move the slat and flap control lever.
(2) Make sure that you did the procedure to prevent engine motoring and to stop the electrical supply to the Electronic Engine Control (EEC)
(Ref. AMM TASK 71-00-00-860-832)
(3) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position.
(4) Make sure that access door 811 is open.
(5) Make sure that the Multipurpose Control and Display Units (MCDUs) (3CA1, 3CA2) (Ref. AMM TASK 22-82-12-000-001) are removed.
(6) Make sure that the Radio Management Panels (RMPs) (1RG1, 1RG2) (Ref. AMM TASK 23-13-13-000-001) are removed.
(7) Make sure that the Audio Control Panels (ACPs) (2RN1, 2RN2) (Ref. AMM TASK 23-51-12-000-001) are removed.
(8) Make sure that the weather radar control unit (3SQ) (Ref. AMM TASK 34-41-12-000-001) is removed.
(9) Make sure that the ATC/TCAS control unit (3SH) (Ref. AMM TASK 34-52-12-000-001) is removed.
(10) Make sure that the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU are removed.
(11) Make sure that the throttle control levers are at idle (0 deg. TLA).
(12) Make sure that the 98DNSA20208120 RIGGING PIN (11) is installed in the artificial feel unit.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | AUTO FLT/FMGC/1 | 10CA1 | B02 |
| 49VU | LIGHTING/EMER LT/CKPT/DOME | 1LE | H08 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | ENGINE/1 AND 2/IGN/SYS A | 1JH | A03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | AUTO FLT/FMGC/1 | 10CA1 | H08 |
| 49VU | LIGHTING/EMER LT/CKPT/DOME | 1LE | H06 |
| ** ON A/C NOT FOR ALL | |||
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | AUTO FLT/FMGC/2 | 10CA2 | M17 |
| 121VU | ENGINE/IGN/ENG2/SYS B | 3JH2 | P42 |
| 121VU | ENGINE/IGN/ENG1/SYS B | 3JH1 | P41 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
| 122VU | LIGHTING/INSTL LT/MAIN INST/PNL AND/PED | 4LF | Y04 |
| 122VU | LIGHTING/FLOOD/CTR INST/PNL | 2LE | Z04 |
Subtask 76-11-41-420-060-A ** ON A/C NOT FOR ALL
A. Installation of the Throttle Control Lever Assembly
(1) On the bellcrank (55), install a new AIPC 76-11-81-01-300 BEARING (50).
(2) On the bellcrank (41), install a new AIPC 76-11-81-01-300 BEARING (40), the spacer (47) and a new AIPC 76-11-81-01-300 BEARING (48).
(3) Engage the shaft (54) and push it. At the same time install:
(a) The bushing (53)
(b) The bellcrank (55)
(c) The adjustment bushing (49)
(d) The bellcrank (41)
(e) The bushing (39).
(4) Push the shaft (54) and install the washer (38) and the nut (37).
(5) TORQUE the nut (37) to between 4 and 3 m.daN (29.50 and 22.12 lbf.ft )
.
(6) Wirelock the nut (37).
14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - .
(7) Remove the blanking caps from the connectors 2145VC and 2146VC.
(8) Connect connectors 2145VC and 2146VC.
(9) Install the clamps (82), the washers (81) and (83) and the screws (80).
(10) Install the clamps (77), the washers (78) and (79) and the screw (76).
(11) Install the rocker (57) and the pin (59).
(12) Install the link (25), the bearing (65), the bushing (66), the screw (64), the bushing (61), the bearing (60), the washer (73) and the nut (74).
(13) Install the two new AIPC 76-11-81-01-230 COTTER PINS (72).
(14) Install the two forward covers (63) and the two aft covers (42).
(15) Install the eight screws (46), the eight washers (45) and the eight nuts (44).
(16) Install eight new AIPC 76-11-81-01-230 COTTER PINS (43).
Subtask 76-11-41-220-054-A ** ON A/C NOT FOR ALL (1) On the bellcrank (55), install a new AIPC 76-11-81-01-300 BEARING (50).
(2) On the bellcrank (41), install a new AIPC 76-11-81-01-300 BEARING (40), the spacer (47) and a new AIPC 76-11-81-01-300 BEARING (48).
(3) Engage the shaft (54) and push it. At the same time install:
(a) The bushing (53)
(b) The bellcrank (55)
(c) The adjustment bushing (49)
(d) The bellcrank (41)
(e) The bushing (39).
(4) Push the shaft (54) and install the washer (38) and the nut (37).
(5) TORQUE the nut (37) to between 4 and 3 m.daN (29.50 and 22.12 lbf.ft )
. (6) Wirelock the nut (37).
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(a) Wirelock the nut (37) with a lockwire (7) Remove the blanking caps from the connectors 2145VC and 2146VC.
(8) Connect connectors 2145VC and 2146VC.
(9) Install the clamps (82), the washers (81) and (83) and the screws (80).
(10) Install the clamps (77), the washers (78) and (79) and the screw (76).
(11) Install the rocker (57) and the pin (59).
(12) Install the link (25), the bearing (65), the bushing (66), the screw (64), the bushing (61), the bearing (60), the washer (73) and the nut (74).
(13) Install the two new AIPC 76-11-81-01-230 COTTER PINS (72).
(14) Install the two forward covers (63) and the two aft covers (42).
(15) Install the eight screws (46), the eight washers (45) and the eight nuts (44).
(16) Install eight new AIPC 76-11-81-01-230 COTTER PINS (43).
B. Make sure that there is a minimum clearance of 3 mm (0.12 in.) between the two screws (64) and the eight screws (46).
(1) If not, install a new AIPC 76-11-81-01-130 ADJUSTMENT BUSHING (49).
Subtask 76-11-41-420-061-A ** ON A/C NOT FOR ALL (1) If not, install a new AIPC 76-11-81-01-130 ADJUSTMENT BUSHING (49).
C. Installation of the Housing
(1) Connect connector 21LFA (19) on the housing (18) and tighten the nut of the connector.
(2) Install the new AIPC 33-13-88-03-110 LIGHTED LABEL (86) on the housing (18).
(3) Install the five screws (85).
(4) Install the housing (18).
(5) Install the three screws (20).
(6) Install the three screws (17).
Subtask 76-11-41-420-062-A ** ON A/C NOT FOR ALL (1) Connect connector 21LFA (19) on the housing (18) and tighten the nut of the connector.
(2) Install the new AIPC 33-13-88-03-110 LIGHTED LABEL (86) on the housing (18).
(3) Install the five screws (85).
(4) Install the housing (18).
(5) Install the three screws (20).
(6) Install the three screws (17).
D. Installation of the Levers
(1) Install the lever (29). To do this, push the lever to connect the connector located inside, at the lever-to-bellcrank junction.
(2) Apply Threadlocking Adhesive-- Medium strength - (Material No.05BAE1) on the two screws (15).
(3) Install the two screws (15) and the two hollow pins (13).
(4) Assemble the trigger (27) and the link (25) with the pin (26).
(5) Engage the trigger (27) in the lever (29) and install the hollow pin (24) and the screw (28).
(6) Install the index (16) and the two screws (14).
(7) Install the index (22) and the two screws (23).
(8) Put the two control levers in the idle position (0 deg.TLA) and engage the two links.
(9) If necessary, install two new bushings (33) on the screws (34) and bond them with Retaining adhesive-Cylindrical fitting Medium strength Low viscosity - (Material No.05ABF1) .
(10) Install the two screws (34), washers (32) and nuts (31).
(11) Install the two new AIPC 76-11-81-01-010 COTTER PINS (30).
Subtask 76-11-41-080-054-A ** ON A/C NOT FOR ALL (1) Install the lever (29). To do this, push the lever to connect the connector located inside, at the lever-to-bellcrank junction.
(2) Apply Threadlocking Adhesive-- Medium strength - (Material No.05BAE1) on the two screws (15).
(3) Install the two screws (15) and the two hollow pins (13).
(4) Assemble the trigger (27) and the link (25) with the pin (26).
(5) Engage the trigger (27) in the lever (29) and install the hollow pin (24) and the screw (28).
(6) Install the index (16) and the two screws (14).
(7) Install the index (22) and the two screws (23).
(8) Put the two control levers in the idle position (0 deg.TLA) and engage the two links.
(9) If necessary, install two new bushings (33) on the screws (34) and bond them with Retaining adhesive-Cylindrical fitting Medium strength Low viscosity - (Material No.05ABF1) .
(10) Install the two screws (34), washers (32) and nuts (31).
(11) Install the two new AIPC 76-11-81-01-010 COTTER PINS (30).
E. Remove the rigging pin (11) from the artificial feel unit.
5. Close-upSubtask 76-11-41-410-058-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Install the pitch-trim control mechanism (Ref. AMM TASK 27-41-41-400-001).
(2) Install the plates (4) and (10).
(3) Install the screws (6) and the washers (5).
(4) Install the clamps (9).
(5) Install the ventilation plates (8).
(6) Install the screws (7).
(7) Install the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU.
(b) Install the connector (2) on the panel (1).
(c) Install the panel (1) on the structure.
(d) Fully tighten the fasteners on the panel (1).
(8) Install the Multipurpose Control and Display Units (MCDUs) (3CA1, 3CA2) (Ref. AMM TASK 22-82-12-400-002).
(9) Install the Radio Management Panels (RMPs) (1RG1, 1RG2) (Ref. AMM TASK 23-13-13-400-001).
(10) Install the Audio Control Panels (ACPs) (2RN1, 2RN2) (Ref. AMM TASK 23-51-12-400-001).
(11) Install the weather radar control unit (3SQ) (Ref. AMM TASK 34-41-12-400-001).
(12) Install the ATC/TCAS control unit (3SH) (Ref. AMM TASK 34-52-12-400-001).
Subtask 76-11-41-410-059-A ** ON A/C NOT FOR ALL (1) Install the pitch-trim control mechanism (Ref. AMM TASK 27-41-41-400-001).
(2) Install the plates (4) and (10).
(3) Install the screws (6) and the washers (5).
(4) Install the clamps (9).
(5) Install the ventilation plates (8).
(6) Install the screws (7).
(7) Install the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU.
NOTE: The installation procedure is the same for the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU.
(a) Remove the blanking caps from the connectors (2) and (3). (b) Install the connector (2) on the panel (1).
(c) Install the panel (1) on the structure.
(d) Fully tighten the fasteners on the panel (1).
(8) Install the Multipurpose Control and Display Units (MCDUs) (3CA1, 3CA2) (Ref. AMM TASK 22-82-12-400-002).
(9) Install the Radio Management Panels (RMPs) (1RG1, 1RG2) (Ref. AMM TASK 23-13-13-400-001).
(10) Install the Audio Control Panels (ACPs) (2RN1, 2RN2) (Ref. AMM TASK 23-51-12-400-001).
(11) Install the weather radar control unit (3SQ) (Ref. AMM TASK 34-41-12-400-001).
(12) Install the ATC/TCAS control unit (3SH) (Ref. AMM TASK 34-52-12-400-001).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(3) Close access door 811.
(4) Remove the WARNING NOTICE(S).
(5) Make sure that all the circuit breakers shown in the paragraph Procedure of the engine interface unit installation are closed. If they are not, close them in the recommended sequence
(Ref. AMM TASK 73-25-34-400-802)
Subtask 76-11-41-865-064-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(3) Close access door 811.
(4) Remove the WARNING NOTICE(S).
(5) Make sure that all the circuit breakers shown in the paragraph Procedure of the engine interface unit installation are closed. If they are not, close them in the recommended sequence
(Ref. AMM TASK 73-25-34-400-802)
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 76-11-41-710-056-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | LIGHTING/EMER LT/CKPT/DOME | 1LE | H08 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | ENGINE/1 AND 2/IGN/SYS A | 1JH | A03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | LIGHTING/EMER LT/CKPT/DOME | 1LE | H06 |
| ** ON A/C NOT FOR ALL | |||
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | ENGINE/IGN/ENG2/SYS B | 3JH2 | P42 |
| 121VU | ENGINE/IGN/ENG1/SYS B | 3JH1 | P41 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
| 122VU | LIGHTING/INSTL LT/MAIN INST/PNL AND/PED | 4LF | Y04 |
| 122VU | LIGHTING/FLOOD/CTR INST/PNL | 2LE | Z04 |
D. Do the test that follows:
(1) Do an operational test of the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU.
(a) Operate the light adjustment knobs of the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU.
(b) Make sure that the light intensity of the glareshield 13VU, F/O glareshield panel 130VU, CAPT glareshield panel 131VU and overhead control and indicating panel 48VU changes.
(2) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001).
(1) Do an operational test of the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU.
(a) Operate the light adjustment knobs of the FLOOD LT/INTEG LT panel 111VU and the FLOOD LT panel 112VU.
(b) Make sure that the light intensity of the glareshield 13VU, F/O glareshield panel 130VU, CAPT glareshield panel 131VU and overhead control and indicating panel 48VU changes.
(2) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001).
NOTE: If the aircraft is operated in CAT III conditions, do the operational test of the LAND CAT III capability (Ref. AMM TASK 22-97-00-710-001).
Panels 111VU and 112VU