TASK 76-11-41-400-042
Installation of the Throttle Control Lever Assembly
1. Reason for the Job
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Self Explanatory
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
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No specific warning notice
No specific access platform 1.8 m (5 ft. 11 in.)
No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) 98DNSA20208120 1 RIGGING PIN
B. Consumable Materials
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Material No. CP8001 * lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00) Material No. CP8002 *
lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00) R Material No. 08-007A R SEALANT, HIGH TEMP. (Ref. 20-31-00)
Material No. 08-029 USA MIL-R-46082 TYPE I
ADHESIVE (Ref. 20-31-00)
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C. Expendable Parts
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R 30 cotter pins 76-11-01 01C-010 R 40 bearing 76-11-01 01C-310 R 43 cotter pins 76-11-01 01C-230 R 48 bearing 76-11-01 01C-310 R 49 adjustment bushing 76-11-01 01C-110 R 50 bearing 76-11-01 01C-310 R 72 cotter pins 76-11-01 01C-230 R
D. Referenced Information
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22-82-12-000-001 Removal of the MCDU (3CA1,3CA2,3CA3)
22-82-12-400-002 Installation of the MCDU (3CA1,3CA2,3CA3)
22-96-00-710-001 Operational Test of the AFS
22-97-00-710-001 Operational Test of the LAND CAT III Capability
23-13-13-000-001 Removal of the Radio Management Panel (CRMP) (1RG1,
1RG2, 1RG3) 23-13-13-400-001 Installation of the Radio Management Panel (CRMP) (1RG1, 1RG2, 1RG3) 23-51-12-000-001 Removal of the Audio Control Panel (ACP) (2RN1, 2RN2, 2RN3, 2RN4, 2RN5) 23-51-12-400-001 Installation of the Audio Control Panel (ACP) (2RN1, 2RN2, 2RN3, 2RN4, 2RN5) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 27-41-41-000-001 Removal of the Control Mechanism-Pitch Trim 27-41-41-400-001 Installation of the Control Mechanism-Pitch Trim 31-60-00-860-001 EIS Start Procedure
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31-60-00-860-002 EIS Stop Procedure 34-41-12-000-001 Removal of the Weather Radar Control Unit (3SQ) 34-41-12-400-001 Installation of the Weather Radar Control Unit (3SQ) 34-52-12-000-001 Removal of the ATC/TCAS Control Unit (3SH) 34-52-12-400-001 Installation of the ATC/TCAS Control Unit (3SH) 76-11-41-991-914 Fig. 401 76-11-41-991-915 Fig. 402 76-11-41-991-916 Fig. 403 76-11-41-991-917 Fig. 404 76-11-41-991-918 Fig. 405 76-11-41-991-919 Fig. 406 76-11-41-991-920 Fig. 407
3. Job Set-up
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Subtask 76-11-41-865-057
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FMGC/1 10CA1 B02 49VU LIGHTING/EMER LT/CKPT/DOME 1LE H08 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 ENGINE/IGN/ENG2/SYS A BAT 2JH2 P40 121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 P39 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
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