5. Close-up________
Subtask 27-34-00-860-057
A. Put the Aircraft back to its Initial Configuration.
(1)
On the maintenance panel 50VU:
-Push the HYD LEAK MEASUREMENT VALVES/G and HYD LEAK MEASUREMENT VALVES/Y pushbutton switches (on these pushbutton switches the OFF legends go off).
(2)
On the overhead panel 23VU:
-Push the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches (on these pushbutton switches, the OFF legends go off).
(3)
On the overhead panel 24VU:
-Push the FLT CTL/ELAC 2 and FLT CTL/SEC 2 pushbutton switches (on these pushbutton switches, the OFF legends go off).
(4)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).
(5)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
1EFF : ALL 1 27-34-00Page 513 1 1 May 01/00R 1 1 1CES 1
(6) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
002).
R Subtask 27-34-00-410-061
R B. Close Access.
R (1) Install the protective cover on the battery power center 105VU.
R (2) Tighten the two screws.
R (3) Close the access door 822
R (4) Remove the access platform(s).
TASK 27-34-00-820-001
Adjustment of the Elevator and Hydraulic Actuation (with the reference triangle on the tail cone)
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.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
No specific warning notices
No specific access platform 1.6 m (5 ft. 3 in.)
No specific access platform 2.8 m (9 ft. 2 in.)
No specific access platform 5.36 m (17 ft. 7 in.)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 0U190360 1 PIN - RIGGING 98D27303000001 1 LOAD APPLICATION TOOL - ELEVATOR, AILERON, RUDDER 98D27903500000 2 PIN-SIDE STICK LOCKING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Lockwire-corrosion resistant steel dia 0.8 mm (0.03 in.)
1EFF : ALL 1 27-34-00Page 515 1 1 Feb 01/05R 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002
24-41-00-862-002
27-34-00-200-002
27-34-00-220-003
27-34-00-710-001
29-10-00-863-003
29-10-00-864-003
29-23-00-863-001
29-23-00-864-001
29-24-00-863-001
29-24-00-864-001
R 55-13-11-000-001
R 55-13-11-400-001 27-34-00-991-001 27-34-00-991-009
3. Job Set-up
__________ Subtask 27-34-00-861-051
Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerCheck of the Elevator Servo Control Oscillations.Check of the Position of the Reference Triangle on the Tail ConeOperational Test of the Elevator and Hydraulic ActuationPressurize the Blue Hydraulic System with a Ground Power SupplyDepressurize the Blue Hydraulic SystemPressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric PumpDepressurize the Green and Yellow Hydraulic Systems after Operation of the PTUPressurize the Yellow Hydraulic System with the Electric PumpDepressurize the Yellow Hydraulic System Removal of the THS Trailing Edge Access Panels Installation of the THS Trailing Edge Access PanelsFig. 501Fig. 502
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