Speedbrake Control Transducer Unit
Figure 401/TASK 27-92-14-991-001
1EFF : ALL 1 27-92-14 Page 403
1 1 Feb 01/98
1 1
1CES 1
(2)
Remove the screws (1) and the washers (2).
(3)
Lift the unit (3).
(4)
Disconnect the connectors (4), (5), (6) and (7).
(5)
Remove the unit (3).
(6)
Put blanking caps on the connectors (4), (5), (6), (7) and on the connectors of the unit (3).
TASK 27-92-14-400-001
Installation of the Speedbrake Control Transducer Unit (7CE)
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.
R CAUTION : WHEN YOU CONNECT THE ELECTRICAL CONNECTORS, MAKE SURE THAT YOU_______
R CONNECT EACH PLUG TO THE CORRECT RECEPTACLE (USE THE IDENTIFICATION
R MARKS).
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-92-14-400-002 Installation of the Lighted Plate 27-94-00-710-001 Operational Test of the Spoiler Elevator Computer 3 (SEC 3) 27-94-00-710-002 Operational Test of the Spoiler Elevator Computer 1 (SEC 1) 27-94-00-710-003 Operational Test of the Spoiler Elevator Computer 2
(SEC 2) 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
after Operation of the PTU
29-24-00-864-001 Depressurize the Yellow Hydraulic System
27-92-14-991-001 Fig. 401
3. Job Set-up
__________ Subtask 27-92-14-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that hydraulic systems are depressurized (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).
(2)
Make sure that the access platform is in position at the access door
822.
(3)
Make sure that the access door 822 is open.
(4)
On the battery power center 105VU:
-make sure that the protective cover is removed. Subtask 27-92-14-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 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
4. Procedure
_________
(Ref. Fig. 401/TASK 27-92-14-991-001) Subtask 27-92-14-420-050
A. Installation of the Speed Brake Lever Control
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Remove the blanking caps from the connectors (4), (5), (6), (7) and from the connectors of the unit.
1EFF : ALL 1 27-92-14Page 406 1 1 May 01/00R 1 1 1CES 1
(4)
Make sure that the electrical connectors are clean and in the correct
condition.
(5)
Connect the connectors (4), (5), (6), (7) to the unit (3).
(6)
Put the unit (3) in position.
(7)
Install the washers (2) and the screws (1) and tighten.
(8)
Install the Lighted Plate.
(a) (Ref. TASK 27-92-14-400-002) Subtask 27-92-14-865-052
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(19)
