-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
On the overhead panel 23VU (24VU), push the FLT CTL/ELAC1 (FLT CTL/ELAC2) pushbutton switch 6CE1 (6CE2).
2.
Push the left or right pedal fully and keep it in this position
3.
Push the pedal disconnection pushbutton switch on the CAPT or F/O handwheel
4.
Release the pedal disconnection pushbutton switch on the CAPT or F/O handwheel
5.
Release the pedals
- on the pushbutton switch 6CE1 (6CE2),the OFF legend goes off, the FAULTlegend comes on and goes off aftersome seconds.
-do a check of the steering of thenose wheels (Ref. TASK 32-51-00-720-004).
-make sure that the nose wheels go tothe zero position: the pointer on thenose gear is aligned with the index.
-
the wheels move to their angle ofturn.
-
the wheels move to the zero position: the pointer on the nose gear is aligned with the fixed index.
1EFF : ALL 1 32-51-00Page 536 1 1 Aug 01/05R 1 1 1CES 1
Subtask 32-51-00-865-069
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2EN1, 2EN2.
5. Close-up________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
Subtask 32-51-00-860-059
A. Put the aircraft back to its initial configuration.
(1) Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
(2) Lower the aircraft on its wheels (Ref. TASK 07-12-00-582-001).
(3) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(5) If the front of the aircraft is lifted off the ground, lower the aircraft to the ground (Ref. TASK 07-11-00-586-001).
(6) If the nosewheels are on grease plates, move the aircraft to remove the grease plates (Ref. TASK 09-10-00-584-002).
(7) Make sure that the work area is clean and clear of tool(s) and other items.
R **ON A/C 401-499,
R Subtask 32-51-00-860-059-A
R A. Put the aircraft back to its initial configuration.
R R (1) Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-002).
R (2) Lower the aircraft on its wheels (Ref. TASK 07-12-00-582-001).
1EFF : ALL 1 32-51-00Page 537 1 1 Aug 01/05 1 1 1CES 1
R (3) Do the EIS stop procedure
R (Ref. TASK 31-60-00-860-002).
R (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
R 002).
R (5) If the front of the aircraft is lifted off the ground, lower the
R aircraft to the ground (Ref. TASK 07-11-00-586-001).
R (6) If the nosewheels are on grease plates, move the aircraft to remove
R the grease plates (Ref. TASK 09-10-00-584-002).
R (7) Make sure that the work area is clean and clear of tool(s) and other
R items.
R 1EFF : 401-499, 1 32-51-00Page 538 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL
TASK 32-51-00-710-002 Integrity Test of the Nose Wheel Steering System WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______
OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1.
Reason for the Job
__________________
To ensure aircraft safety after maintenance work on the wiring
2.
Job Set-up Information
______________________
A. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 04-022 USA MIL-PRF-81322 GRADE 2
SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
(Ref. 20-31-00)
1EFF : ALL 1 32-51-00Page 539 1 1 Aug 01/05 1 1 1CES 1 B. Referenced Information 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 LANDING GEAR 起落架8(87)
