1EFF : ALL 1 32-31-00Page 519 1 1 May 01/05R 1 1 1CES 1
4. Procedure
_________ Subtask 32-31-00-710-050
A. Operational Check of the Retraction Inhibition Baulk
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On panel 400VU:
-Pull the landing-gear - An UP selection is prevented by the control-lever 6GA towards you, action of the retraction inhibition then try to lift it to the UP baulk. position.
5. Close-up
________ Subtask 32-31-00-862-050
A. De-energize the Electrical Circuits
(1) De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002)
Subtask 32-31-00-860-058
B. Aircraft Maintenance Configuration
(1) Pressurize the applicable hydraulic reservoirs (Ref. TASK 29-14-00-614-002).
Subtask 32-31-00-942-058
C. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 32-31-00Page 520 1 1 May 01/05R 1 1 1CES 1
TASK 32-31-00-710-005
Operational Check to Ensure Safety Valve Closes at 260 kts
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 GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Refer to the MPD TASK: 323100-04 Operational Check to Ensure Safety Valve Closes at 260 kts using the APU to energize the aircraft electrical circuits.
NOTE : This task is an alternative procedure to:
____
- operational check to ensure safety valve closes at 260 kts using the aircraft batteries and electrical ground power or
- operational check to ensure safety valve closes at 260 kts using the GND PWR Contactor (3XG) Override Box.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
R No specific colored adhesive tape No specific safety barriers No specific warning notice 36122 1 ADAPTOR-CHARGING,PITOT PROBE 87202126V15 1 GENERATOR - GROUND PRESSURE 98D29207542000 1 SAFETY DEVICE - RAT 98D29208246001 1 SAFETY DEVICE - RAT
R 98D34003500000 1 ADAPTER COVER-STATIC PORT 98F32304000000 1 FALSE TARGET
1EFF : ALL 1 32-31-00Page 521 1 1 May 01/05 1 1 1CES 1 B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the APU 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the APU 29-22-00-860-001 Installation of the Safety Device of the Ram Air
Turbine 29-22-00-860-002 Removal of the Safety Device of the Ram Air Turbine 29-22-00-860-007 Installation of the Safety Device of the Ram Air
Turbine 29-22-00-860-008 Removal of the Safety Device of the Ram Air Turbine 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump 29-24-00-864-001 Depressurize the Yellow Hydraulic System 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears 32-00-00-860-001 Flight Configuration Precautions with Electrical Power 32-00-00-860-002 Ground Configuration after Flight Configuration with Electrical Power TSM 32 PB 101 (for corrective action) R 32-31-00-991-025 Fig. 505
3. Job Set-up
__________
R **ON A/C 001-049, 051-061, 101-105, 201-203,
Subtask 32-31-00-941-079
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Make sure that the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).
(3)
Install the SAFETY DEVICE - RAT (98D29207542000) (Ref. TASK 29-22-00-860-001).
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4(62)
