(2)
Close the doors of the main gear (Ref. TASK 32-12-00-410-001).
(3)
Close the doors of the nose gear (Ref. TASK 32-22-00-410-001).
(4)
Remove the warning notice(s).
(5)
Remove the access platform(s).
(6)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 05-51-24Page 627 1 1 May 01/05R 1 1 1CES 1
INSPECTION AFTER FLIGHT THROUGH DUST STORM/VOLCANIC ASH OR SEVERE CONDITIONS ON
_______________________________________________________________________________
GROUND - INSPECTION/CHECK
_________________________
TASK 05-51-25-200-002
Inspection after Flight through Dust Storm or Dust Contamination on Ground
1. Reason for the Job
__________________
R Do this inspection after flight in a very bad dust storm or after dust contamination on ground.
NOTE : If the dust contamination occurred when the aircraft was on ground
____ with applicable protection by covers and blankets (Ref. AMM 10-11-00), and if there is no dust behind the covers, the inspections specified in para. 4.D.(Inspection of the probes and sensors) and in para.4.F.(Inspection of the nacelles and engines) are not necessary.
NOTE : An adjustable access platform (2.5m to 12m/8.2ft to 39.4ft) is
____ necessary to get access to the different parts of the aircraft during the inspection.
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-21-11-615-001 External Cleaning
12-24-34-600-001 Bleeding of the Standby Air Data System
12-32-28-281-003 Sample Fuel for Microbiological Contamination
Analysis
12-32-29-281-001 Hydraulic Fluid Sample of Green,Blue and Yellow
Systems for Analysis R 21-00-00-615-005 Decontamination of the Environmental Control System R (ECS) after Dust or Volcanic Ash Contamination
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power R 26-21-00-720-003 Check Distribution Piping for Leakage and Obstruction 26-22-00-210-001 Inspection of the APU Fire-Extinguishing Distribution
Piping 27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 27-80-00-866-004 Extending the Slats on the Ground
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-005
28-12-47-200-001
28-13-00-200-001
29-00-00-864-001
29-10-00-200-004
29-10-00-200-007
30-11-00-710-001
30-11-51-000-002
30-11-51-400-002
32-00-00-481-001
32-12-00-010-001
32-12-00-410-001
32-22-00-010-001
32-22-00-410-001
34-10-00-170-001
34-10-00-170-002
34-10-00-170-003
35-12-41-100-001
R 36-11-00-710-003
R 49-16-00-100-001
49-16-00-100-002
49-16-00-100-003
R 49-16-00-200-002
R
R 49-16-00-210-001
R
R 49-16-00-210-002
R
R 49-20-00-200-001
49-20-00-290-001
R 49-91-44-000-001
49-91-44-000-003
49-91-44-000-004
R 49-91-44-400-001
49-91-44-400-003
49-91-44-400-004
53-15-11-200-001
Retracting the Slats on the GroundVisual Check of NACA Intake for Signs of BlockageCheck Drain Mast Outlet for ObstructionPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionCheck of the Clogging Indicators of the Hydraulic System Filters (Other than the two Case Drain Filters of the Engine-Driven Pumps)Check Clogging Indicator on Engine-Driven Pump (EDP) Case Drain FilterOperational Test of the Wing Ice-Protection SystemRemoval of the Anti-Ice Valve FilterInstallation of the Anti-Ice Valve FilterInstallation of the Safety Devices on the Landing GearsOpen the Main Gear Doors for AccessClose the Main Gear Doors after AccessNose Gear Doors - Ground Doors OpeningNose Gear Doors - Ground Doors ClosingFlushing of the Principal Total Pressure LinesFlushing of the Principal Static Pressure LinesDraining and Flushing of Standby Pneumatic CircuitsCleaning of the Mask-Full Face / Q.D, Oxygen (5757HM,5758HM,5759HM,5760HM) Operational Test of the Bleed Air System Cleaning of the APU Air Intake System (GTCP 36-300)Cleaning of the APU Air Intake System (APS 3200)Cleaning of the APU Air Intake System (131-9(A)) Detailed Inspection of APU Air Intake, Diffuser Elbow, Seals and Felt Metal (131-9(A)) Detailed Inspection of the Air Intake, Diffuser Elbow, Seals and Felt Metal (GTCP 36-300) Detailed Inspection of APU Air Intake, Diffuser Elbow, Seals and Felt Metal (APS 3200) Inspection/Check of the Engine (4005KM) (GTCP 36-300)APU Power Plant Borescope Inspection (APS 3200) Removal of the Oil Cooler (8079KM) (GTCP 36-300)Removal of the Oil Cooler (8079KM) (APS 3200)Removal of the Oil Cooler (8079KM) (131-9(A)) Installation of the Oil Cooler (8079KM) (GTCP 36-300)Installation of the Oil Cooler (8079KM) (APS 3200)Installation of the Oil Cooler (8079KM) (131-9(A))Detailed Inspection of the Radome 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 時(shí)間限制/維護(hù)檢查 4(86)
