(2)
If necessary, clean the aircraft externally (Ref. TASK 12-21-11-615-001).
Subtask 10-11-00-020-065
B. Removal of the Protection Equipment
(1) Remove all the protection equipment from the engines, the APU, the probes.
EFF : ALL 10-11-00Page 227 May 01/05R CES
Subtask 10-11-00-860-077
C. Aircraft Maintenance Configuration
(1)
Connect the batteries 2PB1, 2PB2 and make sure that the battery charge is correct (Ref. TASK 24-38-51-400-001).
(2)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(3)
On the overhead panel 25VU, on the CABIN PRESS section:
-Push the DITCHING pushbutton switch to open the ventilation skin valves and the outflow valve.
Subtask 10-11-00-281-061
D. Protection of the Fuel System
(1) Drain water from all the fuel tanks (Ref. TASK 12-32-28-281-001). Subtask 10-11-00-210-065
E. Inspection
(1) Do a check of the charge pressure of the landing gear shock absorbers:
-
for the NLG (Ref. TASK 12-14-32-614-004)
-
for the MLG (Ref. TASK 12-14-32-614-003)
(2) Do a check of the tire pressure (Ref. TASK 32-41-00-210-003). R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-212, 214-220,
Subtask 10-11-00-170-056
F. Flushing of the Air Data System NOTE : Flush the Air Data System only if the parking period is more than
____
2 days.
(1)
Flush the total pressure line of the Air Data Module (Ref. TASK 34-10-00-170-001).
(2)
Flush the static pressure line of the Air Data Module (Ref. TASK 34-10-00-170-002).
(3)
Drain and flush the standby static and standby total pressure lines of the Air Data Module (Ref. TASK 34-10-00-170-003).
R **ON A/C 106-149, 213-213, 221-299, 301-399, 401-499,
Subtask 10-11-00-170-056-A
F. Flushing of the Air Data System NOTE : Flush the Air Data System only if the parking period is more than
____
2 days.
(1)
Flush the total pressure line of the Air Data Module (Ref. TASK 34-10-00-170-001).
(2)
Flush the static pressure line of the Air Data Module (Ref. TASK 34-10-00-170-002).
(3)
Drain and flush the standby static and standby total pressure lines of the Air Data Module (Ref. TASK 34-22-25-170-001).
**ON A/C ALL
5. Close-up
________
Subtask 10-11-00-942-057
A. Close-up
(1)
De-energize the aircraft electrical circuits supplied from the external power (Ref. TASK 24-41-00-862-002).
(2)
Remove the tag from the Captain side stick or write in the log book that the protection covers/devices are no longer installed.
(3)
Remove all the fixtures, tools, test and support equipment used during this procedure.
TASK 10-11-00-554-004
R
R R R Return to Operation after Parking not more than 12 Weeks
1. Reason for the Job
__________________
This procedure gives the instructions necessary to operate again an aircraft after a parking period of not more than 12 weeks.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice No specific 1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-14-32-614-003 Check Charge Pressure of Main Landing Gear Shock
Absorber 12-14-32-614-004 Check Shock Absorber Charge Pressure 12-21-11-615-001 External Cleaning 12-32-28-281-001 Drain Water Content 12-32-28-281-003 Sample Fuel for Microbiological Contamination
Analysis 12-32-28-281-004 Fuel Sampling for a Microbiological Contamination
Test with a Microb Monitor Test Kit (OBSOLETE) 24-38-51-400-001 Installation of the Batteries (2PB1, 2PB2) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 28-11-00-280-002 Fuel Tank Leak Checks 28-11-00-600-004 Biobor Biocidal Shock Treatment - With Fuel Mixed
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