(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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