(2)
Make sure that the warning notice(s) are position to tell persons not to pressurize the Blue hydraulic system.
-In the cockpit on the hydraulic section 40VU of the overhead panel
-On the ground service panel of the Blue hydraulic system.
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-22-53Page 433 1 1 Config-1 May 01/05 1 1 1CES 1
(3)
Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(4)
Make sure that the reservoir of the Blue hydraulic system is depressurized. (Ref. TASK 29-14-00-614-001).
(5)
Make sure that the access door 197EB is open.
(6)
Make sure that the RAT is extended (Ref. TASK 29-22-00-869-001).
Subtask 29-22-53-865-069
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------106VU CSM/G /EV/MAN/SPLY 6XE B04 121VU HYDRAULIC/RAT/SPLY/EXTN/SOL1 2803GE P33
R **ON A/C 001-049, 051-061, 101-102, 201-202,
121VU HYDRAULIC/RAT/CTL 2801GE P32
R **ON A/C 103-105, 203-203,
121VU HYD/RAT/CTL 2801GE P32
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-22-53Page 434 1 1 Config-1 May 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-061, 101-105, 201-203,
4. Procedure
_________
(Ref. Fig. 404/TASK 29-22-53-991-008) Subtask 29-22-53-420-059
A. Installation of the Eye End of the RAT Ejection Jack
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
Apply SPECIAL MATERIALS (Material No. 05-002) to the thread of the eye end (4).
(5)
Assemble the locking key (3) and the nut (2) to the eye end (4).
(6)
Install the eye end (4) in the ejection jack (1).
(7)
Turn the eye end (4) until the distance "Z" is the same as before the removal of the eye end (refer to the note).
(8)
Tighten the nut (2) and make sure that the locking key (3) engages correctly in the ejection jack (1).
(9)
TORQUE the nut (2) to 4.47 m.daN (32.96 lbf.ft).
(10)
Safety the nut (2) and the locking key (3) with MISCELLANEOUS (Material No. 19-010).
(11)
Install the bolt (8), the washers (7) and a new nut (6).
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-22-53Page 435 1 1 Config-1 May 01/05 1 1 1CES 1
(12) TORQUE the nut (6) to between 2.45 and 2.55 m.daN (18.06 and 18.80 lbf.ft).
Subtask 29-22-53-820-052
B. Do the adjustment procedure of the RAT doors (Ref. TASK 29-22-00-820-001).
5. Close-up
________ Subtask 29-22-53-860-073
A. Put the aircraft back to the serviceable condition.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access door 197EB.
(3)
Remove the safety barriers.
(4)
Remove the warning notice(s).
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-22-53Page 436 1 1 Config-1 May 01/05 1 1 1CES 1R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
中國航空網(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 HYDRAULIC POWER 液壓6(53)
