(9)
Make sure that the container is in position below the hydraulic connections of the Ram Air Turbine.
(10) Make sure that the safety barriers are in position.
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 29-22-53Page 421 1301-399, 401-499, 1Config-1 Aug 01/05 1 1 1CES 1 Subtask 29-22-53-865-077
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU HYD/RAT/CTL 2801GE D14 106VU CSM/G /EV/MAN/SPLY 6XE B04 121VU HYDRAULIC/RAT/SPLY/EXTN/SOL1 2803GE P33
4. Procedure
_________
(Ref. Fig. 402/TASK 29-22-53-991-011, 403/TASK 29-22-53-991-012)
Subtask 29-22-53-210-056
A. Preparation for Installation
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)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(2)
Clean the component interface and/or the adjacent area.
(3)
Do an inspection of the component interface and/or the adjacent area.
(4)
Make sure that the hydraulic line end-fittings are serviceable.
(5)
Make sure that the electrical connectors are clean and in the correct condition.
(6)
Apply SPECIAL MATERIALS (Material No. 05-002) to the shaft of the bolts (1),(19) and (20).
(7)
Apply COMMON GREASE (Material No. 04-011) to the support shafts (31) of the ejection jack (27).
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 29-22-53Page 422 1301-399, 401-499, 1Config-1 Aug 01/05 1 1 1CES 1 Subtask 29-22-53-420-062
B. Installation of the Ejection Jack CAUTION : USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN
_______ YOU DISCONNECT/CONNECT HYDRAULIC LINES ON UNIONS. IF YOU USE THE SECOND WRENCH, YOU WILL NOT LOOSEN OR TIGHTEN THE UNION TOO MUCH.
CAUTION : YOU MUST INSTALL HYDRAULIC TUBES WITH HYDRAULIC FLUID AS
_______
LUBRICANT.
(1)
Put the eye-end (44) of the ejection jack (27) between the forked mounting (43) of the leg assembly (40).
(2)
Install the bolt (42), the washers (41), the washer (45) and the nut (46). Do not tighten the nut (46) at this time.
(3)
Put the rear gimbal half (5) on the ejection jack (27).
(4)
Carefully raise the ejection jack (27) to its correct installation position.
(5)
Hold the gimbal half (5) with your hand.
(6)
Install the bolts (19) and (20) into the upper section of the structure (8) and (18).
(7)
Put the forward gimbal half (14) on the ejection jack (27).
(8)
Make sure that the bolts (19) and (20) are in the correct position between the gimbal halves (5) and (14).
(9)
Install the bolts (13) and the washers (12).
(10)
Install the nuts (6) and the washers (7), but do not tighten the nuts
(6) at this time.
(11)
Install the washers (9) and (15) and the nuts (10) and (16).
(12)
Tighten the nut (10) and safety it with a new cotter pin (11).
(13)
Tighten the nut (16) and safety it with a new cotter pin (17) .
(14)
Tighten the nuts (6).
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 29-22-53Page 423 1301-399, 401-499, 1Config-1 Aug 01/05 1 1 1CES 1
(15)
Put the bonding strap (37) in position and install the washer (36) and the screw (35) (Ref. TASK 20-28-00-912-004).
(16)
Remove the protective caps from the electrical connectors and the receptacles.
(17)
Connect the electrical connectors (25), (28), (33), (34), (38) to their related receptacles.
(18)
Remove the blanking caps from the hydraulic line end-fittings.
(19)
Apply the HYDRAULIC FLUIDS (Material No. 02-003) to the threads of the line end-fittings.
(20)
Remove the blanking plugs from the hydraulic ports.
(21)
Attach the union nuts (29) and (30) to their related ports.
(22)
TORQUE the union nut (29) to between 5.4 and 5.9 m.daN (39.82 and
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 HYDRAULIC POWER 液压6(50)
