Subtask 29-00-00-910-054
 E. Torque Values of the Check Valves (Inline Assembly) - Continuation of
 Table I _____________________________________________________________________________ THREAD SIZE | TORQUE VALUE | FIN
 | m.daN (lbf. in.) _____________________________________________________________________________ INLET | OUTLET | INLET | OUTLET |
 _____________________________________________________________________________ .7500-16UNJF-3A | .8750-14UNJF-3A | 5.311 - 5.763 | 7.006 - 7.684 | 2050GM
 | |(470.00-510.00)|(620.00-680.00)| _____________________________________________________________________________ .8750-14UNJF-3A | 1.0625-12UNJ-3A | 7.006 - 7.684 |9.662 - 10.679 | 2055GM
 | |(620.00-680.00)|(855.00-945.00)| | | | | 2144GM | | | | 3024GM
 _____________________________________________________________________________
 1.0625-12UNJ-3A | 1.3125-12UNJ-3A | 9.662-10.679 | 12.882-14.238 | 1019GM
 | |(855.00-945.00)|(1140.0-1260.0)|
 | | | | 2028GM
 | | | | 3019GM

 _____________________________________________________________________________ 1.3125-12UNJ-3A | 1.6250-12UNJ-3A |12.882-14.238 | 17.176-18.984 | 2029GM
 | |(1140.0-1260.0)|(1520.0-1680.0)| _____________________________________________________________________________ 1.6250-12UNJ-3A | 1.8750-12UNJ-3A | 17.176-18.984 | 21.470-23.730 | 1018GM
 | |(1520.0-1680.0)|(1900.0-2100.0)| | | | | 3018GM
 Subtask 29-00-00-910-055
 F. Torque Values of the Check Valves (Inline/Block Assembly) Table II _____________________________________________________________________________ THREAD SIZE | TORQUE VALUE | FIN

 | m.daN (lbf.in.) | _____________________________________________________________________________ INLET | OUTLET | INLET | OUTLET |
 _____________________________________________________________________________ .5625-18UNJF-3A | .7500-16UNJF-3A | 2.430 - 2.769 | 3.186 - 3.470 | 1024GM
 | |(215.00-245.00)|(281.95-307.08)| _____________________________________________________________________________ .7500-16UNJF-3A | .8750-14UNJF-3A | 3.186 - 3.470 | 7.006 - 7.684 | 2057GM
 | |(281.95-307.08)|(620.00-680.00)| | | 5.311 - 5.763 | 4.320 - 4.609 | 3058GM | |(470.00-510.00)|(382.30-407.88)|
 _____________________________________________________________________________
 .8750-14UNJF-3A | 1.0625-12UNJ-3A | 7.5 - 8.3 | 9.662 - 10.679| 1093GM | |(663.60-734.40)|(855.00-945.00)| | | | | 2022GM | | 3.186 - 3.470 | 9.662 - 10.679| 2057GM | |(281.99-307.08)|(855.00-945.00)| | | 7.006 - 7.684 | 6.260 - 6.830 | 3093GM | |(620.00-680.00)|(553.99-604.43)|
 _____________________________________________________________________________
 1.3125-12UNJ-3A | 1.6250-12UNJ-3A | 9.103 - 10.240|17.176 - 18.984| 1022GM | |(805.58-906.20)|(1520.0-1680.0)| | | | | 3022GM Subtask 29-00-00-910-056

 G. Torque Values of the Check Valves (Block Assembly) Table III _____________________________________________________________________________
 THREAD SIZE  | TORQUE VALUE  | FIN
 | m.daN (lbf.in.)  |
 _________________________ 1.0625-12UNJ-3A  ___________________________________| 6.258 - 6.827  _________________| 1094GM
 |(533.81 - 604.162)  |
 |  | 2059GM

 _____________________________________________________________________________
 1.6250-12UNJ-3A  | 10.240 - 11.380 | 1059GM |(906.20 - 1007.08) | | | 3059GM | | 3094GM
 Subtask 29-00-00-790-051
 H. Leak Test
 (1)
 Make sure that the fluid level in the reservoir of the related hydraulic system is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).

 (2)
 Pressurize the reservoirs of the hydraulic systems (Ref. TASK 29-14-00-614-002).

 (3)
 Pressurize the Green, Yellow or Blue hydraulic system (as applicable) (Ref. TASK 29-10-00-863-001), (Ref. TASK 29-10-00-863-002) or (Ref. TASK 29-10-00-863-003).

 (4)
 Examine the related connection for leaks.

 NOTE : Leaks are not permitted.
____
 (5) Depressurize the hydraulic system pressurized above. (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002) or (Ref. TASK 29-10-00-864-003).

 5. Close-up
________ Subtask 29-00-00-860-081
 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 door(s) which you opened for access.

 TASK 29-00-00-910-004
 General Rules for Removal and Installation Procedures in the Hydraulic Systems
　
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1(67)