• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-24 08:39来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 3. Job Set-up__________
 Subtask 29-13-49-941-083
 A. Safety Precautions
 (1) On the center pedestal, on the ENG panel 115VU: - put a warning notice to tell persons not to start the engine 2.
 (2) Make sure that the engine 2 shutdown occurred not less than 5 minutes before you do this procedure.
 (3) On the overhead maintenance panel 50VU: - make sure that the ON legend of the ENG/FADEC GND PWR 2 pushbutton switch is off.
 (4) Put a warning notice to tell persons not to energize the FADEC 2.
 Subtask 29-13-49-010-071
 B. Get Access
 (1) Open the fan-cowl doors: FOR 1000EM2 - 447AL, 448AR (Ref. TASK 71-13-00-010-040).
 (2) Put the access platform in position at the engine.

 

 Subtask 29-13-49-865-067
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------
PANEL  DESIGNATION  IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU HYDRAULIC/Y HYD/PUMP ENG2/MONG  3700GD  Q37
 4. Procedure_________ 
R  (Ref. Fig. 601/TASK 29-13-49-991-300)
 Subtask 29-13-49-210-052 
R  A. Do a visual inspection of the hydraulic hoses and tubes installed on the 
R  engine.
 -------------------------------------------------------------------------------
INSPECT/CHECK  MAXIMUM  REMARKS
 SERVICEABLE LIMITS
 -------------------------------------------------------------------------------
R  1. Examine the hydraulic suction hose assembly, look for: 
R  A. Cracks.  None permitted.  Replace the hose-tube 
R  assembly (Ref. TASK 29-13-
R  49-000-001) and (Ref. TASK
 29-13-49-400-001). 
R  B. Crimps.  None permitted.  Replace the hose-tube 
R  assembly (Ref. TASK 29-13-
R  49-000-001) and (Ref. TASK
 29-13-49-400-001). 
R  C. Internal blockage.  None permitted.  Remove the blockage or 
R  replace the hose-tube 
R  assembly (Ref. TASK 29-13-
R  49-000-001) and (Ref. TASK
 29-13-49-400-001). 
R  D. Leakage.  None permitted.  Replace the hose-tube 
R  assembly (Ref. TASK 29-13-
R  49-000-001) and (Ref. TASK
 29-13-49-400-001).

 

R R  Hydraulic Hoses and Tubes Figure 601/TASK 29-13-49-991-300- 12 (SHEET 1)
 1EFF : 1 1 1CES  ALL  1 111 29-13-49 Page 604 Aug 01/05

 

R R  Hydraulic Hoses and Tubes Figure 601/TASK 29-13-49-991-300- 22 (SHEET 2)
 1EFF : 1 1 1CES  ALL  1 111 29-13-49 Page 605 Aug 01/05

 

 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
R  E. Nicks & 
R  scratches-tube 
R  portion of suction 
R  hose-tube 
R  assembly. 

R  F. End-fitting thread 
R  damage. 




R  G. End-fitting 
R  damaged flats. 



Maximum depth cannot be more than 0.0035 in. (0.0889 mm) deep (not more than 10 percent of the wall thickness).
Damage is permitted if the threads that are good are not reduced by more than one thread.
Damage is permitted if the damaged end-fittings can keep the correct torque value.
If the damage is more than the allowable limits, replace the hose-tube assembly (Ref. TASK 29-13-49-000-001) and (Ref. TASK 29-13-49-400-001).
If the damage is more than the allowable limits, replace the hose-tube assembly (Ref. TASK 29-13-49-000-001) and (Ref. TASK 29-13-49-400-001).
If the end-fittings cannot keep the correct torque value, replace the hose-tube assembly (Ref. TASK 29-13-49-000-001) and (Ref. TASK 29-13-49-400-001).
R 2. Examine the Hydraulic Pressure Hose-Tube Assembly, look for:

R  A. Broken wire  Maximum of three broken  If the damage is more than 
R  braids.  wires per plait.  the allowable limits, 
R  No more than six broken  replace the hose-tube 
R  wires in an assembly.  assembly (Ref. TASK 29-13-
R  No more than six broken  49-000-002) and (Ref. TASK 
R  wires in each 1 ft.  29-13-49-400-002). 
 
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4(86)