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时间:2011-03-25 18:04来源:蓝天飞行翻译 作者:admin
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| -20 | -4 | 87 | 1260 |
 | -10 | +14 | 90 | 1310 |
 | 0 | +32 | 93 | 1350 |
 | +10 | +50 | 97 | 1400 |
 | +20 | +68 | 100 | 1450 |
 | +30 | +86 | 104 | 1510 |
 | +40 | +104 | 107 | 1550 |
 | +50 | +122 | 110 | 1600 |
 | +60 | +140 | 114 | 1650 |
 1EFF : ALL 1 32-44-11Page 603 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------| deg. C | deg. F | "P" bar | "P" psi | --------------------------------------------------------------------------------------------------------------------------------------------------------------


(2)
 If the pressure is more than the correct pressure "P" or if the pressure is between "P" and "P"- 15 bars (218 psi):

 (a) Adjust the pressure as necessary (Ref. TASK 12-14-32-614-002).

 (3)
 If the pressure is more than 15 bars (218 psi) less than the correct pressure "P":

 (a)
 Do a leak check with SPECIAL MATERIALS (Material No. 05-004) on the gas manifold of the accumulator.

 (b)
 If you find leaks, try to stop them. Then pressurize the accumulator (Ref. TASK 12-14-32-614-002).

 (c)
 If you do not find leaks or if you cannot stop the leaks, replace the accumulator (Ref. TASK 32-44-11-000-001) and (Ref. TASK 32-44-11-400-001).

 (d)
 If the accumulator is replaced, bleed the Yellow hydraulic system (Ref. TASK 29-00-00-870-007) downstream of the engine pump, to remove nitrogen that can be in the hydraulic system (that the accumulator has caused).

 


R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 32-44-11Page 604 1201-210, 1May 01/05 1 1 1CES 1 **ON A/C ALL


R Post SB 32-1215 For A/C 001-049,051-099,101-105,151-199,201-210,
 Subtask 32-44-11-210-050-A
 A. Check of the Nitrogen Fill Pressure
 (1) Refer to the accumulator pressure gage 2585GM on the brake Yellow-pressure accumulator. Make sure that the fill pressure is as follows:
 -------------------------------------------------------------------------------| deg. C | deg. F | bar | PSI | -------------------------------------------------------------------------------| -20 | -4 | 61 | 885 | | -10 | +14 | 63 | 914 | | 0 | +32 | 65 | 943 | | +10 | +50 | 68 | 986 | | +20 | +68 | 70 | 1015 | | +30 | +86 | 72 | 1044 | | +40 | +104 | 75 | 1088 | | +50 | +122 | 77 | 1117 | | +60 | +140 | 80 | 1160 | -------------------------------------------------------------------------------
(2)
 If the pressure is high or not more than 15 bars (218 psi) less than the correct pressure:

 (a) Adjust the pressure as necessary (Ref. TASK 12-14-32-614-002).

 (3)
 If the pressure is more than 15 bars (218 psi) less than the correct pressure:

 (a)
 Do a leak check with SPECIAL MATERIALS (Material No. 05-004) on the gas manifold of the accumulator.

 (b)
 If you find leaks, try to stop them. Then pressurize the
 accumulator (Ref. TASK 12-14-32-614-002).


 (c)
 If you do not find leaks or if you cannot stop the leaks, replace the accumulator (Ref. TASK 32-44-11-000-001) and (Ref. TASK 32-44-11-400-001).

 


 1EFF : ALL 1 32-44-11Page 605 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 32-44-11Page 606 1 1 May 01/05 1 1 1CES 1 VALVE - CHARGING (2586GM) - REMOVAL/INSTALLATION


 (d) If the accumulator is replaced, bleed the Yelllow hydraulic system (Ref. TASK 29-00-00-870-007) downstream of the engine pump, to remove nitrogen that can be in the hydraulic system (that the accumulator has caused).
 **ON A/C ALL
 5. Close-up________ 
R  Subtask 32-44-11-865-056 
R R R  A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GG, 2GG, 3GG, 4GG
 Subtask 32-44-11-862-050 
R  B. Aircraft Maintenance Configuration
 (1) De-energize the Ground Service Network (Ref. TASK 24-42-00-862-001).
 Subtask 32-44-11-942-053 
R  C. Removal of Equipment
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Remove the warning notice(s).
 (3) Remove the access platform.
 Subtask 32-44-11-410-050 
R  D. Close Access
 (1) Close the main door of the right main landing gear (Ref. TASK 32-12-00-410-001)

 

________________________________________________
 TASK 32-44-13-000-001
 Removal of the Charging Valve 2586GM
 WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
 YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 
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