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时间:2011-04-02 23:46来源:蓝天飞行翻译 作者:航空
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 716-082
 (38)
 Turn Pressure Regulator No. 1 clockwise until (19.0) inches of Hg. is indicated on Test Set Gauge No. 2.

 S 216-141

 (39)
 Examine the position indicator on the PRSOV.

 (a)  
If the position indicator is NOT in the full-open position, replace the PRSOV (AMM 36-11-15/401), the go to step H.(40).

 (b)  
If the position indicator is in the full-open position, continue.

 


 S 716-083
 (40)
 Turn Pressure Regulator No. 1 counterclockwise until (0.0) psig is indicated on the No. 2 test set gauge.

 S 716-084

 (41)
 Set the SYSTEM SELECTOR valve handle to the OFF position.

 S 436-085

 (42)
 Install the MS21902-6 Union at the sense line fitting.

 S 036-086

 (43)
 Disconnect the TYPE A hose from the Bleed Air Regulator supply pressure port.

 S 436-087

 (44)
 Connect the TYPE A hose to the Union in the sense line.

 (45)
 Close the test set shutoff valves No. 2 and No. 3.

 (46)
 Set the SYSTEM SELECTOR handle to the A position.

 S 716-090

 (47)
 Turn Pressure Regulator No. 1 clockwise until (24) psig. is indicated on the Test Set Gauge No. 3.


 S 716-088
 S 716-089
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-11-05
 ALL  ú ú 01 Page 618 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 216-091
 (48) Examine the 450°F thermostat, sense lines and fittings for leakage.
 (a)  Replace or repair damaged items as necessary.
 S 716-092
 (49)
 Turn Pressure Regulator No. 1 counterclockwise until (0.0) psig.  is indicated on Test Set Gauges No. 2 and No. 3.

 S 436-093

 (50)
 Connect all of the pressure lines disconnected in the test.

 S 716-094

 (51)
 Put the test set back to its pre-test condition (i.e. all test fittings capped, primary regulator turned off).

 S 726-095

 (52)
 Do the Engine Bleed Air Control System Operational Test (ENGINE) (Ref 36-11-05/501).


 I. Examine the High Stage Valve and High Stage Regulator
 S 036-096
 (1)  
Remove the cap from the test set fitting No. 4.

 S 436-097

 (2)  
Install MS21902-6 Union in the control pressure line.

 S 436-098

 (3)  
Connect -6 end of TYPE A hose to the Union at the control pressure line.

 S 436-099

 (4)  
Connect the -4 end of the TYPE A hose to the No. 4 test set fitting. (See Fig. 604 Sheet 1)

 S 716-100

 (5)  
Turn the primary regulator until (50.0 | 5.0) psig is indicated on the primary gauge.


 NOTE: Make sure all of the test set regulators are in the
____ minimum pressure position (i.e. turned to the counterclockwise position).
 S 716-101
 (6)  
Set the SYSTEM SELECTOR handle to the A position.

 S 716-102

 (7)  
Turn the No. 1 pressure regulators clockwise until (18.0 | 1.0) psig. is indicated on test set gauge No. 3.


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 36-11-05
 ALL  ú ú 01 Page 619 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

737-300/400/500MAINTENANCE MANUAL 
HIGH STAGE 
REGULATOR 
SEE  A
HIGH STAGE 
REGULATOR 
HIGH STAGE VALVE 
PORTABLE VALVE 
ACTUATING  UNION 
TEST SET 
(EXAMPLE)  CONTROL 
PRESSURE LINE 

SUPPLY 
VISUAL  PRESSURE 
HIGH STAGE  POSITION  LINE 
VALVE  INDICATOR 


 
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