TYPE A PRESSURE HOSE
TEST SET
FITTING NO. 4

High Stage Regulator and High Stage Valve System Inspection/Check Figure 604 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-11-05
 ALL  ú ú 01 Page 620 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 716-103
 (8)  Turn the No. 1 pressure regulator counterclockwise until (0.0) psig. is indicated on test set gauge No. 3.
 NOTE: Steps I.(7) and I.(8) are completed to exercise the valve.
____
 S 216-142
 (9)  Slowly turn the No. 1 pressure regulator clockwise to a maximum pressure of (10.0) psig. Monitor the pressure and the position indicator on the high stage valve.
 (a)  
If the position indicator is NOT in the full-open position by

 (10.0) psig, replace the high stage valve (AMM 36-11-85/401), then go to step I.(10).

 (b)
If the position indicator is in the full-open position by

 (10.0) psig, continue.
 S 716-104
 (10)
 Turn the No. 1 pressure regulator counterclockwise until (0.0) psig. is indicated on test set gauge No. 3.

 S 716-105

 (11)
 Set the SYSTEM SELECTOR handle to the OFF position.

 S 036-106

 (12)
 Disconnect the TYPE A hose from the control pressure line.

 (13)
 Remove the MS21902-6 Union from the control pressure line.

 (14)
 Connect the control pressure line to the High Stage Regulator.

 (15)
 Remove the relief valve at test port B on the High Stage Regulator.

 S 036-107
 S 436-108
 S 426-109
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-11-05
 ALL  ú ú 01 Page 621 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 436-110
 (16)
 Install the AN815-4D Union with a MS29513-12 O-ring into the High Stage Regulator relief valve port B.

 S 426-111

 (17)
 Remove the cap from test set fitting NO. 2.

 S 436-112

 (18)
 Connect a TYPE B hose between the AN815-4D Union and the Test set.

 S 036-113

 (19)
 Disconnect the supply pressure line to the High Stage Regulator.

 S 436-114

 (20)
 Connect the -6 end of the hose which is connected to test set fitting No. 4 to the supply pressure port on the High Stage Regulator. (See Fig. 604 Sheet 2)

 S 716-115

 (21)
 Set the SYSTEM SELECTOR handle to the A position.

 S 716-116

 (22)
 Turn the NO. 1 pressure regulator clockwise until (36.0 | 1.0) psig. is indicated on test set gauge No. 3.

 S 216-143

 (23)
 Examine the control pressure shown on Test Set Gauge No. 4.

 (a)  
If the control pressure is NOT (15.0 | 2.0) psig for high stage regulator P/N 107484-3 or (16.5 | 1.0) psig for high stage regulator P/N 107484-5 or P/N 107484-6, replace the high stage regulator (AMM 36-11-86/401), then go to step I.(36).

 (b)  
If the control pressure is (15.0 | 2.0) psig for high stage regulator P/N 107484-3 or (16.5 | 1.0) psig for high stage regulator P/N 107484-5 or P/N 107484-6, then remove downstream line on regulator. 1) If leakage is found, replace the high stage regulator

 (AMM 36-11-86/401), then go to step I.(36).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-11-05
 ALL  ú ú 01 Page 622 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

PORTABLE VALVE ACTUATING TEST SET (EXAMPLE)
HIGH STAGE
REGULATOR

SEE B AN815-4D UNION
CONTROL PRESSURE LINE HIGH STAGE REGULATOR
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 PNEUMATIC(56)