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时间:2011-04-08 12:01来源:蓝天飞行翻译 作者:航空
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 TASK 75-24-02-042-013-C00
 2.  HPTCC Timer Deactivation (Electrical Deactivation Procedure)
________________________
 A.  Equipment
 (1)  Switch Pusher, System Test - C75001
 B.  Access
 (1)  Location Zone
 105 E/E Bay

 C.  Procedure
 S 862-015-C00
 (1)  Open these circuit breakers and attach DO-NOT-CLOSE tags:
 (a)  P18-2 Load Control Center 1) STALL WARN AC OR SMC 1 SNSR EXC AC
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITH THE HIGH PRESSURE TURBINE ú

 75-24-02
 CLEARANCE CONTROL (HPTCC) TIMER  ú ú C01 Page 201 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
2) STALL WARN AC OR SMC 2 SNSR EXC AC 3) STALL WARN DC OR SMC 1 CMPTR DC 4) STALL WARN DC OR SMC 2 CMPTR DC 5) STALL WARN ASYM MODE OR SMC STALL WARN ASYM MODE 6) FLIGHT RECORDER DC(BAT) 7) FLIGHT RECORDER AC
 (b)  P18-3 Load Control Center
 1) DRAIN MAST GND
 2) DRAIN MAST AIR

 S 862-022-C00
 (2)  
Make sure you put the antiskid switch to the OFF position.

 S 862-016-C00

 (3)  
Put the flap handle for the trailing edge to the 1 unit detent position.

 S 862-027-C00

 (4)  
On the P5 forward overhead panel, set the mode selector for the cabin pressure control to MAN (manual) mode, and make sure the outlet flow valve is in the fully OPEN position.

 S 032-017-C00

 (5)  
Remove the module cover to get access to the E11 logic shelf for the landing gear.


 NOTE: The E11 logic shelf for the landing gear is found on the
____
 right side of the radar bay just forward of the nose wheel
 well.

 S 862-018-C00
 (6)  Push and hold the AIR SENSING relay push button during the scheduled engine run.
 NOTE: You can hold the AIR SENSING relay push button in the "IN"
____
 position with a system test switch pusher (C75001) for the
 AIR SENSING relay or other clamping methods if it is
 necessary.

 S 862-019-C00
 (7)  After you complete the scheduled engine run(s), do the steps that follow:
 CAUTION: YOU MUST RELEASE THE PUSH BUTTON FOR THE AIR SENSING RELAY
_______ BEFORE FLIGHT. IF YOU DO NOT RELEASE THE PUSH BUTTON FOR THE AIR SENSING RELAY BEFORE FLIGHT, MANY AIRPLANE SYSTEM MALFUNCTIONS WILL OCCUR.
 (a)  Release the push button for the AIR SENSING relay.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITH THE HIGH PRESSURE TURBINE ú

 75-24-02
 CLEARANCE CONTROL (HPTCC) TIMER  ú ú C01 Page 202 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b)  
Install the module cover on the E11 logic shelf for the landing gear.

 (c)  
Put the flap handle for the trailing edge to the 0 unit detent position.


 S 862-026-C00
 (8)  
On the P5 forward overhead panel, set the mode selector for the cabin pressure control to AUTO mode, and make sure the outlet flow valve is in the fully OPEN position.

 S 862-023-C00

 (9)  
Make sure you put the antiskid switch to the ON position.

 S 862-020-C00

 (10)
 Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P18-2 Load Control Center
 1) STALL WARN AC OR SMC 1 SNSR EXC AC
 2) STALL WARN AC OR SMC 2 SNSR EXC AC
 3) STALL WARN DC OR SMC 1 CMPTR DC
 4) STALL WARN DC OR SMC 2 CMPTR DC
 5) STALL WARN ASYM MODE OR SMC STALL WARN ASYM MODE
 6) FLIGHT RECORDER DC(BAT)
 7) FLIGHT RECORDER AC


 (b)  
P18-3 Load Control Center
 1) DRAIN MAST GND
 2) DRAIN MAST AIR

 

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITH THE HIGH PRESSURE TURBINE ú
 
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