(b)
Install the lockwire.
S 794-014
(4) Do this leakage test for the valve.
(a)
Use the APU to pressurize the pneumatic system (Ref 36-05-00/201).
(b)
Examine the valve for leakage.
NOTE: No leakage is permitted at the valve.
____
(c) Remove the pressure from the pneumatic system (Ref 36-05-00/201).
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A
737-300/400/500MAINTENANCE MANUAL
E. Put the Airplane Back to Its Usual Condition S 414-015
(1) Close the stabilizer trim access door.
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A
737-300/400/500MAINTENANCE MANUAL
ENGINE BLEED OVERHEAT SWITCH - REMOVAL/INSTALLATION
___________________________________________________
1. General_______
A. This procedure contains two tasks. The first task removes the engine bleed overheat switch. The second task installs the engine bleed overheat switch.
TASK 36-11-71-004-001
2. Engine Bleed Overheat Switch Removal____________________________________
A. Access
(1)
Location Zones
201/202 Control Cabin
207 Strut
208 Aft Strut Fairing
(2)
Access Panels
5731/5831 Access Door Strut
B. Prepare to Remove the Overheat Switch
S 864-002
(1)
Open the OVERHEAT circuit breaker on the P6 Load Control Panel and attach a DO-NOT-CLOSE tag.
S 014-003
(2)
Open the access panel to get access to the overheat switch.
C. Remove the Overheat Switch (Fig. 401)
S 034-004
(1)
Disconnect the electrical connector from the overheat switch.
S 024-005
(2)
Remove the overheat switch from the mounting boss on the pneumatic duct.
(3)
Remove the packing ring.
S 034-006
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737-300/400/500MAINTENANCE MANUAL
PRECOOLER CONTROL VALVE SENSOR (REF)
STARTER DUCT (REF)
PRECOOLER (REF)
SEE A
FWD PNEUMATIC DUCT
(490`F) SWITCH AIR OVERHEAT ENGINE BLEED
ELECTRICAL CONNECTOR MOUNTING BOSS
PACKING RING
A
Engine Bleed Overheat Switch Installation Figure 401
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A 737-300/400/500MAINTENANCE MANUAL
TASK 36-11-71-404-007
3. Engine Bleed Overheat Switch Installation
_________________________________________
A. Consumable Materials
(1) Antiseize - High temperature compound, MIL-A-907 or equivalent
B. References
(1) AMM 24-22-00/201, Manual Control
C. Access
(1)
Location Zones
201/202 Control Cabin
207 Strut
208 Aft Strut Fairing
(2)
Access Panels
5731/5831 Access Door Strut
D. Install the Overheat Switch (Fig. 401) 中國(guó)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(jī)維護(hù)手冊(cè) PNEUMATIC(78)
