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时间:2011-04-03 11:28来源:蓝天飞行翻译 作者:航空
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____ psig (414-620 kPa) of air or nitrogen to dry the surfaces.
 (b)  
Put the vortex generator (1) without the two shims (9) on the air inlet door (8).

 (c)  
If there is a clearance of more than 0.005 inch (0.13 mm) between the vortex generator (1) and air inlet door (8), then do these steps to install the two shims (9): 1) Clean the mating surfaces of the vortex generator (1) and


 two shims (9) with alcohol and a cloth.
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 49-15-23
 ALL  ú ú 01 Page 403 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL ////////////////////////
2)  Use the air source to dry the surfaces of the vortex generator (1) and two shims (9).
 NOTE: It is recommended that you use a pressure of 60-90
____ psig (414-620 kPa) of air or nitrogen to dry the surfaces of the vortex generator and two shims.
 3)  Mix the two-part adhesive per the manufacturer's instructions.
 NOTE: The pot life of the mixed adhesive is approximately
____ two hours at 68°F-80°F (20°C-26.7°C).
 4)  Apply a thin and continuous layer of mixed adhesive to the
 mating surfaces of the two shims (9). 5) Install the two shims (9) on the vortex generator (1). 6) Remove the unwanted mixed adhesive from the two shims (9)
 and vortex generator (1) with a cloth or cotton swabs.
 7)  Use rubber-tipped clamps or wood strips or equivalent tools to hold the two shims (9) tightly to the vortex generator (1) during the cure time.
 NOTE: The cure time for the mixed adhesive is
____ approximately 15-24 hours at 68°F-80°F (20°C-26.7°C).
 8)  Remove the rubber-tipped clamps, wood strips or equivalent tools from the two shims (9) and vortex generator (1).
 (d)  
Apply a thin layer of sealant to the mating surface of the vortex generator (1).

 (e)  
Put the vortex generator (1) on the air inlet door (8).

 (f)  
Install the six bolts (11), six washers (10), two radius fillers (4) and six nuts (7) that attach the vortex generator (1) to the air inlet door (8).

 (g)  
Install the four bolts (2), four washers (3), four tapered fillers (5) and four nuts (6) that attach the vortex generator (1) to the air inlet door (8).

 (h)  
Remove the unwanted sealant from the vortex generator (1) and air inlet door (8) with a cloth or cotton swabs.

 (i)  
Use a fairing tool to apply a fillet seal between the forward and aft edges of the vortex generator (1) and air inlet door (8) (view A-A).


 S 424-022
 (2)  Do this task: Air Inlet Door Installation (AMM 49-15-22/401).
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 49-15-23
 ALL  ú ú 01 Page 404 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
AIR INLET DOOR ACTUATOR - REMOVAL/INSTALLATION
______________________________________________
 1.  General
_______
 A.  This procedure gives the tasks to remove and to install the air inlet door actuator (which is referred to as the 'actuator'). The actuator is installed aft of the rear pressure bulkhead on the inner side of the fuselage.
 TASK 49-15-31-004-001
 2.  Air Inlet Door Actuator Removal (Fig. 401)
_______________________________
 A.  Access
 (1)  
Location Zones
 101 Control Cabin (Left)
 701 Tail Compartment


 (2)  
Access Panels
 3701 Stabilizer Trim Access Door

 

 B.  Procedure
 S 864-002
 (1)  Set these switches on the P5 forward overhead panel:
 (a)  
Set the BAT switch to the ON position.

 (b)  
Set the APU master switch to the ON position and attach a DO-NOT-OPERATE tag.

 (c)  
After the air inlet door opens, put the BAT switch to the OFF position and attach a DO-NOT-OPERATE tag.


 S 014-003
 (2)
Open the access door to the actuator for the air inlet door.
 
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