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时间:2011-04-08 11:56来源:蓝天飞行翻译 作者:航空
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BOLT HOLE 
2  ALIGNMENT 0.250 (6.35)  (14-15 N.m) 120-130 LB-IN.  FWD  1  2  1 
BOLT HOLE  3 
3  0.3125 (7.938)  220-230 LB-IN.  HORIZONTAL FLANGE BOLTS 
HOLE ALIGNMENT  (25-26 N.m)  (RIGHT SIDE) 
4  0.375 (9.52)  440-410 LB-IN.  A 
ALIGNMENT  (45-46 N.m) 
HOLE  GMM-1098435-00-B 

HPC Front Stator Horizontal Flange Bolts and Nuts Installation
Figure 802

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 72-35-00
 ALL  ú ú C01 Page 805 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
2) Put the lever arm on the vane stem.
 3) Engage the lever arm pin in the actuation ring.
 4) Make sure the lever arm fully engages with the vane stem

 tang.
 (c)  
While you hold the lever arm with the countertorque tool to make sure the vane does not turn, install the nut and washer from the vane stem. 1) Tighten the nut to 55-70 pound-inches (6-8 Newton meters).

 (d)  
Make sure that two to three threads of the vane stem comes out of the nut (Fig. 801). 1) Make sure the lever arm correctly engages the vane. 2) If the lever arm does not engage the vane stem tang, do the


 removal and installation procedures again.
 S 418-013-C00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSER. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (5)
Close the right and left thrust reverser (AMM 78-31-00/201).

 S 418-014-C00

 (6)
Close the right and left fan cowl panel (AMM 71-11-02/201).


 TASK 72-35-00-968-015-C00
 3. Horizontal Flange Bolt on the Front Stator Case to the High Pressure
____________________________________________________________________
 Compressor Replacement

______________________
 A. General
 (1)  This procedure is for the removal and installation of one bolt and nut.
 (a)  If you remove more than one bolt remove and install the bolt and nut, before you remove the subsequent bolt and nut.
 B. Equipment
 (1)  Mallet
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 72-35-00
 ALL  ú ú C01 Page 806 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2) A plastic drift
 C.  Consumable Materials
 (1) Graphite grease - CP2101
 D.  References
 (1)
AMM 70-10-01/201, Consumable Materials

 (2)
AMM 71-11-02/201, Fan Cowl Panels

 (3)
AMM 78-31-00/201, Thrust Reverser System


 E.  Access
 (1)  
Location Zones
 502/602 Left Fan Cowl Panel
 503/603 Right Fan Cowl Panel
 504/604 Left Thrust Reverser
 505/605 Right Thrust Reverser
 506 No. 1 Engine
 606 No. 2 Engine


 (2)  
Access Panels
 5737L Engine No. 1 - Right Fan Cowl Panel
 5738L Engine No. 1 - Left Thrust Reverser
 5739L Engine No. 1 - Right Thrust Reverser
 5746L Engine No. 1 - Left Fan Cowl Panel
 5837R Engine No. 2 - Right Fan Cowl Panel
 5838R Engine No. 2 - Left Thrust Reverser
 5839R Engine No. 2 - Right Thrust Reverser
 5846R Engine No. 2 - Left Fan Cowl Panel

 

 F.  Prepare to Remove the Horizontal Flange Bolt and Nut on the Front Stator Case to the HPC (Fig. 802).
 S 018-016-C00
 (1) Open the right and left fan cowl panel (AMM 71-11-02/201).
 S 018-050-C00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU OPEN THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO THE EQUIPMENT CAN OCCUR.
 (2) Open the right and left thrust reverser (AMM 78-31-00/201).
 
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