(c)  
See that the applicable warning light on the P5 panel is off when the door is latched.

 S 865-043-B00
 (2)  
Open the door to the cocked position.

 S 715-044-B00

 (3)  
Do a test of the snubber.

 (a)  
Try to move the door quickly from the cocked position.

 (b)  
Feel that the snubber operates to make the door move slowly.

 (c)  
Move the door slowly from the cocked position.

 (d)  
Make sure you cannot feel the operation of the snubber.

 (e)  
Replace the snubber if it does not operate correctly.

 S 715-045-B00
 (4)  
Do a check of the torque that is necessary to operate the handle.

 (a)  
Install the torque wrench C52008-1 on the internal door handle.

 (b)  
Open the door to the cocked position.

 1)  See that the torque you use is not more than 360 pound-inches.

 (c)  
Open the door fully.

 1)  See that the torque you use is not more than 600 pound-inches.

 (d)  
Close the door.

 1)  See that the torque you use is not more than 600 pound-inches.

 (e)  
Remove the torque wrench C52008-1.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-41-00
 ALL  ú ú B02A Page 507 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
RIGGING SUMMARY - GALLEY SERVICE DOOR
CHECK  ADJUSTMENT  NECESSARY CONDITION  POSITION DOOR 
FIG.  NAME  FIG. 
LATCH ROD 
502  LATCH ROD ADJUSTMENT  508  1. THE LATCH ROD END PLAY MUST BE LESS THAN 0.02 INCH. OPEN 
0.25 INCH OR MORE. 2. EACH LATCH ROLLER MUST ENGAGE ITS LATCH FITTING BY  LATCHED 
LATCH CRANK AND DOOR 
503  OVERCENTER LATCH CRANK ADJUSTMENT  509  3. THE HOLE IN THE LATCH CRANK MUST ALIGN WITH THE HOLE IN THE DOOR WHEN THE HANDLE IS IN THE LATCHED POSITION. (DOOR OPEN) LATCHED 
ADJUSTMENT PARALLEL  510  4. THE FORWARD AND AFT LATCH ROLLERS MUST ENTER THE LATCH FITTINGS AT THE SAME TIME. ALMOST CLOSED 
DOOR CLEARANCE 
504  FILE THE DOOR  --- 5. THE FORWARD AND AFT EDGES OF THE DOOR MUST HAVE THE CORRECT CLEARANCE AS SHOWN IN FIGURE 504.  LATCHED 
ADJUSTMENT VERTICAL  511  6. THE GATE CLEARANCE MUST BE AS SHOWN AS FIGURE 504. LATCHED 
COVER FILE HINGE  --- FIGURE 504. 7. THE HINGE COVER CLEARANCE MUST BE AS SHOWN IN LATCHED 
DOOR FLUSHNESS 
505  DOOR FLUSHNESS ADJUSTMENT  512  8. THE FORWARD AND AFT EDGES MUST HAVE THE CORRECT FLUSHNESS AS SHOWN IN FIGURE 505. LATCHED 
ADJUSTMENT GATE FLUSHNESS  513  9. THE GATE FLUSHNESS MUST BE AS SHOWN IN FIGURE 505.  LATCHED 
LATCH HANDLE 
506  ADJUSTMENT LATCH HANDLE  514  10. EACH LATCH ROLLER MUST CLEAR THE ENTRY LIP OF ITS LATCH FITTING.  CLOSING 
11. EACH LATCH ROLLER MUST BE IN ITS LATCH FITTING BEFORE THE LATCH ROD STARTS TO TURN.  CLOSING 
12. THE FORCE TO RETRACT THE EXTERNAL HANDLE MUST BE LESS THAN 20 POUNDS.  LATCHED 
LATCH ROLLER CLEARANCE 
507  ADJUSTMENT CLEARANCE LATCH ROLLER  515  13. EACH LATCH ROLLER MUST BE 0.04 TO 0.28 INCH FROM THE BOTTOM OF THE LATCH FITTING. LATCHED 
STOP PINS 
ADJUSTMENT VERTICAL 511  AS SHOWN IN FIGURE 507. 14. EACH DOOR STOP PIN MUST ALIGN WITH THE STOP PAD TARGET  LATCHED 
ADJUSTMENT STOP PIN  516  15. EACH STOP PIN MUST BE 0.015 TO 0.030 INCH FROM ITS STOP PAD. LATCHED 

Adjustment Summary - Galley Service Door
Figure 501A

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-41-00
 ALL  ú ú B02A Page 508 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
B48168
A

737-300/400/500
MAINTENANCE MANUAL

STOP PIN ADJUSTMENT (STOP PIN) TOP GATE
GATE FLUSHNESS ADJUSTMENT (GATE PUSH ROD)
　
中國航空網 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 艙門 DOORS 1(127)