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a) Push the LSK adjacent to PREV MENU on test 51.16 screen.
b) Push the LSK adjacent to PREV MENU on the ELEVATOR RIGGING screen.
c) Push the LSK adjacent to CONTINUE on the RIGGING INDEX screen.
d) Push the LSK adjacent to EXIT on the RIGGING INDEX screen.
e) Push the LSK adjacent to CONTINUE on the END OF BITE RIGGING screen.
f) Push the LSK adjacent to EXIT until you get out of the BITE test.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-086
(1) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
SUBTASK 27-31-00-410-016
(2) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
TASK 27-31-00-700-811
21. Feel Differential Pressure Light - Test
A. General
(1) Use this test to make sure the FEEL DIFF PRESS light operates correctly.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 587
Feb 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
B. References
Reference Title
27-31-00-800-801 Elevator Hydraulic System A and B - Pressurization (P/B 201)
27-31-00-840-801 Put the Elevator Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
334 Left Horizontal Stabilizer - Elevator
344 Right Horizontal Stabilizer - Elevator
D. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
E. Prepare for the Test
SUBTASK 27-31-00-860-087
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SPOILERS, SLATS, AND THRUST REVERSERS CAN MOVE
QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO
PERSONS AND DAMAGE TO EQUIPMENT.
(1) Pressurize elevator hydraulic systems A and B. To pressurize them, do this task: Elevator
Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
SUBTASK 27-31-00-010-018
(2) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
F. Feel Differential Pressure Light Test
GUN ALL; AIRPLANES WITH THE ELEVATOR FEEL SHIFT MODULE
SUBTASK 27-31-00-860-153
(1) Set the FLT CONTROL B switch on the forward overhead panel, P5, to the OFF position.
(a) Make sure the FEEL DIFF PRESS light on the forward overhead panel, P5, illuminates after
a minimum of 35 seconds.
NOTE: The time required for the system to bleed down will vary. It may take up to 120
seconds for the FEEL DIFF PRESS light to illuminate.
GUN ALL
SUBTASK 27-31-00-860-155
(2) Set the FLT CONTROL A switch to the OFF position.
(a) Make sure the FEEL DIFF PRESS light goes off.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 588
Feb 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-31-00-860-156
(3) Set the FLT CONTROL B switch to the ON position.
(a) Wait for a minimum of 35 seconds.
(b) Make sure the FEEL DIFF PRESS light comes on.
NOTE: The time required for the system to bleed down will vary. It may take up to 120
seconds for the FEEL DIFF PRESS light to illuminate.
SUBTASK 27-31-00-860-157
(4) Set the FLT CONTROL A switch to the ON position.
(a) Make sure the FEEL DIFF PRESS light goes off.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-089
(1) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
SUBTASK 27-31-00-410-017
(2) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
TASK 27-31-00-790-801
22. Pitot System Leak - Test
(Figure 515)
A. General
(1) Use this test to do a leak check of the pitot system.
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1742 Regulator - Air Pressure, Elevator Feel Computer
　
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