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(d) Move and hold the captain’s control column aft until it touches the stops.
1) Make sure the left elevator moves 13.16 - 14.87 inches (334.3 - 377.7 mm) up from the
index mark (Figure 523).
(e) Move and hold the captain’s control column forward until it touches the stops.
1) Make sure the left elevator moves 9.90 - 11.08 inches (251.5 - 281.4 mm) down from the
index mark (Figure 523).
(f) Do this task: Put the Elevator Systems A and B Back to the Condition Before the
Pressure Removal, TASK 27-31-00-840-802.
SUBTASK 27-31-00-730-016
(2) Do the elevator travel limit test with hydraulics on:
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.
(a) Pressurize the elevator hydraulic system A. To pressurize it, do the system A portion of this
task: Elevator Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
(b) Move and hold the captain’s control column aft until it touches the stops.
1) Make sure the right elevator moves up 13.73 - 14.87 inches (348.7 - 377.7 mm) from the
index mark (Figure 523).
(c) Move and hold the captain’s control column forward until it touches the stops.
1) Make sure the right elevator moves down 10.18 - 11.08 inches (258.6 - 281.4 mm) from
the index mark (Figure 523).
(d) Set the FLT CONTROL B switch on the forward overhead panel, P5, to the ON position.
(e) Set the FLT CONTROL A switch on the forward overhead panel, P5, to the OFF position.
(f) Move and hold the captain’s control column aft until it touches the stops.
1) Make sure the right elevator moves up 13.73 - 14.87 inches (348.7 - 377.7 mm) from the
index mark (Figure 523).
(g) Move and hold the captain’s control column forward until it touches the stops.
1) Make sure the right elevator moves down 10.18 - 11.08 inches (258.6 - 281.4 mm) from
the index mark (Figure 523).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-059
(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 27-31-00-410-010
(2) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
TASK 27-31-00-700-805
15. Elevator Output Torque Tube Buss Linkage - Test
(Figure 502)
A. General
(1) Use this test to do a check of the elevator output torque tube buss linkage.
B. References
Reference Title
27-31-00-700-801 Null Procedure - Mach Trim Actuator (P/B 201)
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. 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
COM-1557 Gauge - Force
(Part #: DG-200, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPP-500G, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPPH-150, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPPH-50, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: FDIX 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDIX 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDV 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Opt Part #: FDI 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
SPL-1677 Assembly - Trammel Bar, Stabilizer Trim Actuator
(Part #: F80055-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
STD-1278 Block - Loading, 1/8 Inch Thick, 3 Inch by 3 Inch Wood or Fiberglass
Block with Pad to Prevent Damage to the Skin.
D. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
311 Area Aft of Pressure Bulkhead - Left
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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