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20-10-51-400-804 Flareless Tubing Assembly Installation (P/B 401)
27-31-00-700-812 Feel Force System - Test (P/B 501)
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-00-840-802 Put the Elevator Systems A and B Back to the Condition Before the
Pressure Removal (P/B 201)
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-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
SPL-1673 Pin - Safety, Elevator Feel Computer
(Part #: F80153-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
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)
C. Consumable Materials
Reference Description Specification
D00153 Fluid - Hydraulic, Erosion Arresting, Fire Resistant BMS3-11, Type
IV
(interchange~
able&
intermixable
with Type V)
G01048 Lockwire - Corrosion Resistant Steel (0.032 In. Dia.) NASM20995~
C32
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 Computer assembly 27-31-37-01-155 GUN 001-028, 101-121,
155-157, 201-999
9 Packing 27-31-37-01-225 GUN 001-028, 101-121,
155-157, 201-999
14 Packing 27-31-37-01-260 GUN 001-028, 101-121,
155-157, 201-999
17 Packing 27-31-37-01-225 GUN 001-028, 101-121,
155-157, 201-999
19 Packing 27-31-37-01-225 GUN 001-028, 101-121,
155-157, 201-999
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
E. Location Zones
Zone Area
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
F. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
G. Elevator Feel Computer Installation
SUBTASK 27-31-37-860-004
(1) Make sure that pressure is removed from the elevator hydraulic systems A and B. To remove it,
do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-37-860-005
(2) Use the bar, SPL-1677 to make sure that the B dimension is at 39.89 +/- 0.01 inches (1013.21 +/-
0.25 millimeters) (Figure 401).
SUBTASK 27-31-37-420-001
(3) If the packings, filters, unions, and reducers are not installed in the elevator feel computer
assembly [1], then do these steps:
(a) Lightly lubricate the new packings with fluid, D00153.
(b) Install these items in the elevator feel computer assembly [1]:
1) The packings [9] and reducers [10] to the fittings for the computer pressure lines
2) The filters [11], new packings [12], and unions [13] to the fittings for the hydraulic lines
3) The new packings [14] and unions [15] to the fittings for the return lines
4) The new packings [17] and unions [18] to the fittings for the static lines
5) The new packings [19] and unions [20] to the fittings for the pitot lines.
SUBTASK 27-31-37-080-001
(4) Remove the pin, SPL-1673 from the input arm [8] and the elevator feel computer assembly [1].
SUBTASK 27-31-37-480-002
(5) Install the rig pin E-4 from the test set rig pin kit, SPL-1585 in the input arm [8] and the elevator
feel computer assembly [1].
SUBTASK 27-31-37-420-002
(6) Install the elevator feel computer assembly [1]:
(a) Put the elevator feel computer assembly [1] in its position.
(b) Install the bolts [3], washers [4] (under the bolt), washers [5] (under the nut), and nuts [6] to
attach the elevator feel computer assembly [1] to the airplane structure.
(c) Connect the stabilizer pushrod [2] to the input arm [8]:
1) If you cannot install the bolt [21], do these steps to adjust the length of the stabilizer
pushrod [2]:
a) Loosen the checknut [24] on the stabilizer pushrod [2].
b) Turn the rod end fitting of the stabilizer pushrod [2] until you can install the bolt [21]
easily by hand.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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