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(Part #: F71336-501, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-2036 Protector - Horizontal Stabilizer Hinge Pin Thread
(Part #: C27054-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
STD-1238 Indicator - Dial
B. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
D00015 Grease - Aircraft Bearing BMS3-24
D00633 Grease - Aircraft General Purpose BMS3-33
D50004 Compound - Antiseize BMS3-28
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
333 Left Horizontal Stabilizer - Rear Spar to Trailing Edge
343 Right Horizontal Stabilizer - Rear Spar to Trailing Edge
D. Access Panels
Number Name/Location
331A Horizontal Stabilizer, Gap Cover
331AZ Horizontal Stabilizer, Access Panel, Inboard L.E. Closure Rib
332AB Horizontal Stabilizer, Gap Cover, Horizontal Stabilizer to Body
341A Horizontal Stabilizer, Gap Cover
341AZ Horizontal Stabilizer, Access Panel - Inbd L.E. Closure Rib
342AB Horizontal Stabilizer, Gap Cover - H. Stab. to Body
E. Hinge Fitting Installation
(Figure 402)
NOTE: You must do the removal and installation of the hinge fitting on one side at a time.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-41-31-420-001
(1) Install the hinge fitting [24]:
(a) Lubricate the bolt threads of bolt [29] and bolt [40] with grease, D00633.
(b) Put the hinge fitting [24] in its position.
(c) Install the bolt [29], washer [30] (under the bolt), washers [31] (3 maximum under nut), nut
[32].
1) Tighten the nut [32] to 2200 in-lb (248.6 N
m) -- 3300 in-lb (372.8 N
m).
2) Install the new pin [33].
NOTE: Tighten nut [32] if it is necessary to get the pin hole alignment but do not
exceed 5300 in-lb (598.8 N
m).
(d) Install the bolt [41], washer [42] (under the bolt), washers [43] (3 maximum under nut), and
nut [44].
1) Tighten the nut [44] to 6450 in-lb (728.7 N
m) -- 6400 in-lb (723.1 N
m).
2) Install the new pin [45].
NOTE: Tighten nut [44] if it is necessary to get the pin hole alignment but do not
exceed 8600 in-lb (971.7 N
m).
SUBTASK 27-41-31-420-002
(2) Install the fail safe link [10] to the hinge fitting [24]:
(a) Lubricate the bolt [12] and bolt threads with grease, D00633.
(b) Apply sealant, A00247 to the bolt [4] and bolt [9].
(c) Put the fail safe link [10] and filler [11] on the hinge fitting [24].
(d) Install the bolt [12], washer [13] (under the bolt), washers [14] (3 maximum under nut), and
nut [15].
1) Tighten the nut [15] to 1300 in-lb (146.9 N
m) -- 1530 in-lb (172.9 N
m).
2) Install the new pin [56].
NOTE: Tighten nut [15] if it is necessary to get the pin hole alignment but do not
exceed 2000 in-lb (226.0 N
m).
(e) Install the bolt [4], washer [5] (under the bolt), washer [6] (under the nut), and nut [7].
1) Tighten the nut [7] to 370 in-lb (41.8 N
m) -- 690 in-lb (78.0 N
m).
(f) Install the bolt [9], washer [5] (under the bolt), washers [6] (under the nut), bonding jumper
[8] (between washers [6]), and nuts [7].
1) Tighten the nut [7] to 370 in-lb (41.8 N
m) -- 690 in-lb (78.0 N
m).
2) Use bonding meter, COM-1550 to make sure the resistance between the free end of the
bonding jumper [8] and fail safe link [10] is not greater than 0.00216 ohms.
3) Apply sealant, A00247 at the end of the bonding jumper [8].
SUBTASK 27-41-31-420-003
(3) Install the thrust brace fitting [51] on the hinge fitting [24]:
(a) Lubricate the bolts [47] with sealant, A00247.
(b) Put the thrust brace fitting [51] and shim [46] on the hinge fitting [24].
1) Remove or add shim [46] until you can install the bolt [34] and bolt [40] easily.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-31
Page 412
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(c) Install the bolts [47], washers [48] (under the bolt), washers [49] (under the nut), and nuts
[50].
1) Tighten the nuts [50] to 630 in-lb (71.2 N
m) -- 1070 in-lb (120.9 N
m).
SUBTASK 27-41-31-420-004
(4) Connect the upper thrust brace [38] and lower thrust brace [39] to the thrust brace fitting:
(a) Lubricate the bolt [34], bolt [40], and bolt threads with grease, D00015.
(b) Put the lower thrust brace [39] and upper thrust brace [38] in their positions.
　
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