曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
captain’s rudder forward quadrant.
(c) Remove the rig pins R-3 and R-5.
(d) Adjust the pressure seals at the aft pressure bulkhead with the control cables RA and RB.
To adjust them, do this task: Location of the Flight Control Cables Air Pressure Seals,
TASK 27-09-17-860-801.
(e) Make sure the cables RA and RB do not touch the pulley or the quadrant flanges for the
total cable travel.
(f) Make sure the cables RA and RB are in less than 2 degrees of the plane of the pulley or the
quadrant.
(g) Make sure you install the cables through the grommets in the structure.
(h) Make sure that the cables do not move from the neutral rig position.
(i) Make sure that the pulleys turn freely with sufficient clearance with the guards.
(j) Remove the nut [50], washer [49], washer [48], and bolt assembly [47] to disconnect the
standby rudder PCU control rod [34] from the rudder control torque tube [33].
(k) Remove the nut [45], washer [44], washer [43], and bolt assembly [42] to disconnect the
main rudder PCU control rod [36] from the rudder control torque tube [33].
(l) Move the rudder pedals 25 times through full travel.
(m) Connect the main rudder PCU control rod [36] to the center crank [41].
1) Install the bolt assembly [42] with the bolt head end up and washer [43].
2) Tighten the outer bolt of the bolt assembly [42] to 70 in-lb (7.9 Nm) -- 85 in-lb (9.6 Nm).
3) Install the washers [44] and nut [45].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 513
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
CAUTION: DO NOT TIGHTEN THE OUTER BOLT OF THE BOLT ASSEMBLY [42]
AFTER YOU TIGHTEN THE NUT [45]. THIS CAN CAUSE DAMAGE TO
EQUIPMENT.
4) Tighten the nut [45] to 25 in-lb (2.8 Nm) -- 30 in-lb (3.4 Nm).
(n) Install the bolt assembly [47] with the bolt head end up, washer [48] (under bolt), washer
[49] (under nut), and nut [50] to connect the standby rudder PCU control rod [34] to the
upper crank [46].
SUBTASK 27-21-00-820-009-001
(2) Adjust the control cables RA and RB to their correct cable rigging tension:
(a) Install the rig pin R-5 from the rig pin kit, SPL-1585 in the rudder feel and centering unit.
(b) Adjust the turnbuckles in the cables RA and RB to get the cable tension as given in
(Table 501):
Table 501/27-21-00-993-814-001 737-800 / 737-900 Rudder Cable Rigging Load
Temp Deg F (C) Nominal Lbs (Kg) Minimum Lbs (Kg) Maximum Lbs (Kg)
110 (43.3) 190 (86.1) 180 (81.6) 200 (90.7)
109 (43.8) 190 (86.1) 180 (81.6) 200 (90.7)
108 (42.2) 189 (85.7) 179 (81.2) 199 (90.3)
107 (41.7) 189 (85.7) 179 (81.2) 199 (90.3)
106 (41.1) 188 (85.3) 178 (80.7) 198 (89.8)
105 (40.5) 188 (85.3) 178 (80.7) 198 (89.8)
104 (40.0) 187 (84.8) 177 (80.3) 197 (89.3)
103 (39.4) 187 (84.8) 177 (80.3) 197 (89.3)
102 (38.9) 186 (84.4) 176 (79.8) 196 (88.9)
101 (38.3) 186 (84.4) 176 (79.8) 196 (88.9)
100 (37.8) 185 (83.9) 175 (79.3) 195 (88.4)
99 (37.2) 184 (83.5) 174 (78.9) 194 (88.0)
98 (36.7) 184 (83.5) 174 (78.9) 194 (88.0)
97 (36.1) 183 (83.0) 173 (78.5) 192 (87.5)
96 (35.5) 183 (83.0) 173 (78.5) 193 (87.5)
95 (35.0) 182 (82.5) 172 (78.0) 192 (87.1)
94 (34.4) 182 (82.5) 172 (78.0) 192 (87.1)
93 (33.9) 181 (82.1) 171 (77.6) 191 (86.6)
92 (33.3) 181 (82.1) 171 (77.6) 191 (86.6)
91 (32.8) 180 (81.6) 170 (77.1) 190 (86.2)
90 (32.2) 180 (81.6) 170 (77.1) 190 (86.2)
89 (31.7) 179 (81.2) 169 (76.7) 189 (85.7)
88 (31.1) 179 (81.2) 169 (76.7) 189 (85.7)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 514
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
Temp Deg F (C) Nominal Lbs (Kg) Minimum Lbs (Kg) Maximum Lbs (Kg)
87 (30.5) 178 (80.7) 168 (76.2) 188 (85.3)
86 (30.0) 178 (80.7) 168 (76.2) 188 (85.3)
85 (29.4) 177 (80.3) 167 (75.7) 187 (84.8)
84 (28.9) 177 (80.3) 167 (75.7) 187 (84.8)
83 (28.3) 176 (79.8) 166 (75.3) 186 (84.4)
82 (27.8) 176 (79.8) 166 (75.3) 186 (84.4)
81 (27.2) 175 (79.4) 165 (74.8) 185 (83.9)
80 (26.7) 175 (79.4) 165 (74.8) 185 (83.9)
79 (26.1) 174 (78.9) 164 (74.4) 184 (83.5)
78 (25.5) 174 (78.9) 164 (74.4) 184 (83.5)
77 (25.0) 173 (78.5) 163 (73.9) 183 (83.0)
76 (24.4) 173 (78.5 163 (73.9) 183 (83.0)
75 (23.9) 172 (78.0) 162 (73.5) 182 (82.5)
74 (23.3) 172 (78.0) 162 (73.5) 182 (82.5)
73 (22.8) 171 (77.6) 161 (73.0) 181 (82.1)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(25)
