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44 (7) 119 (54) 99 (45)
45 (7) 120 (54) 100 (45)
46 (8) 120 (54) 100 (45)
47 (8) 121 (55) 101 (46)
48 (9) 121 (55) 101 (46)
49 (9) 121 (55) 101 (46)
50 (10) 122 (55) 102 (46)
51 (11) 122 (55) 102 (46)
52 (11) 123 (56) 103 (47)
53 (12) 123 (56) 104 (47)
54 (12) 124 (56) 104 (47)
55 (13) 124 (56) 104 (47)
56 (13) 124 (56) 104 (47)
57 (14) 125 (57) 105 (48)
58 (14) 125 (57) 105 (48)
59 (15) 126 (57) 106 (48)
60 (16) 126 (57) 106 (48)
61 (16) 127 (58) 107 (49)
62 (17) 127 (58) 107 (49)
63 (17) 127 (58) 107 (49)
64 (18) 128 (58) 108 (49)
65 (18) 128 (58) 108 (49)
66 (19) 129 (59) 109 (49)
67 (19) 129 (59) 109 (49)
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(Continued)
Temperature Deg F (C) Maximum Lbs (Kg) Minimum Lbs (Kg)
68 (20) 130 (59) 110 (50)
69 (21) 130 (59) 110 (50)
70 (21) 130 (59) 110 (50)
71 (22) 131 (59) 111 (50)
72 (22) 131 (59) 111 (50)
73 (23) 132 (60) 111 (50)
74 (23) 132 (60) 112 (51)
75 (24) 133 (60) 113 (51)
76 (24) 133 (60) 113 (51)
77 (25) 133 (60) 113 (51)
78 (26) 134 (61) 114 (52)
79 (26) 134 (61) 114 (52)
80 (27) 135 (61) 115 (52)
81 (27) 135 (61) 115 (52)
82 (28) 136 (62) 116 (53)
83 (28) 136 (62) 116 (53)
84 (29) 136 (62) 116 (53)
85 (29) 137 (62) 117 (53)
86 (30) 137 (62) 117 (53)
87 (31) 138 (63) 118 (54)
88 (31) 138 (63) 118 (54)
89 (32) 139 (63) 119 (54)
90 (32) 139 (63) 119 (54)
91 (33) 140 (64) 120 (54)
92 (33) 140 (64) 120 (54)
93 (34) 140 (64) 120 (54)
94 (34) 141 (64) 121 (55)
95 (35) 141 (64) 121 (55)
96 (36) 142 (64) 122 (55)
97 (36) 142 (64) 122 (55)
98 (37) 143 (65) 123 (56)
99 (37) 143 (65) 123 (56)
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(Continued)
Temperature Deg F (C) Maximum Lbs (Kg) Minimum Lbs (Kg)
100 (38) 143 (65) 123 (56)
101 (38) 144 (65) 124 (56)
102 (39) 144 (65) 124 (56)
103 (39) 145 (66) 125 (57)
104 (40) 145 (66) 125 (57)
105 (41) 146 (66) 126 (57)
106 (41) 146 (66) 126 (57)
107 (42) 147 (67) 127 (58)
108 (42) 147 (67) 127 (58)
109 (43) 147 (67) 127 (58)
110 (43) 148 (67) 128 (58)
(g) Adjust the pitch force transducers. To adjust them, do this task: Pitch Force Transducer
Adjustment (DFCS BITE Test), TASK 22-11-92-820-801.
(h) Make sure the tension of control cables EA and EB are same as shown on the table above
(Table 501).
(i) Make sure you can move the rig pins E-1, E-2, E-3, and E-5 freely.
(j) Remove the rig pins E-2 and E-3.
(k) Install the bolts [4], washers [5], and nuts [6].
(l) Install the locking clips on the turnbuckles.
(m) Remove the rig pins E-1 and E-5.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-410-001
(1) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-00-940-001
(2) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-940-002
(3) Close this access panel:
Number Name/Location
112A Forward Access Door
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SUBTASK 27-31-00-860-019
(4) Do this task: Put the Elevator Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-31-00-840-802.
------------------------- END OF TASK ---------------------------
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Elevator Control Cables Adjustment
Figure 501 (Sheet 1 of 2)/27-31-00-990-803
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Elevator Control Cables Adjustment
Figure 501 (Sheet 2 of 2)/27-31-00-990-803
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(136)
