-80 -40 0 40 80 120 160
AMBIENT TEMPERATURE (`F) RIG LOAD VS AMBIENT TEMPERATURE
NOTE: THE TEMPERATURE OF THE AREA OF THE AIRPLANE WHICH IS NOT PRESSURIZED, MUST BE |10`F OF THE AMBIENT TEMPERATURE. THE TEMPERATURE MUST BE STABLE FOR AT LEAST ONE HOUR BEFORE YOU CAN RIG THE CABLES.
Stabilizer Body Cable Rigging
Figure 503
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STAB TRIM LEVERS ú
27-41-00
ON THE CONTROL STAND ú ú 02 Page 507 ú May 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
SEE A
COLUMN CONTROL CAPTAIN'S FIRST-OFFICER'S CONTROL COLUMN
SEE B A
A A
COLUMN CONTROL CAPTAIN'S CAM SURFACE CAM ROLLER
STOP STOP
B B
E/ST6 RIG PIN A-A FWD S335, S10237 (CAPTAIN) FWD SWITCHES: BOLT ACTUATING SWITCH S338, S10235 (FIRST OFFICER) B S337, S10234 (FIRST OFFICER) S334, S10236 (CAPTAIN) AFT SWITCHES: BOLT ACTUATING BOLT SWITCH STOP
Stabilizer-Trim Cutoff Switches Figure 504 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-00
ALL ú ú 02 Page 508 ú Sep 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
S338 S337
S335 S334
B-B
TABLE 1 SWITCH CONTINUITY REQUIREMENTS
CONTROL COLUMN POSITION FORWARD SWITCHES (S335, S338, S10235, S10237) AFT SWITCHES (S334, S337, S10234, S10236)
RIG POSITION (RIG PIN E/ST6 INSTALLED) CONTINUITY CONTINUITY
3.5 - 4.0 DEGREES FWD OF RIG POSITION CONTINUITY NO CONTINUITY
2.2 - 2.7 DEGREES AFT OF RIG POSITION NO CONTINUITY CONTINUITY
Stabilizer-Trim Cutoff Switches
Figure 504 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-00
ALL ú ú 02 Page 509 ú Sep 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
(2) The Operational Test for the Stabilizer Trim Control System contains these topics:
-Stabilizer Trim Electrical Operation
-Alternate-Electrical Operation
-Manual Operation and Mechanical Travel Limits
-Alternate-Electric Operation and Travel Limits
-Manual Override Operation
-Alternate-Electric Trim Authority
-
Stabilizer Trim Secondary Brake
-
Stabilizer Trim Shutoff Switches
-Manual-Mechanical Stabilizer Trim Control
-Electrical Travel Limits
-
Stabilizer Trim Cutoff Switches
-
Stabilizer Trim Override Capability with Split Control Column Commands
B.
References
(1)
24-22-00/201, Electrical Power - Control
(2)
29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
C.
Access
(1)
Location Zones
211/212 Control Cabin
PROTRACTOR
PENDULUM
(EXAMPLE)
Protractor Installation - Fore and Aft Control Measurement
Figure 505
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-00
ALL ú ú 02 Page 510 ú Sep 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
D. Stabilizer Trim Electrical Operation Test
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 4(6)
