757
MAINTENANCE MANUAL
LEFT RIGHT
ENGINE THRUST ENGINE THRUST
MICROSWITCHES (20 LOCATIONS)
PIN ARRANGEMENT FOR EACH SWITCH (EXAMPLE) (EXAMPLE) MICROSWITCH PACK - SWITCH OPERATION MODES
POSITION OF MICROSWITCH WHEN THE
ASSEMBLY ARM IS IN THE RELEASED STATE.
POSITION OF MICROSWITCH WHEN THE ASSEMBLY
ARM IS IN THE PUSHED IN (ACTIVATED) STATE.
Microswitch Pack Assembly Switches
Figure 202 (Sheet 3)
H02215
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-32-04
ALL ú ú 05 Page 206 ú Jan 20/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
MICROSWITCH ACTIVATION ARM
SWITCH/TRUNNION HOUSING
TRAVEL SEE
SPRING
CHANNEL
TRUNNION
MOUNTING
ARM
ADJUSTING BOLTS
MICROSWITCH PACK - MOUNTING ARM/TRUNION DETAIL
INITIAL ADJUSTMENT RANGE
ADJUSTING BOLT ADJUSTMENT DIRECTIONS: . CW DIRECTION - PUSHES IN THE MICROSWITCH ACTIVATION ARM. . CCW DIRECTION - RELEASES THE MICROSWITCH ACTIVATION ARM.
Microswitch Pack Assembly Switches
Figure 202 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-32-04
ALL ú ú 03 Page 207 ú Jan 20/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
H02152
A
757
MAINTENANCE MANUAL
TASK 22-32-04-402-014
2. Microswitch Pack Assembly Installation
______________________________________
A. Equipment
(1)
VTVM, Model 427A
Hewlett Packard
1501 Page Mill Rd.
Palo Alto, CA 94304
(2)
Rig Pin AT1 - P/N B20003-25, part of kit
B20003-67 (Ref 20-10-24)
B. Access
(1)
Location Zones
113/114 Area Forward of NLG Wheel Well
211/212 Flight Compartment
(2)
Access Panel 113AL Flight/Landing Gear/Engine Control Components
C. Install the Microswitch Pack Assembly (Fig. 201)
S 432-042
(1) Put the microswitch pack in position and attach the four bolts, washers, and nuts.
D. GUN 001-010, 101-104 PRE-SB 78-32;
Microswitch Adjustment (Fig. 204)
NOTE: Make sure the correct Figure and Sheet is selected for the
____ airplane being tested. The airplane information is located on the lower left corner of the page.
S 862-102
(1)
Make sure the thrust lever rod is adjusted correctly (AMM 76-11-00/501).
S 482-133
(2)
With the throttle in the idle position, put the rig pin AT1 through the autothrottle side frames and cams.
S 482-134
(3)
The rig pin must be installed so that the autothrottle clutch link is in the center.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-32-04
ALL ú ú 13 Page 208 ú Sep 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
NO NC S14: SPEED BRAKE RETRACT RIGHT
NO NC S10: SPEED BRAKE RETRACT LEFT
NO NC S17: LOAD SHED/PRESSURE CONTROL LEFT
NO NC S1: LANDING WARNING LEFT
NC NO S16: TMS RIGHT THRUST REVERSER
NC NO S12: TMS LEFT THRUST REVERSER
NO NC S2: LEFT AUTOBRAKE/AUTOBRAKE RTO
NO NC S3: LEFT AUTOBRAKE/AUTOBRAKE RTO
NO NC S19: ECC OFF LEFT
P1 CONNECTOR ____ SWITCH MODES SHOWN WITH THROTTLE
NOTE: AT IDLE POSITION (O` A/T CAM POSITION).
Microswitch Pack - Wire Schematic Figure 203 (Sheet 1)
F59182
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 2(137)
