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A
747-400
MAINTENANCE MANUAL
(b) The alternate landing gear subsystem has these sensors:
1) The alternate uplock sensors:
-S1636 LH Body Gear
-S1637 RH Body Gear
-S1638 LH Wing Gear
-S1639 RH Wing Gear.
2) The alternate downlock sensors:
-S412 RH Wing Gear
-S413 RH Body Gear
-S414 LH Body Gear
-S415 LH Wing Gear.
3) The alternate tilt sensors:
-S612 LH Body Gear Tilt
-S613 RH Body Gear Tilt
-S614 RH Wing Gear Tilt
-S615 LH Wing Gear Tilt.
4) The alternate nose gear up sensor:
-S411 Nose Gear Up.
5) The alternate nose gear lock sensor:
-S424 Nose Gear Lock.
6) The alternate nose gear squat sensor:
-S801 Nose Gear Squat.
7) The alternate nose door sensor:
-S425 RH Nose Door Warning.
8) The alternate body gear door sensors:
-S427 RH Body Door Warning
-S428 LH Body Door Warning.
9) The alternate wing gear door sensors:
-S395 L Wing Door Warning
-S426 R Wing Door Warning.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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747-400 MAINTENANCE MANUAL
(c) The thrust reverser and auto restow subsystems have these sensors:
1) The auto restow sensors:
-
S1604 Eng No. 1 LH T/R Stowed
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S1604 Eng No. 2 LH T/R Stowed
-
S1604 Eng No. 3 LH T/R Stowed
-
S1604 Eng No. 4 LH T/R Stowed
-
S1605 Eng No. 1 RH T/R Stowed
-
S1605 Eng No. 2 RH T/R Stowed
-
S1605 Eng No. 3 RH T/R Stowed
-
S1605 Eng No. 4 RH T/R Stowed.
2) The lock sensors:
-
S1607 Eng No. 1 LH Actuator Lock
-
S1607 Eng No. 2 LH Actuator Lock
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S1607 Eng No. 3 LH Actuator Lock
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S1607 Eng No. 4 LH Actuator Lock
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S1608 Eng No. 1 RH Actuator Lock
-
S1608 Eng No. 2 RH Actuator Lock
-
S1608 Eng No. 3 RH Actuator Lock
-
S1608 Eng No. 4 RH Actuator Lock.
3) The deploy sensors:
-
S1609 Eng No. 1 LH Cowl Deployed
-
S1609 Eng No. 2 LH Cowl Deployed
-
S1609 Eng No. 3 LH Cowl Deployed
-
S1609 Eng No. 4 LH Cowl Deployed
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S1610 Eng No. 1 RH Cowl Deployed
-
S1610 Eng No. 2 RH Cowl Deployed
-
S1610 Eng No. 3 RH Cowl Deployed
-
S1610 Eng No. 4 RH Cowl Deployed.
(2)
The logic/driver operation mixes sensor logic signals and discrete switch inputs. This supplies discrete outputs for control systems and indication (Fig 3).
(a)
The discrete input signals are as follows:
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