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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(b)
For the position resolver of the No. 2 thrust lever, the
connection will be made at P1 of the connector T1743.
(c)
For the position resolver of the No. 3 thrust lever, the
connection will be made at P1 of the connector T1744.
(d)
For the position resolver of the No. 4 thrust lever, the
connection will be made at P1 of the connector T1745.
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(3)
Move all four thrust levers forward to the full forward thrust position.
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(4)
Make sure the API display values are in limits that follow:
(a)
85.0 |1.00 degrees for the position resolvers of the No. 1 and 2 thrust levers
(b)
5.0 |1.00 degrees for the position resolvers of the No. 3 and 4 thrust levers
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(5)
Retract all four forward thrust levers to the idle position.
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(6)
Make sure the API display values are in limits that follow:
(a)
34.82 |0.75 degrees for No. 1 and 2 resolvers.
(b)
55.18 |0.75 degrees for No. 3 and 4 resolvers.
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(7) Disconnect the electrical connectors for the interlock actuators of the reverse thrust lever as follows:
(a)
DM7986
(b)
DM7987
(c)
DM7988
(d)
DM7989
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WARNING: MAKE SURE TO KEEP PERSONS AND EQUIPMENT AWAY FROM THE INTERLOCK
_______ ACTUATORS OF THE REVERSE THRUST LEVER DURING THE OPERATION. THE INTERLOCK ACTUATOR OPERATES IN LESS THAN ONE SECOND. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(8) Motor each interlock actuator for the reverse thrust lever to the extend position.
(a)
Apply 28 volts dc to the pin 8 of each connector.
(b)
Ground the pins 6 and 10 of each connector.
(c)
Remove the 28 volts dc power source from each connector.
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(9) Move all four reverse thrust levers to the full reverse thrust position.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
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(10) Make sure the API display values are in limits that follow:
(a)
4.56 |0.81 degrees for the position resolvers of the No. 1 and 2 thrust levers
(b)
85.44 |0.81 degrees for the position resolvers of the No. 3 and 4 thrust levers
S 865-040-N00
(11)
Move all four reverse thrust levers back to the stow position.
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(12)
Motor each interlock actuator to the retracted position.
(a)
Apply 28 volts dc to the pin 6 of each connector.
(b)
Ground the pins 8 and 10 of each connector.
(c)
Remove the 28 volts dc power source from each connector.
S 435-042-N00
(13) Connect the electrical connectors of the interlock actuators with the steps that follow:
(a)
DM7986
(b)
DM7987
(c)
DM7988
(d)
DM7989
S 865-043-N00
(14) Move the No. 1 thrust lever forward from the idle position until the API shows a value of 80.00 degrees.
NOTE: Move the thrust levers forward smoothly from the idle
____ position to prevent hysteresis during the thrust lever adjustment. If more than 80.00 degrees occurs, put the thrust lever back to the idle position and do this step again.
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本文链接地址:747-400 AMM 飞机维护手册 发动机控制 ENGINE CONTROLS(18)