C. Install the Thrust Management Computer
S 914-010
CAUTION: DO NOT TOUCH THE THRUST MANAGEMENT COMPUTER BEFORE YOU DO THE
_______ PROCEDURE FOR DEVICES THAT ARE SENSITIVE TO ELECTROSTATIC DISCHARGE. ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE THRUST MANAGEMENT COMPUTER.
(1)
Do the procedure for devices that are sensitive to electrostatic discharge (AMM 20-41-01/201).
S 424-006
(2)
Install the thrust management computer (AMM 20-10-01/401).
D. Do a Test of the Thrust Management Computer
S 864-007
(1) Supply electrical power (AMM 24-22-00/201).
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S 864-008
(2) Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P11 panel:
(a)
11A17, AUTOFLIGHT WARN
(b)
11F14, TMC AC
(c)
11F15, TMC DC
(d)
11F16, TMC SERVO
S 864-015
WARNING: THIS TEST USES MOVEMENT OF THRUST LEVERS AND
_______ CAN CAUSE AIRPLANE MOVEMENT IF ENGINES ARE ON OR SPOILER/SPEEDBRAKE MOVEMENT IF PRESSURE TO THE HYDRAULIC SYSTEMS IS ON. REFER TO THE SPOILER/SPEEDBRAKE DEACTIVATION PROCEDURE (AMM 27-61-00/201). ACCIDENTAL ENGINE OPERATION OR SPOILER/SPEEDBRAKE MOVEMENT CAN CAUSE BAD INJURY TO PERSONS.
(3)
Do the deactivation procedure for the spoilers (AMM 27-61-00/201) or move all persons and equipment away from the spoilers.
S 864-016
(4)
Make sure the engines are not on.
S 864-017
(5)
Set the MCDP to OFF or go into Flight Faults Mode to make sure that the MCDP is out of Ground Test Mode.
NOTE: Before the MCDP Ground Test 02 TMC is done, the MCDP
____ must be put out of Ground Test Mode to remove from the MCDP memory problems that have been corrected.
S 714-018
(6) Go into Ground Test Mode and do the MCDP Ground Test 02 TMC (AMM 22-00-02/201).
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E. Put the Airplane Back to Its Initial Condition
S 864-013
(1)
Do the activation procedure for the spoilers if you did the deactivation procedure (AMM 27-61-00/201).
S 414-019
(2)
Close the access panel, 119BL (AMM 06-41-00/201).
S 864-009
(3)
Remove electrical power if it is not necessary (AMM 24-22-00/201).
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THRUST MODE SELECT PANEL - REMOVAL/INSTALLATION
_______________________________________________
1. General
_______
A. The thrust mode select panel (TMSP) is installed on the center instrument panel P3-1. The TMSP is held in position by a mounting clamp. One multi-pin connector is at the rear of the unit.
TASK 22-31-02-004-002
2. Remove the Thrust Mode Select Panel
___________________________________
A. Access
(1) Location Zone
211/212 Flight Compartment
B. Remove the Thrust Mode Select Panel
S 864-001
(1) Open these circuit breakers on the overhead circuit breaker panel, P11, and attach DO-NOT-CLOSE tags:
(a)
11A17, AUTOFLIGHT WARN
(b)
11F14, TMC AC
(c)
11F15, TMC DC
