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EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 562
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-21-00-710-128-001
(34) Make sure the difference in amperage values is more than 0.5 amps.
SUBTASK 27-21-00-710-129-001
(35) If the difference in amperage values is not more than 0.5 amps, do a trouble-shooting on the
authority limiter.
I. Put the Airplane Back to its Usual Condition
SUBTASK 27-21-00-710-130-001
(1) Put the RUDDER TRAVEL DIRECTION switch, on the test box, SPL-1805, in the OFF position.
NOTE: The green indicator light should go off. The rudder might move slowly to the right or left
as much as 3 degrees.
SUBTASK 27-21-00-710-131-001
(2) Put the YAW DAMPER POWER switch, on the test box, SPL-1805, to the OFF position.
NOTE: The red indicator light should go off.
SUBTASK 27-21-00-840-014-001
(3) Put the YAW DAMPER switch, on the P5 panel, in the OFF position.
SUBTASK 27-21-00-860-160
(4) Set the mode select IRS switches to the OFF position.
SUBTASK 27-21-00-840-015-001
(5) Set the flap control lever to 25 units.
SUBTASK 27-21-00-840-016-001
(6) Put the arm switch for the ALTERNATE FLAPS, on the P5 panel, in the OFF position.
SUBTASK 27-21-00-840-017-001
(7) Put the LANDING GEAR handle, on the P2 panel, in the DN position.
SUBTASK 27-21-00-840-018-001
(8) Set the flap control lever to UP.
NOTE: Wait for the flaps to move.
SUBTASK 27-21-00-840-019-001
(9) Do this task: Hydraulic System A or B Power Removal, TASK 29-11-00-860-805.
SUBTASK 27-21-00-710-132-001
(10) Remove the test box, SPL-1805 from the rudder PCU.
(a) Open these circuit breakers and install safety tags:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 7 C00285 YAW DAMPER AC
D 6 C01354 YAW DAMPER 2 DC
D 7 C00286 YAW DAMPER 1 DC
(b) Verify that all the toggle switches on the test box are in the OFF position.
(c) Disconnect the J1 connector of the test box from the D291 connector.
(d) Disconnect the P1 connector of the test box from the rudder PCU.
(e) Connect the D291 connector to the rudder PCU.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 563
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(f) Remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 7 C00285 YAW DAMPER AC
D 6 C01354 YAW DAMPER 2 DC
D 7 C00286 YAW DAMPER 1 DC
SUBTASK 27-21-00-865-001
(11) Remove the safety tag and close this circuit breaker:
Power Distribution Panel Number 2, P92
Row Col Number Name
F 2 C01449 STANDBY HYDRAULIC PUMP
SUBTASK 27-21-00-840-020-001
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES. THE AILERONS, RUDDER, ELEVATOR, FLAPS, SLATS, SPOILERS,
LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(12) Pressurize the hydraulic systems A and B with the electric motor-driven pump. To pressurize
them, do this task: Hydraulic System A or B Pressurization, TASK 29-11-00-860-801.
SUBTASK 27-21-00-740-002-001
(13) Do the stall management yaw damper (SMYD) servo test/sweep test for SMYD1 to ensure that
the rudder PCU yaw damper is operational. To perform this test, do this task: Stall Management
Yaw Damper (SMYD) BITE Test - Ground Test, TASK 27-32-00-740-803.
SUBTASK 27-21-00-840-021-001
(14) Do this task: Hydraulic System A or B Power Removal, TASK 29-11-00-860-805.
SUBTASK 27-21-00-840-022-001
(15) Put the FLT CONTROL A and B switches, on the P5 panel, to the OFF position.
SUBTASK 27-21-00-410-017-001
(16) Close this access panel:
Number Name/Location
324DR Vertical Fin, Trailing Edge Access
SUBTASK 27-21-00-480-028-001
(17) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-3
Row Col Number Name
A 16 C01345 LANDING GEAR AUTOBRAKE BITE CONT 2
A 18 C00583 LANDING GEAR AUTOBRAKE BITE CONT 1
E 16 C00196 LANDING GEAR ANTISKID INBD
E 18 C00195 LANDING GEAR ANTISKID OUTBD
SUBTASK 27-21-00-480-029-001
(18) Remove the current meter, COM-2531 or clamp meter, COM-3837.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 564
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
　
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本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊2(46)