(b)
Push the LSK adjacent to <INDEX.
(c)
Push the LSK adjacent to <MAINT.
(d)
Push the LSK adjacent to <DFCS.
(e)
Push the NEXT PAGE key.
(f)
Make sure that the OVERNIGHT MAINT 2/2 page shows on the CDU.
S 745-024
(2) Get access to COMPLETE ELEV RIG:
(a)
Push the LSK adjacent to <RIGGING.
(b)
Continue with the instructions on the FMCS CDU.
(c)
Push the LSK adjacent to <ELEVATOR.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-11-14
ALL ú ú 07 Page 507 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(d)
Continue with the instructions on the CDU.
(e)
Push the LSK adjacent to <COMPLETE ELEV RIG.
S 745-025
(3) Do test 51.01 through 51.04:
NOTE: Three-unit of trim is the same as a B dimension of
____
41.57 +/-0.01 inches (AMM 27-41-81/401).
NOTE: Test 51.04 is for the sensor signal and the mechanical offset
____ check. Two degrees of feedback sensor signal will cancel the elevator movement of 2 degrees.
(a) Continue with the instructions until test 51.04 shows on the CDU.
S 825-026
(4) Adjust the sensor:
(a)
Lightly loosen the screw on the sensor clamp.
(b)
Turn the sensor housing clockwise slowly until the CDU display shows -1.35 +/-0.05 volts.
NOTE: At the end of the sensor shaft, you can find the
____ index mark on the sensor housing. Turn the sensor counterclockwise approximately 6 degrees against the index mark on the sensor clamp.
(c)
Tighten the clamp screw 8 to 12 pound-inches.
(d)
Remove the lockwire from the thumb nut on the microadjustment rod.
(e)
Turn the thumb nut until you get -1.35 +/-0.03 volts.
(f)
Install the lockwire on the thumb nut.
(g)
Push the INIT REF key on the CDU to get out of the BITE.
(h)
Install the 3802 access door on the tail cone.
TASK 22-11-14-715-027
4. Elevator Neutral Shift Sensor Test - BITE TEST
______________________________________________
A. References
(1) 22-11-00/501 or 22-11-01/501, Digital Flight Control System
B. Access
(1) Location Zone
101 Control Cabin - Left
102 Control Cabin - Right
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-11-14
ALL ú ú 04 Page 508 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
C. Procedure
S 745-033
(1)
Do the preparation for the DFCS BITE Test in this task:
"Operational Test - Digital Flight Control System"
(Ref 22-11-00/501 or 22-11-01/501).
S 745-030
(2)
Get access to the DFCS BITE TEST LINE MAINT 1/2 page:
(a)
Push the INIT REF key on the CDU.
(b)
Push the LSK adjacent to <INDEX.
(c)
Push the LSK adjacent to MAINT>.
(d)
Push the LSK adjacent to <DFCS.
(e)
Make sure that the DFCS BITE TEST LINE MAINT 1/2 page shows on the CDU.
S 745-031
(3) Do the ACT POS SENS test:
(a)
Push the LSK adjacent to <LRU INTERFACE.
(b)
Push the LSK adjacent to <CHANNEL A AND B.
(c)
Push the NEXT PAGE key on the CDU.
(d)
Make sure that the DFCS BITE TEST INTERFACE -A/-B 2/2 page shows on the CDU.
(e)
Push the LSK adjacent to ACT POS SENS>.
(f)
Do the preparation steps for the quick tests as shown on the CDU display.
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 自動(dòng)飛行 AUTOFLIGHT 1(168)
