22-11-00
ú ú 11 Page 573 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 745-118
(17)
Do the preparation steps as shown on the CDU display but keep the TR2, TR3, and AFCS B FCC DC circuit breakers open.
S 745-119
(18)
Push the LSK adjacent to <CONTINUE until the question "Is the G/S ENGAGE displayed on the CAPT FMA?" is shown on the CDU.
S 745-120
(19)
Make sure that the TRU meter on the Pilots' Overhead Panel, P5-13 is at 0v dc when the question "Is the G/S ENGAGE displayed on the CAPT FMA?" is shown on the CDU.
S 865-121
(20)
Close the AFCS B FCC DC circuit breaker on the P6-2 Circuit Breaker Panel.
S 865-122
(21)
Close the TR2 circuit breaker on the P6-4 Circuit Breaker Panel.
S 865-123
(22)
Set the meter selector switch for the TRU to the TR1 position.
S 865-124
(23)
Open the TR1 circuit breaker on the P6-4 Circuit Breaker Panel.
S 865-125
(24)
Open the AFCS A FCC DC circuit breaker on the P18-1 Circuit Breaker Panel.
S 745-142
(25)
Make sure that the DC voltmeter on the Pilots' Overhead Panel, P5-13 reads 22 to 30v dc.
S 745-126
(26)
Do the steps (5) thru (11) until the CDU display shows the CHANNEL SELECTION page.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 11 Page 574 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 745-127
(27)
Push the LSK adjacent to <CHANNEL B to show the FCC memory contents of channel B.
S 745-168
(28)
Push the LSK adjacent to <TEST SELECTION.
S 745-167
(29)
Use the CDU keyboard to put the library test No. 13 into the CDU scratchpad.
S 745-166
(30)
Push the LSK 6R to put the library test No. 13 on the screen and in the memory.
S 745-165
(31)
Push the LSK adjacent to <EXECUTE to do the test 60.13 (MCP Interface Quick Test).
S 745-180
(32)
Do the preparation steps as shown on the CDU display but keep the TR1, TR3, and AFCS A FCC DC circuit breakers open.
S 745-163
(33)
Push the LSK adjacent to <CONTINUE until the question "Is the G/S ENGAGE displayed on the F/O FMA?" is shown on the CDU.
S 745-179
(34)
Make sure that the DC voltmeter on the Pilots' Overhead Panel, P5-13 is at 0v dc when the question "Is the G/S ENGAGE displayed on the F/O FMA?" is shown on the CDU.
S 865-135
(35)
Close the TR1 and TR3 circuit breakers on the P6-4 Circuit Breaker Panel.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 10 Page 575 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-161
(36)
Close the AFCS A FCC DC circuit breaker on the P18-1 Circuit Breaker Panel.
S 745-160
(37)
Push the INIT/REF key on the CDU keyboard to get out of the BITE.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 10 Page 576 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
DIGITAL FLIGHT CONTROL SYSTEM - DESCRIPTION AND OPERATION
_________________________________________________________
1. General_______
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(76)
