NOTE: (E/53/350/10, BIT 13) = SRM-L OPTION PIN FAIL (SRM-L)
____ (E/53/350/10, BIT 12) = SRM-L PROGRAM PIN INPUT FAIL (SRM-L)
 S 745-141
 (14)
 Use the NEXT PAGE key on the CDU to show page 5 of the INPUT MONITORING.

 S 745-142

 (15)
 Use the alphanumeric keys on the CDU to put "E/26/350/00" into the scratchpad.

 S 745-143

 (16)
 Push the LSK 1L to move the data into the correct position.

 S 745-144

 (17)
 Make sure that bits 17 and 16 for the ARINC word "E/26/350/00" are "0".

 NOTE: (E/26/350/00, BIT 17) = SRM-L AUTOTRIM ENGAGE-CONT SIGNAL ->
____
 SRM-R INTERFACE FAIL

 (E/26/350/00, BIT 16) = SRM-L AUTOTRIM ENGAGE-ARM SIGNAL -> SRM-R INTERFACE FAIL
 S 745-145
 (18)
 Use the NEXT PAGE key on the CDU to show page 6 of the INPUT MONITORING.

 S 745-146

 (19)
 Use the alphanumeric keys on the CDU to put "E/26/350/01" into the scratchpad.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-22-00
 ALL  ú ú 01 Page 517 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 745-147
 (20)
 Push the LSK 1L to move the data into the correct position.

 S 745-148

 (21)
 Make sure that bits 21, 19, 18 and 16 for the ARINC word "E/26/350/01" are "0".

 NOTE: (E/26/350/01, BIT 21) = FCC-R -> SRM-R DATA FAIL
____
 (E/26/350/01, BIT 19) = FCC-C -> SRM-R DATA FAIL
 (E/26/350/01, BIT 18) = FCC-R -> SRM-R BUS FAIL
 (E/26/350/01, BIT 16) = FCC-C -> SRM-R BUS FAIL
 S 745-149
 (22)
 Use the NEXT PAGE key on the CDU to show page 7 of the INPUT MONITORING.

 S 745-150

 (23)
 Use the alphanumeric keys on the CDU to put "E/53/350/10" into the scratchpad.

 S 745-151

 (24)
 Push the LSK 1L to move the data into the correct position.

 S 745-152

 (25)
 Make sure that bits 13 and 12 for the ARINC word "E/53/350/10" are "0".

 NOTE: (E/53/350/10, BIT 13) = SRM-L OPTION PIN FAIL (SRM-L)
____ (E/53/350/10, BIT 12) = SRM-L PROGRAM PIN INPUT FAIL (SRM-L)
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-22-00
 ALL  ú ú 01 Page 518 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 865-155

 WARNING:_______ MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
 SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER.  AILERONS, RUDDERS,
 ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST
 REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER.
 THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.

 (26)
 Supply hydraulic pressure to the hydraulic systems N0. 1, 2, 3 and 4 (AMM 29-11-00/201).

 S 865-232

 (27)
 Set the FLT CONTROL HYD POWER TAIL 1, 2, 3, and 4 switches to the NORM position. These switches are on the Pilots' Overhead Maintenance Panel (P461).

 S 865-157

 (28)
 Set the FLT CONTROL HYD POWER WING 1, 2, 3, and 4 switches to the NORM position. These switches are on the Pilots' Overhead Maintenance Panel (P461).

 S 865-162

 (29)
 Make sure that the radio altitude shown on the EADI is less than 2 feet.

 S 865-163

 (30)
 Use the manual trim switches (captain's or first officer's) on the Pilots' Control Wheel to set the stabilizer between -3 degrees (down arrow) and -5 degrees (down arrow).

 S 865-223

 (31)
 Set the flight director switch (captain's or first officer's) on the mode control panel to the ON position.

 S 865-224

 (32)
 Push the VS button on the mode control panel.

 S 865-225

 (33)
 Use the thumb-wheel switch on the mode control panel to set the vertical speed to -2000/minute.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 空調 AUTO FLIGHT(194)