FMCS -AIRLINE MODIFIABLE INFORMATION

*
Bit 11 -Time stamp IEI enable

*
Bit 12 -Ground address IEI enable

*
Bit 13 -Company distribution IEI enable

*
Bit 14 -Scratchpad IEI enable

*
Bit 15 -Flight number IEI enable

*
Bit 16 -Flight plan response enable

*
Bit 17 -Performance initialize response message enable

*
Bit 18 -Takeoff response message enable

*
Bit 19 -Wind response message enable

*
Bit 20 -Pos report trigger response message enable

*
Bit 21 -ALTN response message enable

*
Bit 22 -Change in destination airport trigger enable

*
Bit 23 -Change in arrival runway trigger enable.

Downlink Trigger Parameters
The table shows the default values and the valid range for the downlink trigger parameters.
Parameter  Default Value  Valid Range 
Head wind discrepancy  Disable  0-99 kts 
Change in destination ETA  Disable  0-999 min 
Time to top of descent 1  Disable  0-999 min 
Time to top of descent 2  Disable  0-999 min 
Time to top of descent 3  Disable  0-999 min 
Time to top of descent 4  Disable  0-999 min 
Time to top of descent 5  Disable  0-999 min 
Time to destination 1  Disable  0-999 min 
Time to destination 2  Disable  0-999 min 

Parameter  Default Value  Valid Range 
Time to destination 3  Disable  0-999 min 
Time to destination 4  Disable  0-999 min 
Time to destination 5  Disable  0-999 min 

Downlink Address Table
The downlink address table has the ground addresses and the company distribution for IMIs. There are no default entries for this table. You may enter a maximum of 20 IMIs in the table.
Airline Ground Address Table
The airline ground address table has the ground addresses with the identification of ADS uplinks that originate with the airline. There are no default entries for this table. You may enter a maximum of 5 ground addresses or 5 groups of addresses in the table.
Default Values Summary
Default values are non-modifiable values found in the operational software of the CPM/Basic and the CPM/ACMF. To cause the function to operate with new values, you must develop a customized AMI and load that software into the CPMs. These new values do not override the default values but are used instead of the default values. If the AMI fails, FMCFs use the default values.
EFFECTIVITY BEJ ALL  34-61-00 
Page 98.97 
D633W101-BEJ  May 05/2003 

FMCS -AIRLINE MODIFIABLE INFORMATION
With the FMCF, you can also use the airline policy page to modify the AMI values on a short term basis. You can do this between flights.
EFFECTIVITY BEJ ALL  34-61-00 
Page 98.98 
D633W101-BEJ  May 05/2003 

777 AIRCRAFT MAINTENANCE MANUAL

FMCS -AIRLINE MODIFIABLE INFORMATION

EFFECTIVITY BEJ ALL  34-61-00 
Page 98.99 
D633W101-BEJ  May 05/2003 

FMCS -CDU FUNCTIONAL DESCRIPTION

General
The left and right CDUs operate independently to supply different pages of data with CDU keyboard entries. The CDU main interface is with the active FMCF for flight control. The CDUs interface with other systems. The CDUs also do back-up functions and alternate functions for some systems.
The CDUs receive inputs from these:
*
External systems

*
Flight deck panels

*
AIMS cabinets

*
Other CDUs.

The CDUs use the inputs to do these functions:
*
Menu control and access of systems

*
Alternate control panel functions

*
Alternate LNAV function

*
Alternate LNAV guidance

*
Alternate LNAV engage and disengage logic

*
Alternate navigation radio tuning

*
Bite and fault monitoring

*
Display and control

*
Liquid crystal display (LCD).

The CDUs supply data to these functions and components:
*
AIMS (CMCF, FMCF, and PDF)

*
LCD function

*
Navigation radios

*
Autopilot flight director system (AFDS)

*
Satellite data unit (SDU)

*
Passenger address/cabin interphone (PA/CI) controller.

Systems Access
Push the MENU key to access the MENU page. This MENU page shows the FMC and other systems the operator may access. The left and right CDUs are the main crew interface for preflight and inflight control. The crews use the CDUs and the mode control panel (MCP) to initialize the FMCFs during preflight. The flight crews use the CDUs to change the lateral and vertical flight profile inflight.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：777 AMM 飛機維護手冊 導航 Navigation 2(70)