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时间:2011-04-02 23:42来源:蓝天飞行翻译 作者:航空
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 13. FMCS Messages_____________
 A. General
 (1)  The FMCS (Flight Management Computer System) displays a set of messages for information. These messages are displayed in the scratch pad line of the CDU when conditions warrant their appearance. There are three categories of messages. the messages have a defined priority for display should their set conditions occur at the same time. The three types, listed in order of highest priority, are: Alerting Messages, Entry Error Advisory Messages, and Readiness Advisory Messages
 B. Entry Error Advisory Messages (Fig. 15)
 (1)  
Entry error advisory messages indicate that an entry of data from the scratch pad into a data field is not correct. The operator must clear the message and repeat the entry in the proper manner. These messages appear only on the CDU on which the data entry attempt was made.

 (2)  
If two or more messages of the same priority are set for display, the one occuring first is displayed until it is cleared, bringing up the next to occur. Messages of differing priorities are stacked for display in the same manner. Clearance of the various messages is normally accomplished by some sort of external clear: pressing the CLR key, or reversion to valid conditions that set the message. Some messages are cleared by the page being changed, which also deletes any of the entries and actions that precipitated the message.

 (3)  
When a message appears in the scratch pad, of any page, the CDU MSG annunciator light will illuminate. The light will illuminate even if the page on which the message appears is not currently displayed on the CDU.


 C. Alerting Messages (Fig. 16)
 (1)  
Alerting Messages indicate some condition which must be acknowledged and remedied before further FMCS-guided flight is advisable or possible. These messages appear on the CDU. Occurence of alerting messages will also cause the FMC annunciator on the autoflight status annunciator panel to illuminate by setting the FMC message discrete. The FMC annunciator is also illuminated for system hardware failures (Fig. 1).

 (2)  
Display priority and the CDU MSG light for the alerting messages operate the same as the entry error advisory messages.


 D. Readiness Advisory Messages (Fig. 17)
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 34-62-01

 AND A SINGLE FMC  ú CONFIG 1 ú 06 Page 56 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
_____________________________ENTRY ERROR ADVISORY MESSAGES MESSAGE / CONDITION 
REQUIRED DATA A SEARCH OF THE NAV DATA BASE, INCLUDING TEMPORARY, DID NOT RESULT IN FINDING THE ________________NOT IN DATA BASE 
__________ GUIDANCE BUFFER IS FILLED TO ALLOWABLE CAPACITY ROUTE FULL 
THE ENTRY HAS AN INCORRECT FORMAT AND/OR RANGE FOR THE SELECTED CDU FIELD _____________INVALID ENTRY 
______________INVALID DELETE THE DELETE KEY HAS NO APPLICATION FOR THE SELECTED FIELD 
ENTRY ATTEMPTED HAS EXCEEDED THE CAPACITY FOR THE TEMPORARY OR SUPPLEMENTAL DATA BASES ______________DATA BASE FULL 
CONSTRAINT ALTITUDE AT OTHER WAYPOINTS IN THE ROUTE. XXXXX IS THE FIRST DOWN-AN ADDED OR CHANGED ALTITUDE CONSTRAINT OR CRUISE ALTITUDE CONFLICTS WITH THE ____________________ALT CONSTRAINT XXXXX STREAM WAYPOINT WHICH CONFLICTS WITH THE ENTERED CONSTRAINTS 
NOT IN FLIGHT PLAN__________________ ENTERED RTA WAYPOINT IS NOT IN CURRENT FLIGHT PLAN 

FMCS Entry Error Advisory Messages Figure 15
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 AND A SINGLE FMC  ú CONFIG 1 ú 07 Page 57 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C98008
A 737-300/400/500MAINTENANCE MANUAL
ALERTING MESSAGES___________________ MESSAGE / CONDITION 
____________END OF ROUTEPASSING LAST ROUTE LEG TERMINATION 
_____________DISCONTINUITY PASSING LAST WAYPOINT PRIOR TO A DISCONTINUITY 
FMC IN IRS ONLY MODE FOR NAVIGATION ____________IRS NAV ONLY 
EITHER NOT TUNED OR A VALID SIGNAL IS NOT BEING RECEIVED ________________________NAV INVALID - TUNE XXXXX R NAV OR VOR APPROACH PROCEDURE REQUIRES A SPECIFIC NAVAID BE TUNED AND IT IS 
 
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