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_______________UNABLE NEXT ALT NEXT CLIMB RESTRICTION IN CLIMB PROFILE CANNOT BE MET DUE TO UNDERSHOOT OR NEXT DESCENT RESTRICTION CANNOT BE MET DUE TO OVERSHOOT 
_____________RESET MCP ALT PASSING TOP OF DESCENT POINT WITHOUT LOWERING MCP ALT WINDOW 
CAUSES THE COMPUTED FUEL BURN TO SHOW LESS THAN 2000 LBS AT DESTINATION _________________INSUFFICIENT FUEL A CHANGE IN FLIGHT CONDITIONS OCCURS OR A CHANGE IN THE ROUTE IS MADE WHICH 
PROPER LOCALIZER CAPTURE MANEUVER WAS PERFORMED BUT DFCS DID NOT CAPTURE ______________MISSED CAPTURE 
AN ERROR IN THE NAVIGATION DATA BASE HAS BEEN FOUND AND CORRECTED _______________________FIXING NDB-CHK FLT PLAN 
PERF DEFAULTS INVALID_____________________ THE LOADED DEFAULTS TABLE FAILS ITS CRC CHECK 
SELECT MODE AFTER RTA_____________________ RTA FUNCTION EXITED BY WAYPOINT DELETION OR RTA WAYPOINT SEQUENCED 
SYSTEM GROSS WEIGHT OR ZERO FUEL WEIGHT HAS CHANGED SINCE THE T/O SPEEDS WERE VERIFY TAKEOFF SPEEDS_____________________ SELECTED 

FMCS Alerting Messages Figure 16 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-62-01

 AND A SINGLE FMC  ú CONFIG 1 ú 06 Page 58 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C98018
A 737-300/400/500MAINTENANCE MANUAL
MESSAGE / CONDITION ___________________ALERTING MESSAGES 
VERIFY POSITION_______________ COMPARISON THRESHOLD THE DIFFERENCE BETWEEN COMPUTED RADIO POSITION AND FMC POSITION USING IRUs EXCEEDS 
VNAV DISCONNECT_______________ VNAV INVALID CAUSES VNAV DISCONNECT 
AIRPLANE EXCEEDS DESCENT SPEED RESTRICTIONS BY 15 KTS OR MORE OVERSPEED DISCONNECT____________________ 
WITHOUT BYPASSING MORE THAN ONE WAYPOINT GEOMETRY OF THE NEXT WAYPOINTS WILL NOT ALLOW THE FMC TO FLY THE ACTIVE PLAN DISCO INSRTD AFTER XXXXX________________________ 
DATA BASE INVALID_________________ THE VALIDITY CHECK OF THE PERMANENT NAVIGATION DATA BASE HAS FAILED, OR AN ATTEMPT IS MADE TO ACCESS A FAILED NAVIGATION DATA BASE 
FROM THE PILOTS GMT CLOCK NAV DATA OUT OF DATE____________________ THE EFFECTIVITY DATES OF THE NAVIGATION DATA BASE DO NOT CORRESPOND TO THE DATE 
___________________CYCLE IRS NAV - OFF IRS LOGIC REQUIRES A MANUAL RESTART OF THE ALIGNMENT 
REQUIRES A POSITION ENTRY ENTER IRS POSITION__________________ THE IRS DID NOT ALIGN TO THE ENTERED POSITION OR THE IRS HAS ENTERED A MODE WHICH 
THE IRS DETECTED MOTION DURING ALIGNMENT __________IRS MOTION 
TIVE ACTION MAY BE TAKEN RTA IS CURRENTLY OUTSIDE OF THE COMPUTED WINDOW PLUS A TIME MARGIN AND NO CORREC-________________RTA UNACHIEVABLE 

FMCS Alerting Messages Figure 16 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-62-01

 AND A SINGLE FMC  ú CONFIG 1 ú 07 Page 59 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C98047
A 737-300/400/500MAINTENANCE MANUAL
MESSAGE / CONDITION _____________________CDU ADVISORY MESSAGES 
XXXX (EXAMPLE KJFK) (REF AIRPORT NAME FROM POS INIT PAGE)_________________________________________________________ ORIGIN FIELD ON PAGE 1 OF RTE PAGE CONTAINS NO DATA AND REFERENCE AIRPORT ENTERED ON POS INIT PAGE. DISPLAYED ON CDU WITH RTE PAGE 1 DISPLAYED 
ABOVE MAX CERT ALT__________________ THE AIRCRAFT HAS EXCEEDED ITS MAXIMUM CERTIFIED ALTITUDE 
ROUTE FULL__________ THE MAXIMUM ALLOWABLE NUMBER OF HOLDING PATTERNS AND/OR FIXED, FLOATING, AND PHANTOM WAYPOINTS HAS BEEN EXECUTED 
NOT ON INTERCEPT HEADING________________________ AIRPLANE IS NOT WITHIN THE CAPTURE CRITERIA OF ACTIVE LEG 
VALUE APPEARS IN THE SCRATCH PAD WHEN THE MCP ALTITUDE IS RESET TO A VALUE NOT EQUAL TO THE CRZ ALT, THE CRZ ALT XXXXX (ALTITUDE VALUE OR WAYPOINT IDENTIFIER)_____________________________________________ 
SELECT ACTIVE WPT/LEG_____________________ POWER UP WHILE AIRBORNE OR INSERTION OF A DIFFERENT FLIGHT PLAN WHILE AIRBORNE 
RESET MCP ALT_____________ NORMAL FMCS OPERATION WOULD REQUIRE FLYING AWAY FROM MCP ALTITUDE 
MIN CAS XXX___________ THE TARGET SPEED IS LIMITED BECAUSE IT EXCEEDS THE MINIMUM BUFFET SPEED 
MIN MACH XXX____________ THE TARGET SPEED IS LIMITED BECAUSE IT EXCEEDS THE MINIMUM BUFFET SPEED 
　
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