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A 737-300/400/500MAINTENANCE MANUAL
ADVISORY MESSAGES MESSAGE / CONDITION ___________________
ROUTE FULL__________ THE MAXIMUM ALLOWABLE NUMBER OF FIXED, FLOATING, AND PHANTOM WAYPOINTS HAS BEEN EXCEEDED 2
UNABLE CRZ ALT______________ PERFORMANCE PREDICTS A ZERO CRUISE TIME AT THE ENTERED CRUISE ALTITUDE OR IT WILL BE UNABLE TO REACH CRUISE ALTITUDE DUE TO PERFORMANCE LIMITATIONS
BUFFET ALERT____________ AT CURRENT CONDITIONS, THE AIRPLANE HAS A BUFFET MARGIN LESS THAN THAT SELECTED ON PERF FACTORS PAGE
USING RSV FUEL______________ A CHANGE IN FLIGHT CONDITIONS OCCURS OR A CHANGE IN THE ROUTE IS MADE WHICH CAUSES THE COMPUTED FUEL BURN TO EXCEED THE TOTAL FUEL ON BOARD LESS ENTERED RESERVES
ALT CONSTRAINT XXXXX____________________ A FLIGHT PLAN EDIT HAS CAUSED AN ALTITUDE CONSTRAINT TO CONFLICT WITH A CONSTRAINT ALTITUDE AT OTHER WAYPOINTS IN THE ROUTE. XXXXX IS THE FIRST DOWNSTREAM WAYPOINT AT WHICH A CONFLICT OCCURS
DES PATH UNACHIEVABLE_____________________ AIRPLANE IS TOO FAR ABOVE THE COMPUTED DESCENT PATH TO RECAPTURE IT WITHOUT VIOLATING EXISTING ALTITUDE CONSTRAINTS
DRAG REQUIRED DUE TO UNFORECAST CONDITIONS, AIRPLANE OVERSPEEDING _____________
FMCS Readiness Advisory Messages
Figure 17 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
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A 737-300/400/500MAINTENANCE MANUAL
MESSAGE / CONDITION ___________________ADVISORY MESSAGES
LOC CAP ACTIVE______________ AIRPLANE IS APPROACHING THE TURN ON TO THE LOCALIZER COURSE AND WILL HOLD AN INTERCEPT HEADING TO FACILITATE DFCS LOCALIZER CAPTURE
LOC CAP CANCELLED_________________ LOC CAP ACTIVE WAS DISPLAYED PREVIOUSLY, IT'S SET LOGIC IS NO LONGER SATISFIED AND LOCALIZER CAPTURE HAS NOT OCCURRED
TAT ON ABOVE 10`C_________________ AIRPLANE IS OPERATING IN A THRUST LIMIT MODE ABOVE A TOTAL AIR TEMPERATURE OF +10`C WITH THE ANTI-ICING SYSTEMS ON
MAX ALT FL XXX______________ ALTITUDE ENTRY ON ANY PAGE IS ABOVE THE MAXIMUM ALTITUDE OR THE CRUISE ALTITUDE BECOMES GREATER THAN CURRENT CALCULATED MAXIMUM ALTITUDE
RUNWAY SELECTED NOT COMPATIBLE WITH DEPARTURE RUNWAY N/A FOR SID__________________
ARR N/A FOR RUNWAY__________________ RUNWAY/APPROACH SELECTED IS NOT COMPATIBLE WITH ARRIVAL SELECTED
PROGRAM PIN ERROR_________________ PROGRAM PINS ARE FOUND TO BE IN AN INVALID CONFIGURATION DURING POWER-UP CHECK OF PINS. NO FMC INTERNAL FAILURES HAVE BEEN DETECTED
DES PATH UNACH AT XXXXX_______________________ PROFILE PREDICTION PROCESS IS UNABLE TO CONSTRUCT A DESCENT PATH THAT SATISFIES ALL ALTITUDE CONSTRAINTS NO DES PATH AFTER XXXX______________________1 2
FMC WITH "OP PROGRAM" 539632-35-01 ALL EXCEPT FMC WITH "OP PROGRAM" 539632-35-01
FMCS Readiness Advisory Messages
Figure 17 (Sheet 3)
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A
737-300/400/500MAINTENANCE MANUAL
(2) Display priority and the CDU MSG light operate for the advisory messages the same as for alerting messages.
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737-300/400/500MAINTENANCE MANUAL
FLIGHT MANAGEMENT COMPUTER SYSTEM - TROUBLE SHOOTING
____________________________________________________
1. General_______
A. You use the Flight Management System (FMS) Built-In-Test-Equipment (BITE) to identify Flight Management Computer System (FMCS) failures and malfunctions.
B. You can find the FMS BITE procedure in Chapter 22. FMS BITE includes BITE for these systems:
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