FMCS Readiness Advisory Messages
Figure 17 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH DUAL FMC ú
34-62-01
ú CONFIG ú 04 Page 63 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C89016
A 737-300/400/500MAINTENANCE MANUAL
___________________ MESSAGE / CONDITION ADVISORY MESSAGES
BE UNABLE TO REACH CRUISE ALTITUDE DUE TO PERFORMANCE LIMITATIONS PERFORMANCE PREDICTS A ZERO CRUISE TIME AT THE ENTERED CRUISE ALTITUDE OR IT WILL ______________UNABLE CRZ ALT
ON PERF FACTORS PAGE AT CURRENT CONDITIONS, THE AIRPLANE HAS A BUFFET MARGIN LESS THAN THAT SELECTED ____________BUFFET ALERT
RESERVES CAUSES THE COMPUTED FUEL BURN TO EXCEED THE TOTAL FUEL ON BOARD LESS ENTERED A CHANGE IN FLIGHT CONDITIONS OCCURS OR A CHANGE IN THE ROUTE IS MADE WHICH ______________USING RSV FUEL
AT WHICH A CONFLICT OCCURS ALTITUDE AT OTHER WAYPOINTS IN THE ROUTE. XXXXX IS THE FIRST DOWNSTREAM WAYPOINT A FLIGHT PLAN EDIT HAS CAUSED AN ALTITUDE CONSTRAINT TO CONFLICT WITH A CONSTRAINT ____________________ALT CONSTRAINT XXXXX
AIRPLANE IS TOO FAR ABOVE THE COMPUTED DESCENT PATH TO RECAPTURE IT WITHOUT _____________________DES PATH UNACHIEVABLE VIOLATING EXISTING ALTITUDE CONSTRAINTS
WITHIN 5 KTS OF VMO. DUE TO UNFORECAST CONDITIONS, THE AIRPLANE IS 10KT OR MORE ABOVE TARGET SPEED OR _____________DRAG REQUIRED
SPEED ENTERED INTO TARGET SPEED FIELD IS IMPOSSIBLE TO ACHIEVE AT ANY ALTITUDE AT _______________UNABLE MACH XXX THE CURRENT AIRPLANE WEIGHT
THE TARGET SPEED IS LIMITED BECAUSE IT EXCEEDS THE MAXIMUM BUFFET SPEED ___________MAX CAS XXX
____________MAX MACH XXX THE TARGET SPEED IS LIMITED BECAUSE IT EXCEEDS THE MAXIMUM BUFFET SPEED
FMCS Readiness Advisory Messages
Figure 17 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH DUAL FMC ú
34-62-01
ú CONFIG ú 04 Page 64 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C89021
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 XXXALTITUDE ENTRY ON ANY PAGE IS ABOVE THE MAXIMUM ALTITUDE FOR ECON MODE
RUNWAY N/A FOR SIDRUNWAY SELECTED NOT COMPATIBLE WITH DEPARTURE
ARR N/A FOR RUNWAYRUNWAY/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
NO DES PATH AFTER XXXXX
PROFILE PREDICTION PROCESS IS UNABLE TO CONSTRUCT A DESCENT PATH THAT SATISFIES ALL ALTITUDE CONSTRAINTS
CHECK FMC FUEL QUANTITY THE FMC HAS DETECTED AN UNEXPECTED DROP IN FUEL QUANTITY
FMCS Readiness Advisory Messages
Figure 17 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH DUAL FMC ú
34-62-01
ú CONFIG ú 04 Page 65 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C88971
A 737-300/400/500MAINTENANCE MANUAL
ACARS MESSAGE WAITING ____________ACARS UPLINK 1
ACARS VOICE___________ VHF TRANSCEIVER SET TO VOICE
ACARS VOICE BUSY________________ ALL VHF VOICE CIRCUITS ARE BUSY
NO ACARS LINK IS AVAILABLE _____________ACARS NO COMM 1
ACARS MU HAS FAILED _____________ACARS MU FAIL 1
FLIGHT CREW ACTION REQUIRED FOR ACARS ACARS ALERT 1___________
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