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HOLD PATTERN BUILT
BY FMCS GUIDANCE
FUNCTION EXCEEDS
HOLD AIRSPACE
CLEAR MESSAGE AND
NOTIFY ATC IF
NECESSARY.
ALERTING MESSAGE CAUSE CORRECTIVE ACTION
UNABLE NEXT ALT NEXT CLB/DESC
CONSTRAINT XANNOT
BE ACHIEVED
CLEAR MESSAGE AND
REVIEW FMCS ERROR AT
PREDICTION.
UNABLE REQD NAV
PERF-RNP
ACTUAL NAV
PERFORMANCE IS NOT
SUFFICIENT FOR
MANUALLY ENTERED
RNP VALUES
CLEAR MESSAGE AND
VERIFY FMCS POSITION
DATA ON POS SHIFT
PAGE.
SHZ ALL POST SB 737-34-1918
UNABLE XXX KTS AT
YYYYY
NEXT WAYPOINT(YYYYY)
SPEED(XXX)
RESTRICTION CANNOT
BE MET
CLEAR MESSAGE AND
NOTIFY ATC IF
NECESSARY.
SHZ ALL
VERIFY GW AND FUEL FAILURE OF TOTAL FUEL
QTY OR IT HAS BEEN 30
MINUTES SINCE MANUAL
FUEL QTY ENTRY.
MESSAGE INHIBITED IN
DESCENT
CLEAR MESSAGE AND
CHECK GW AND FUEL.
MAKE MANUAL ENTRY
OF GW AS REQUIRED.
SHZ ALL PRE SB 737-34-1918
VERIFY POSITION FMCS AND POSITION
SENSORS EXCEED
ALLOWABLE
TOLERANCES
CLEAR MESSAGE CHECK
POSITIONS ON THE POS
SHIFT PAGE.
SHZ ALL POST SB 737-34-1918
VERIFY POS: IRS-IRS
VERIFY POS: IRS-FMC
VERIFY POS: IRS-RADIO
VERIFY POS: FMC-RADIO
VERIFY POS: FMC-GPS
VERIFY POS: FMC-FMC
(Msgs enabled during
flight)
FMCS AND POSITION
SENSORS EXCEED
ALLOWABLE
TOLERANCES
CLEAR MESSAGE CHECK
POSITIONS ON THE POS
SHIFT PAGE.
SHZ ALL
FMCS - DISPLAYS - CDU - MESSAGES
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.88
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-044
ALERTING MESSAGE CAUSE CORRECTIVE ACTION
VERIFY RNP DEFAULT VALUE OF RNP
IS LESS THAN THE
MANUALLY ENTERED
VALUE
CLEAR MESSAGE AND
CHECK MANUALLY
ENTERED RNP VALUE.
ALERTING MESSAGE CAUSE CORRECTIVE ACTION
VERIFY TAKEOFF
SPEEDS
SYSTEM GROSS WEIGHT
OR ZERO FUEL WEIGHT
CHANGED SINCE THE T/
O REF SPEEDS WERE
SELECTED
RESELECT TAKEOFF
SPEEDS.
VNAV DISCONNECT CRITERIA FOR VNAV
ENGAGEMENT NO
LONGER EXISTS
MANUALLY CONTROL
THE VERTICAL PATH.
MESSAGE CLEARS IF
VNAV RE-ENGAGED.
Advisory Messages
ADVISORY MESSAGE CAUSE CORRECTIVE ACTION
ABOVE MAX CERT ALT AIRPLANE EXCEEDS ITS
MAXIMUM CERTIFIED
ALTITUDE
DESCEND TO AN
ALTITUDE BELOW THE
MAXIMUM CERTIFIED
ALTITUDE.
ALT CONSTRAINT XXXXX FLIGHT PLAN EDIT HAS
CAUSED AN ALTITUDE
CONSTRAINT TO
CONFLICT WITH A
CONSTRAINT ALTITUDE
AT OTHER WPTS IN THE
ROUTE. XXXXX IS THE
FIRST WPT
EDIT FLIGHT PLAN TO
RESOVE THE ALT
CONSTRAINT CONFLICT
AND CLEAR MESSAGE.
APPRCH VREF NOT
SELECTED
FMC IN APPROACH
ENVIRONMENT AND
VREF NOT SELECTED
SELECT VREF ON
APPROACH REF PAGE.
ADVISORY MESSAGE CAUSE CORRECTIVE ACTION
ARR N/A FOR RUNWAY RUNWAY OR APPROACH
SELECTED IS NOT
COMPATIBLE WITH
ARRIVAL SELECTED
GO TO ARRIVALS PAGE
AND MODIFY SELECTION.
ADVISORY MESSAGE CAUSE CORRECTIVE ACTION
BUFFET ALERT CURRENT CONDITIONS
RESULT IN MANEUVER
MARGIN LESS THAN
THAT SELECTED FOR
AIRPLANE
BRING AIRPLANE BACK
TO WITHIN OPERATING
ENVELOPE.
CHECK FMC FUEL
QUANTITY
THE FMCS DETECTED A
DROP IN FUEL QUANTITY
(> 1500 LBS FOR 120
SECONDS)
CHECK THE FUEL
QUANITY SYSTEM
DESCENT PATH
UNACHIEVABLE
WHILE IN DESCENT, THE
FMC PREDICTIONS
SHOW THE PROFILE
CONSTRAINTS AT THE
NEXT WPT CANNOT BE
MADE
MODIFY THE ACTIVE
ROUTE LEGS OR DES
PAGE PLANS AND REENGAGE
LNAV AND
VNAV.
DRAG REQUIRED DUE TO UNFORECAST
CONDITIONS, THE
AIRPLANE IS 10 KTS OR
MORE ABOVE FMCS
TARGET SPEED OR
WITHIN 5 KTS OF VMO
USE SPEEDBRAKES OR
TRIM AS NECESSARY TO
BRING AIRPLANE BELOW
FMCS TARGET SPEED.
FMCS - DISPLAYS - CDU - MESSAGES
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.89
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-044
ADVISORY MESSAGE CAUSE CORRECTIVE ACTION
DUAL FMC OP
RESTORED (DUAL FMC
ONLY)
MOVEMENT OF FMC
SOURCE SELECT
SWITCH CAUSED A
RESYNCH AND DUAL
FMC OPERATION IS
　
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