FMCS Alerting Messages
Figure 15 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
34-62-00
ú ú 08 Page 60 ú Mar 15/89
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 OR TOO MANY HOLDS ARE ENTERED __________ROUTE FULL
THE ENTRY HAS AN INCORRECT FORMAT AND/OR RANGE FOR THE SELECTED CDU FIELD _____________INVALID ENTRY
______________ THE DELETE KEY HAS NO APPLICATION FOR THE SELECTED FIELD INVALID DELETE
DIR/INTC BUTTON PRESSED WITHOUT AN ACTIVE ROUTE. CDU REMAINS ON PAGE BEING DIS-PLAYED WHEN BUTTON IS PRESSED _______________NO ACTIVE ROUTE
AIRPORT) AND THE CREW ATTEMPTS TO DEFINE ANOTHER OF THAT CATEGORY THE TEMPORARY DATA BASE IS FULL IN A PARTICULAR CATEGORY (NAVAID, WAYPOINT, OR ______________DATA BASE FULL
STREAM WAYPOINT WHICH CONFLICTS WITH THE ENTERED CONSTRAINTS 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
FMCS Entry Error Advisory Messages
Figure 16
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
34-62-00
ú ú 03 Page 61 ú Feb 25/87
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
MESSAGE / CONDITION _____________________CDU ADVISORY MESSAGES
RE-ENTER IRS POSITION_____________________ FIVE SECONDS AFTER LINE SELECTION OF POSITION LAT/LONG INTO CDU FOR IRS INPUT, POSITION DATA OTHER THAN THAT CORRESPONDING TO THE SET IRS POSITION IS RECEIVED BACK FROM ANY IRS
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
V-PATH NOT READY________________ PATH DESCENT IS THE SELECTED GUIDANCE MODE, AND A CREW ACTION ON THE CDU HAS STIMULATED A RECOMPUTATION OF THE DESCENT PATH, AND THE NEW PATH IS NOT YET READY FOR VERTICAL STEERING
NOT ON INTERCEPT HEADING________________________ AIRPLANE IS NOT WITHIN THE CAPTURE CRITERIA OF ACTIVE LEG AND L NAV BUTTON IS PUSHED
XXXXX_____ XXXXX IS THE ALTITUDE INDICATED ON THE MODE CONTROL PANEL (MCP). THIS APPEARS ON AND THE RESET VALUE DOES NOT EQUAL THE CRUISE ALTITUDE. A SUITABLE TIME DELAY IS USED TO ALLOW THE MCP RESET OPERATION TO BE COMPLETED. DATA INCORPORATED IN CRUISE PAGE WHENEVER THE INDICATED ALTITUDE IN THE MCP ALTITUDE WINDOW IS CHANGED SCRATCH PAD MESSAGE MAY BE LINE SELECTED TO THE APPROPRIATE FIELD
SELECT ACTIVE WPT/LEG_____________________ POWER UP WHILE AIRBORNE OR INSERTION OF A DIFFERENT FLIGHT PLAN REQUIRES CREW DEFINITION OF THE ACTIVE LEG
RESET MCP ALT_____________ NORMAL FMCS OPERATION WOULD REQUIRE FLYING AWAY FROM MCP ALTITUDE
FMCS Readiness Advisory Messages
Figure 17 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 導航 NAVIGATION 5(8)
