BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
34-61-00
ALL ú ú 07 Page 31 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
THRUST RESOLVER ANGLE (TRA)EEC STATUS
EIU-L-I-1
EPR - ACTUAL COMMAND & MAX (HI SPEED)
EXHAUST GAS TEMPMAIN OIL TEMP
BLEED DISC STATUSBLEED DISCRETESENG 1-4 FUEL FLOWL & R MANIFOLD PRESS.
EIU-L-D-1FUEL JETTISON DISC
(LO SPEED)SEL FLAP POSITIONSTK SHAKERVMAX CONF
~2
M7353 L-EIU (E2-6)
EIU-C-I-1
AUTO THROTTLE STATUS SAME AS L-EIU(HI SPEED)
ADF FREQUENCYADF INDENTCENTER OF GRAVITYEIU-C-D-1CONTROL MAX, MIN SPEED (SPD) SAME AS L-EIU (LO SPEED)
DATE
~2
DECISION SPDDISCRETE PARAMETER
M7352 C-EIU (E2-6)
DISTANCE TO GODMEEPRFLAP SPDFLIGHT INFORMATIONFMC BITE DATA EIU-R-I-1SAME AS L-EIU (HI SPEED)GMT TIMEWEIGHTHORZ, VERT STEERINGFMC DISCRETE EIU-R-D-1SAME AS L-EIU
(LO SPEED) INTERFACE MONITORILS
~2 MAX, MIN MANEUVER SPD
M7351 R-EIU (E2-6)
MAX ALTITUDEMIN BUFFET SPDSELECTED AIRSPEEDSELECTED ALTITUDESELECTED MACHSET CRUISE ALTITUDE
CROSS TRACK DISTANCESET LAND ALTITUDE
DESIRED TRACKSET LATITUDE, LONGITUDEDIST-TO-GOSET MAGNETIC HEADING DRIFT ANGLESTAB TRIM MAP BACKGROUNDTAKEOFF CLIMB AIRSPEED ENERGY MANAGEMENT BRAKESTARGET AIRSPEED ENERGY MANAGEMENT CLEANTEMPERATURE SELECTED ESTIMATED TIME OF ARRIVALTIME FOR CLIMB, DESCENTFLIGHT PATH ANGLETIME TO TOP OF DESCENT FMC DISCRETETRUE AIR TEMP GROUND SPDUTILITY SPDPRESENT POS LAT, LONGVERT SPD COMMANDRANGE TO ALTITUDEVERT STEERING RATE START DYNAMIC DATAVOR TRACK ANGLEVR AIRSPEEDVERTICAL DEVIATIONVREF AIRSPEED V1 SPD WAYPOINT BEARINGVR/VREF SPDWRAP AROUND TEST WAYPOINT BEARINGTRANSITION ALTITUDE WIND SPD, DIR
FMC - Integrated Display System Interface
Figure 13
IFMC-L-B-1
IFMC-L-B-2
IFMC-L-B-3
IFMC-L-D-5
IFMC-L-D-6
IFMC-R-B-1
IFMC-R-B-2
IFMC-R-B-3
IFMC-R-D-5
IFMC-R-D-6
M7443 R-FMC (E2-1)
NOTE: ~2 INDICATES THE ITEMAPPEARS TWICE
M7348 R-ND(P3)
M7347 R-PFD(P3)
A
747-400
MAINTENANCE MANUAL
NOTE: ~2 INDICATES ITEMAPPEARS TWICE IFMC-L-B-1
ALONG TK HRZ ACCEL
BODY LATERAL ACCEL
~2
BODY LONGIT ACCEL
IFMC-L-B-2B7161 L-IRU (E1-6)BODY NORMAL ACCEL
B7161 L-IRU (E1-6)CROSS TK HRZ ACCELE-W VELOCITY
IFMC-L-B-3
FLIGHT PATH ACCEL
GROUND SPEED
INERTIAL ALTITUDE
M7442 L-FMC (E2-3)
INERTIAL VERT SPD
IRS DISCRETES
~2
MAGNETIC HEADING
N-S VELOCITY
B7162 R-IRU (E1-6)
B7163 C-IRU (E1-6) IFMC-R-B-1
PITCH ANGLE
PRESENT POS-LAT
PRESENT POS-LONG
ROLL ANGLE
IFMC-R-B-2
TRACK ANGLE TRUE
TRUE HEADING
VERTICAL ACCEL
IFMC-R-B-3
~2 INITIAL:
B7163 C-IRU (E1-6)ì LATITUDE M7443 R-FMC (E2-1)
B7162 R-IRU (E1-6)
ì LONGITUDE
ì MAGNETIC HDG
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
34-61-00
ALL ú ú 02 Page 32 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
FMC - Inertial Reference System
Figure 14
IFMC-L-B-1
IFMC-L-B-3
IFMC-L-B-2
M7442 L-FMC (E2-3)
IFMC-R-B-1
IFMC-R-B-3
IFMC-R-B-2
M7443 R-FMC (E2-1)B10010 R-MMR(E1-4) B10010 R-MMR(E1-4)
NOTE: ~2 INDICATES ITEM APPEARS TWICE.
FMC - NAV Radio Interface
Figure 15
A
747-400
MAINTENANCE MANUAL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
34-61-00
ALL ú ú 11 Page 33 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
K65730
A
747-400
MAINTENANCE MANUAL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：747-400 AMM 飞机维护手册 导航 NAVIGATION 3(122)
