747飞机维护手册AMM CHAPTER 34 - NAVIGATION 第34章导航4(129)

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V87 VALVE 4 PYLON CLOSE  PACKAGE (E3-1) M836 FUEL FLOW ELECTRONICS  DATA OUT  LO HI  17 16  RZ BI POLAR  E9 E8  LO HI  BCD EIU DATA IN  INDICATOR (P2) N255 PMS LIMIT 
SHUTOFF AND PRESSURE REGULATING RIGHT WING  UNIT (E2-5) B762 PMS ENGINE INTERFACE  UNIT (E2-5) B752 PMS COMPUTER  IB AIRPLANES EFFECTIVITY 
Performence Management System Engine Interface Schematic 
Figure 12 (Sheet 2) 

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Performance Managment System Airframe Interface Schematic
Figure 13

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B164 CENTRAL AIR DATA B752 PMS COMPUTER UNIT (E2-5) COMPUTER -2 (E1-5)
Performance Management System Air Data Interface Schematic
Figure 14

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B753 PMS SWITCHING B763 PMS CONTROL DISPLAY DATA WARN C5DATA WARN T P R DATA IN DATA OUT U LO HI LO HI S UNIT (P9)  R-Z BI-POLAR R-Z BI-POLAR  E22 E18 E19 E20 E21  HI LO LO HI  CDU A DATA IN CDU A/B DATA OUT PMS WARN  BINARY OUTPUT DATA WARN INS-1 ACCELERATION VERTICAL SYNC CLOCK DATA  HI LO  F60 F66 F65 F64 F63 F62 F61 E50 E49  ARINC 583 BINARY  DATA VALID DATA VALID DATA VALID DATA VALID VERTICAL ACCELERATION DATA, CLOCK, SYNC DATA, CLOCK, SYNC DATA, CLOCK, SYNC DATA, CLOCK, SYNC PMS INPUT CHANNEL A CHANNEL B BINARY OUTPUT 
UNIT (E2-5) 
DATA IN DATA WARN DATA OUT  HI LO HI LO  R U P S T  R-Z BI-POLAR  E24 E25  LO HI  (LSP) DATA IN CDU-8  INS-1 INPUT  SYNC CLOCK DATA  E13 E12 E17 E16 E11 E10  ARINC 583 BINARY  B109 INS-1 NAV UNIT (E2-6) INPUT PMSDATA, CLOCK, SYNC DATA VALID 
B812 PMS LIMIT SELECT PANEL (P8)  DATA WARN  E7  DATA, CLOCK, SYNC DATA VALID  CHANNEL A 
B762 ENGINE INTERFACE 17 5 16 4 LO HI -+ DATA OUT DC IN  EIU POWER R-Z BI-POLAR  E8 E9 E14 E15  LO HI -+  BCD EIU DATA IN DC OUT  INS-3 INPUT  SYNC CLOCK DATA  B8 B9 B4 B5 B6 B7  ARINC 583 BINARY  B173 INS-3 NAV UNIT (E2-6) OUTPUT BINARY CHANNEL B DATA, CLOCK, SYNC DATA, CLOCK, SYNC DATA VALID DATA VALID 
UNIT (E2-5)  DATA WARN  B1 
FLAG  E6  DME-1 WARN 
DISTANCE  ARINC 568 PULSE PAIR  LO HI E4 E5  DISTANCE DME-1  DATA  C95 C94  DATA VALID DATA, CLOCK, SYNC  PMS INPUT 
N123 FLT ENGR'S CLOCK (P4) GMT OUT FLAG DISTANCE B81 DME-1 INTERROGATOR (E3-6) B82 DME-2 INTERROGATOR (E3-6)  ARINC 568 PULSE PAIR ARINC 419 BCD  F57 F58 C80 C96 C97  DME-2 DME-2 WARN DISTANCE LO HI GMT IN LO HI  INS-2 INPUT DATA WARN SYNC CLOCK ACCELERATION INS-2 VERTICAL LIMIT OUT INDICATION  HI LO LO HI  C87 C93 C92 C91 C90 C106 C105 E60 E59  ARINC 575 BINARY 9 10 ARINC 583 BINARY  HI LO  DIGITAL DATA IN  DATA VALID DATA VALID DATA VALID DATA, CLOCK, SYNC DATA, CLOCK, SYNC DATA, CLOCK, SYNC CHANNEL A CHANNEL B BINARY OUTPUT B110 INS-2 NAV UNIT (E2-6) VERTICAL ACCELERATION 
DATA WARN  E58  8  DATA WARN 
N255 PMS LIMIT 
B752 PMS COMPUTER UNIT (E2-5)  INDICATOR (P2) 
Performance Management System and INS Interface Schematic 
Figure 15 
EFFECTIVITY 

AIRPLANES WITH PMS
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28V DC  PMS SU PRIM  ENGAGE A/T  TURB  OFF 
PROVISIONS  V/S 
IAS  PMS  CMD  PMS 
A CMD +  ROLL A+B+C 
PMSD  B42  C CMD  ON F/D  CH-C CH-B  HOLDING SWITCH TURB/SPEED 
LRRA-1 TRIP LRRA-2  B CMD  CH-C CH-B  SOLENOID 
TRIP  C2 F2 E2  A C B  A/P CMD  ROLL DC  MAN  SWITCH ENGAGE CMD  B1  DC 
C15 F15 E15 B18 C94  C B A  V/S HOLD TURB IAS HOLD PMS ENG A/P-F/D MODE SELECT PANEL OFF  ALT SEL ARM . ALT SELECT . PMS ENG FD ON . (MAN+CMD) SS G/S ENG  C66 C67  TURB/SPEED SW INHIBIT TURB/SPEED SW ENABLE  PMS AMS  + 250 m SEC SS 
　
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