A330 - A340 MCDU Training Просмотр ZIP-архива

mcdu/A330 MCDU-PW/TEST_ATA7080.txt

PAGE=ECUTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1LB=LAST LEG, SMALLFONT
 1LD=<REPORT
 2LB=PREVIOUS LEGS, SMALLFONT
 2LD=<REPORT
 3LD=<LRU IDENT
 4LD=<GND SCANNING
 5LB=TROUBLE SHOOT, SMALLFONT
 5LD=<DATA
 6LD=<RETURN, CYAN
 1RB=
 1RD=
 2RB=SYSTEM,SMALLFONT
 2RD=TEST>
 3RB=SUBSYSTEM,SMALLFONT
 3RD=TESTS>
 4RB=GUIDED,SMALLFONT
 4RD=TEST>
 5RB=GROUND,SMALLFONT
 5RD=REPORT>
 6RB=OTHER FAULT,SMALLFONT
 6RD=REPORT>
 LSK1L=LASTLEGRPT
 LSK1R=LASTLEGCL3
 LSK2L=PREVLEGFAULTDEF
 LSK3L=LRUIDENTDEF
 LSK4L=GNDSCANDATADEF
 LSK5R=GNDREPORTDEF
 LSK5L=TROUBLEDATADEF
 LSK6L=$RETURN
 LSK2R=ECUSYSTEMTEST
 LSK3R=ENGINETESTS
 LSK4R=GUIDEDTEST
 LSK6R=OTHERFAULTREPORTS
ENDPAGE

PAGE=ECUSYSTEMTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=SYSTEM TEST
 2CB=INITIAL CONDITIONS:, SMALLFONT
 2CD=-SET ADIRU 1 + 2 TO NAV, SMALLFONT
 5LD=<START TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUTEST
 LSK5L=ECUSYSTEMTEST2
ENDPAGE

PAGE=ECUSYSTEMTEST2
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=SYSTEM TEST
 2CD=TEST IN PROGRESS 3 S, SMALLFONT
 6RD=PRINT*,CYAN
 GOTO3SEC=ECUSYSTEMTEST3
ENDPAGE

PAGE=ECUSYSTEMTEST3
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=SYSTEM TEST
 2CD=TEST OK
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUTEST
 LSK5L=TESTRESULTFORMAT
ENDPAGE
 
PAGE=ENGINETESTS
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=SUBSYSTEMS TEST
 1LD=<REVERSER ISOL VALVE TEST
 2LD=<ACTUATORS TEST
 3LD=<REVERSER CYCLING TEST
 4LD=<IGNITERS TEST
 5LD=<PROBE HEATER TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK1L=REVISOLTEST
 LSK6L=ECUTEST
 LSK2L=ACTUATORSTEST
 LSK3L=REVERSERTEST
 LSK4L=IGNITIONTEST
 LSK5L=PROBEHEATTEST
ENDPAGE

PAGE=PROBEHEATTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=PROBE HEATER TEST
 1LD=CAUTION:, AMBER
 2LB=PROBE WILL GET HOT, SMALLFONT, AMBER
 5LD=<START OF TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK5L=PROBEHEATTEST2
ENDPAGE

PAGE=PROBEHEATTEST2
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=PROBE HEATER TEST
 2CD=TEST IN PROGRESS 10 S, SMALLFONT
 6RD=PRINT*,CYAN
 GOTO3SEC=PROBEHEATTEST3
ENDPAGE

PAGE=PROBEHEATTEST3
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=PROBE HEATER TEST
 2CD=TEST OK, SMALLFONT
 6LD=<RETURN,CYAN 
 6RD=PRINT*,CYAN
LSK6L=ENGINETESTS
ENDPAGE

PAGE=ACTUATORSTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=ACTUATORS TEST 1/2
 1LD=CAUTION:, AMBER
 1CD=ENGINE WILL, SMALLFONT, AMBER, #10
 2LB=ROTATE AND COMPONENTS, SMALLFONT, AMBER
 2LD=WILL MOVE DURING TEST, SMALLFONT, AMBER
 3LB=INITIAL CONDITIONS, SMALLFONT
 3LD=-SUPPLY STARTER AIR, SMALLFONT
 4LB=-SET ENGINE MODE SEL, SMALLFONT
 4LD=SWITCH TO CRANK, SMALLFONT
 5LB=-SET ENGINE MAN START, SMALLFONT
 5LD=TO ON, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 ARROWDN=ACTUATORSTEST2
 ARROWUP=ACTUATORSTEST2
ENDPAGE

PAGE=ACTUATORSTEST2
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=ACTUATORS TEST 2/2
 1LD=CAUTION:, AMBER
 1CD=ENGINE WILL, SMALLFONT, AMBER, #10
 2LB=ROTATE AND COMPONENTS, SMALLFONT, AMBER
 2LD=WILL MOVE DURING TEST, SMALLFONT, AMBER
 3LB=INITIAL CONDITIONS, SMALLFONT
 4LB=-WAIT FOR ENGINE TO, SMALLFONT
 4LD=STABILIZE ABOVE 20% N2, SMALLFONT
 5LD=<START TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK5L=ACTUATORSTEST3
ENDPAGE

PAGE=ACTUATORSTEST3
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=ACTUATORS TEST 2/2
 1LD=CAUTION:, AMBER
 1CD=ENGINE WILL, SMALLFONT, AMBER, #10
 2LB=ROTATE AND COMPONENTS, SMALLFONT, AMBER
 2LD=WILL MOVE DURING TEST, SMALLFONT, AMBER
 5LD=<CONFIRM START OF TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK5L=ACTUATORSTEST4
ENDPAGE

PAGE=ACTUATORSTEST4
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=ACTUATORS TEST 2/2
 2CD=TEST IN PROGRESS 60 S, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 GOTO3SEC=ACTUATORSTEST5
ENDPAGE

PAGE=ACTUATORSTEST5
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=ACTUATORS TEST 2/2
 2CB=TEST OK
 5LD=<TEST CLOSE UP
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK5L=ACTUATORSTEST6
 LSK5R=TESTRESULTFORMAT
ENDPAGE

PAGE=ACTUATORSTEST6
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=ACTUATORS TEST
 1CD=TEST CLOSE UP, SMALLFONT
 2LB=-SET ENGINE MODE SEL, SMALLFONT
 2LD= SWITCH TO NORM, SMALLFONT
 3LB=-SET ENGINE MAN START, SMALLFONT
 3LD= TO OFF, SMALLFONT
 4LB=-SWTICH OFF STARTER AIR, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
ENDPAGE

PAGE=REVERSERTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER CYCLING TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=WILL MOVE DURING TEST, SMALLFONT, AMBER
 2LD= INITIAL CONDITIONS:, SMALLFONT
 3LB= THROTTLE LEVER AT IDLE, SMALLFONT
 3LD= T/R NOT INHIBITED, SMALLFONT
 4LB= SELECT HYD PRESS ON, SMALLFONT
 5LD=<START TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK5L=REVERSERTEST2
ENDPAGE

PAGE=REVERSERTEST2
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER CYCLING TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=WILL MOVE DURING TEST, SMALLFONT, AMBER
 3LB=WAIT FOR 10 SECONDS, SMALLFONT
 5LD=<CONFIRM START OF TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK5L=REVERSERTEST3
ENDPAGE
 
PAGE=REVERSERTEST3
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER CYCLING TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=WILL MOVE DURING TEST, SMALLFONT, AMBER
 3LB=-PULL ENG THROTTLE, SMALLFONT
 3LD= LEVER TO MAX REVERSE, SMALLFONT
 4LB= WITHIN 50 SECONDS, SMALLFONT
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 GOTO3SEC=REVERSERTEST4
ENDPAGE

PAGE=REVERSERTEST4
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER CYCLING TEST
 2LB= TEST IN PROGRESS 10 SEC, SMALLFONT
 3LB=T/R DEPLOYING, SMALLFONT
 GOTO3SEC=REVERSERTEST5
ENDPAGE

PAGE=REVERSERTEST5
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER CYCLING TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=WILL MOVE DURING TEST, SMALLFONT, AMBER
 3LB= T/R CURRENTLY DEPLOYED, SMALLFONT 
 4LD= PUSH ENG THROTTLE, SMALLFONT
 4LB= LEVER TO IDLE WITHIN, SMALLFONT
 5LB= 50 SECONDS, SMALLFONT
 GOTO3SEC=REVERSERTEST6
ENDPAGE

PAGE=REVERSERTEST6
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER CYCLING TEST
 2CD=TEST OK
 4LD=<T/R CYCLING AGAIN
 5LD=<TEST CLOSE UP
 6RD=PRINT*,CYAN
 LSK5L=REVERSERTEST7
 LSK4L=REVERSERTEST3
ENDPAGE

PAGE=REVERSERTEST7
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER CYCLING TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=WILL MOVE DURING TEST, SMALLFONT, AMBER1CD=TEST CLOSE UP
 2LD=TEST CLOSE UP, SMALLFONT
 3LB=CONFIRM ENG THROTTLE, SMALLFONT
 3LD=LEVER AT IDLE, SMALLFONT
 4LB=SELECT HYD PRESSURE OFF, SMALLFONT
 4LD=IF FAILURE DETECTED, SMALLFONT
 5LB=PROCEED PER TROUBLE, SMALLFONT
 5LD=SHOOTING PROCEDURE, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
ENDPAGE

PAGE=IGNITIONTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 TLR=1/2, #20
 1CB=IGNITERS TEST
 1LD=CAUTION:, AMBER
 1CD=DRY CRANK THE, SMALLFONT, AMBER, #10
 2LB=ENGINE TO REMOVE ANY, SMALLFONT, AMBER
 2LD=RESIDUAL FUEL BEFORE, SMALLFONT, AMBER
 3LB=RUNNING THIS TEST, SMALLFONT, AMBER
 ARROWDN=IGNITIONTEST1
 ARROWUP=IGNITIONTEST1

PAGE=IGNITIONTEST1
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 TLR=2/2, #20
 1CB=IGNITERS TEST
 1LD=CAUTION:, AMBER
 1CD=IGNITERS WILL, SMALLFONT, AMBER, #10
 2LB=SPARK DURING TEST., SMALLFONT, AMBER
 3LB=INITIAL CONDITIONS:, SMALLFONT
 3LD=-SET MASTER LEVER TO ON, SMALLFONT
 5LD=<START TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK5L=IGNITIONTEST2
 ARROWDN=IGNITIONTEST
 ARROWUP=IGNITIONTEST
ENDPAGE

PAGE=IGNITIONTEST2
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 TLR=2/2, #20
 1CB=IGNITERS TEST
 1LD=CAUTION:, AMBER
 1CD=IGNITERS WILL, SMALLFONT, AMBER, #10
 2LB=SPARK DURING TEST., SMALLFONT, AMBER
 4LD=<CONFIRM START OF TEST
 6LD=<TEST CLOSE UP,CYAN
 6RD=PRINT*,CYAN
 LSK6L=IGNITIONTEST6
 LSK4L=IGNITIONTEST3
ENDPAGE

PAGE=IGNITIONTEST3
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=IGNITERS TEST
 1LD=CAUTION:, AMBER
 1CD=IGNITERS WILL, SMALLFONT, AMBER, #10
 2LB=SPARK DURING TEST., SMALLFONT, AMBER
 3LD=<ENABLE IGNITOR 1 
 4LD=<ENABLE IGNITOR 2
 5LD=<TEST CLOSE UP,CYAN
 6RD=PRINT*,CYAN
 LSK5L=IGNITIONTEST6
 LSK3L=IGNITIONTEST4A
 LSK4L=IGNITIONTEST4B
ENDPAGE


PAGE=IGNITIONTEST4A
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=IGNITERS TEST
 2CD=TEST IN PROGRESS, SMALLFONT
 3CB=IGNITOR 1 ON, SMALLFONT
 3LD=AUDIBLY VERIFY THAT THE, SMALLFONT
 4LB=IGNITOR SPARKED, SMALLFONT
 5LD=<YES, SMALLFONT
 5RD=NO>, SMALLFONT
 6RD=PRINT*,CYAN
 LSK5R=IGNITIONTEST5B
 LSK5L=IGNITIONTEST5A
ENDPAGE

PAGE=IGNITIONTEST4B
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=IGNITERS TEST
 2CD=TEST IN PROGRESS, SMALLFONT
 3CB=IGNITOR 2 ON, SMALLFONT
 3LD=AUDIBLY VERIFY THAT THE, SMALLFONT
 4LB=IGNITOR SPARKED, SMALLFONT
 5LD=<YES, SMALLFONT
 5RD=NO>, SMALLFONT
 6RD=PRINT*,CYAN
 LSK5R=IGNITIONTEST5B
 LSK5L=IGNITIONTEST5A
ENDPAGE

PAGE=IGNITIONTEST5B
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=IGNITERS TEST
 2LD=ATA, SMALLFONT
 2RD=CLASS, SMALLFONT
 3LD=742161, SMALLFONT
 3RD=1, SMALLFONT
 4LB=IGN CABLE/IGN PLUG, SMALLFONT
 6RD=PRINT*,CYAN
 6LD=TEST CONT/CLOSE
 LSK6L=IGNITIONTEST3
ENDPAGE

PAGE=IGNITIONTEST5A
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=IGNITERS TEST
 2CD=TEST OK, SMALLFONT
 4LD=<CONTINUE TEST, SMALLFONT
 5LD=<TEST CLOSE UP, SMALLFONT
 6RD=PRINT*,CYAN
 LSK4L=IGNITIONTEST3
 LSK5L=IGNITIONTEST6
ENDPAGE

PAGE=IGNITIONTEST6
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=IGNITERS TEST
 1CD=TEST CLOSE-UP
 3LB=-SET MASTER LEVER TO OFF, SMALLFONT
 3LD=(THIS WILL RESET THE EEC, SMALLFONT
 4LB= AND EXIT MAINTENANCE , SMALLFONT
 4LD= MODE), SMALLFONT
 6LD=<RETURN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
ENDPAGE

PAGE=RUNNINGTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=ENGINE RUNNING TEST
 2LD=-DISCRETE OF, SMALLFONT
 2CD=@VAR(1), #14, SMALLFONT
 2RD=@VAR(2), #20, SMALLFONT
 3LB=TO ENGINE RUNNING STATE, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ACPOWERTEST
ENDPAGE

PAGE=GUIDEDTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=GUIDED TESTS
 2LD=<A/C POWERED OUTPUT TEST, SMALLFONT
 3LD=<GROUND HARNESS TEST, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK2L=ACPOWERTEST
 LSK6L=ECUTEST
ENDPAGE

PAGE=ACPOWERTEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=A/C POWERED OUTPUT TEST
 2LD=<ENG RUNNING TEST, SMALLFONT
 4LD=<NAI SYSTEM IND TEST, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=GUIDEDTEST
 LSK2L=RUNNINGTEST
 LSK4L=NAITEST
ENDPAGE

PAGE=NAITEST
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=NAI SYSTEM IND TEST
 2LD=-INITIAL CONDITIONS, SMALLFONT
 3LD= PUSH THE ENG-A-ICE P/B, SMALLFONT
 5LD=<START TEST, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK5L=NAITEST2
 LSK6L=ACPOWERTEST
ENDPAGE

PAGE=NAITEST2
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=NAI SYSTEM IND TEST
 2LD=MAKE SURE THAT THE ANTI, SMALLFONT
 3LB=ICE FAULT LIGHT COMES ON, SMALLFONT
 5LD=<YES, SMALLFONT
 5RD=NO>, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK5L=NAITEST3
 LSK5R=NAITEST3A
 LSK6L=ACPOWERTEST
ENDPAGE

PAGE=NAITEST3
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=NAI SYSTEM IND TEST
 3LD=RELEASE THE ENG-A-ICE , SMALLFONT
 4LB=P/B TO OFF POSITION, SMALLFONT 
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=NAITEST4
ENDPAGE

PAGE=NAITEST3A
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=NAI SYSTEM IND TEST
 2CD=NAI SYSTEM IND TEST, SMALLFONT
 3CB=FAILED, SMALLFONT
 4LD=30-21-60, SMALLFONT
 5LB=WRG:EEC J14 TO NAI, SMALLFONT
 5LD=NOT OPEN SIG, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ACPOWERTEST
ENDPAGE

PAGE=NAITEST4
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=NAI SYSTEM IND TEST
 4CB=TEST OK, SMALLFONT 
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ACPOWERTEST
ENDPAGE

PAGE=OTHERFAULTREPORTS
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=OTHER FAULT REPORTS
 2LD=<PREVIOUS GROUND REPORTS
 3LD=<SCHEDULED MAINT REPORT
 4LD=<PREVIOUS SCHD MAINT REPORT
 5LD=<EXEEDANCE REPORTS
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUTEST
 LSK2L=PREVIOUSGROUNDREPORTS
 LSK3L=SCHEDULEDMAINTREPORT
 LSK4L=PREVIOUSSCHDMAINTREPORT
 LSK5L=EXEEDANCEREPORTS
ENDPAGE

PAGE=PREVIOUSGROUNDREPORT
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 TLR=1/4
 1CB=CURRENT STATUS, SMALLFONT
 1CD=INPUT DISCRETE STATE, SMALLFONT
 2LB=  DISCRETE     STATE A/B, SMALLFONT
 2LD=A/THR ENGAGEMENT     O/O, SMALLFONT
 3LB=INST DISCONNECT      C/C, SMALLFONT
 3LD=ALTERNATE START      O/O, SMALLFONT
 4LB=EIVMU TRDV PWR SW    O/O, SMALLFONT
 4LD=EIVMU IGNA PWR SW    O/O, SMALLFONT
 5LB=EIVMU IGNB PWR SW    O/O, SMALLFONT
 5LD=REV INHIB SW         O/O, SMALLFONT
 6LB=MASTER LEVER SW      C/C, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUSPECIFIC
 ARROWDN=CURRSTATUS2
 ARROWUP=CURRSTATUS4
ENDPAGE

PAGE=PREVIOUSSCHDMAINTREPORT
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 TLR=2/4
 1CB=CURRENT STATUS, SMALLFONT
 1CD=INPUT ANALOG STATE, SMALLFONT
 2LB=ANALOG STATE  A  /  B, SMALLFONT
 2LD= TRA =    - 0.19 /- 0.27, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUSPECIFIC
 ARROWDN=CURRSTATUS3
 ARROWUP=CURRSTATUS1
ENDPAGE

PAGE=REVISOLTEST
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 1CB=REVERSER ISOL VLV TEST
 2LB=THIS TEST WILL CONFIRM, SMALLFONT
 2LD=IF THE REVERSER SYSTEM, SMALLFONT
 3LB=IS FAILED PRESSURIZED, SMALLFONT
 5LD=<CONTINUE
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK5L=REVISOLTEST2
 LSK6L=ENGINETESTS
ENDPAGE

PAGE=REVISOLTEST2
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER ISOL VLV TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=WILL MOVE DURING TEST, SMALLFONT, AMBER
 2LD=-INITIAL CONDITIONS:, SMALLFONT
 3LB=-THROTTLE LEVER AT IDLE, SMALLFONT
 3LD=-T/R NOT INHIBITED, SMALLFONT
 4LB=-T/R FULLY STOWED, SMALLFONT 
 4LD=SELECT HYD PRESS ON, SMALLFONT
 5LD=<START TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK5L=REVISOLTEST3
ENDPAGE

PAGE=REVISOLTEST3
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER ISOL VLV TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=MAY MOVE DURING TEST, SMALLFONT, AMBER
 3CB=WAIT FOR 10 SECONDS, SMALLFONT
 4LD=<CONFIRM START OF TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 LSK4L=REVISOLTEST4
ENDPAGE

PAGE=REVISOLTEST4
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER ISOL VLV TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=MAY MOVE DURING TEST, SMALLFONT, AMBER
 3LB=-MOVE ENG THROTTLE, SMALLFONT
 3LD= LEVER TO MAX REVERSE, SMALLFONT
 4LB= WITHIN 50 SECONDS, SMALLFONT
 6RD=PRINT*,CYAN
 GOTO3SEC=REVISOLTEST5
ENDPAGE

PAGE=REVISOLTEST5
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER ISOL VLV TEST
 2CD=TEST IN PROGRESS, SMALLFONT
 4LB=IF REVERSER DEPLOYS, SMALLFONT
 4LD=ISOLATION VALVE FAILED, SMALLFONT
 5LB=PRESSURIZED, SMALLFONT
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
 GOTO3SEC=REVISOLTEST6
ENDPAGE

PAGE=REVISOLTEST6
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER ISOL VLV TEST
 1LD=CAUTION:, AMBER
 1CD=NACELLE SURFACE, SMALLFONT, AMBER, #10
 2LB=MAY MOVE DURING TEST, SMALLFONT, AMBER
 4LD=-MOVE ENG THROTTLE, SMALLFONT
 5LB= LEVER TO IDLE WITHIN, SMALLFONT
 5LD= 50 SECONDS, SMALLFONT
 6RD=PRINT*,CYAN
 GOTO3SEC=REVISOLTEST7
ENDPAGE

PAGE=REVISOLTEST7
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER ISOL VLV TEST
 2CD=TEST OK
 4LD=<REPEAT TEST, SMALLFONT
 5LD=<TEST CLOSE UP, SMALLFONT
 6RD=PRINT*,CYAN
 LSK5L=REVISOLTEST8
 LSK4L=REVISOLTEST
ENDPAGE

PAGE=REVISOLTEST8
 TLC=@VAR(1), #10
 TLR=@VAR(2), #15
 1CB=REVERSER ISOL VLV TEST
 1CD=TEST CLOSE UP, SMALLFONT
 2LB=CAUTION, SMALLFONT, AMBER, #10
 2LB=NACELLE SURFACE, SMALLFONT, AMBER,
 2LD=MAY MOVE DURING TEST, SMALLFONT, AMBER
 3LD=-CONFIRM ENG THROTTLE, SMALLFONT
 4LB= LEVER AT IDLE, SMALLFONT
 4LD=-SELECT HYD PRESSURE OFF, SMALLFONT
 5LB=-IF FAILURE DETECTED, SMALLFONT
 5LD= PROCEED PER TROUBLE, SMALLFONT
 6LB= SHOOTING PROCEDURE, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ENGINETESTS
ENDPAGE

PAGE=EXEEDANCEREPORTS
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 1CB=EXEEDANCE REPORTS
 2LB=      DATE      UTC
 2LD=     21APR     13:24
 3LB=  N1 PEAK:     101.3%RPM, SMALLFONT
 3LD=  N1 TIME:         2 SEC, SMALLFONT
 4LB=  N2 PEAK:     102.0%RPM, SMALLFONT
 4LD=  N2 TIME:         2 SEC, SMALLFONT
 5LB= EGT PEAK:     640.2DEGC, SMALLFONT
 5LD= EGT TIME:         2 SEC, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=OTHERFAULTREPORTS
ENDPAGE

PAGE=PWRMAXSET2
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 1CB=PWR SETTING MAX VALUES, SMALLFONT
 1LD= physical values:, SMALLFONT
 2LB= VALUE   REACHED   TIME, SMALLFONT
 2LD=  N1     102.3%     12S, SMALLFONT
 3LB=  N2     101.9%     12S, SMALLFONT
 3LD=  EGT    803DEG      3S, SMALLFONT
 4LB= INDICATED VALUES:, SMALLFONT
 4LD=  N1     102.2%     11S, SMALLFONT
 5LB=  EGT    789DEG      2S, SMALLFONT
 5LD=<CONFIRM RESET
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUSPECIFIC
 LSK5L=PWRMAXSET3
ENDPAGE

PAGE=PWRMAXSET3
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 1CB=PWR SETTING MAX VALUES, SMALLFONT
 1LD=            MAX, SMALLFONT
 2LB= VALUE   REACHED   TIME, SMALLFONT
 2LD=  N1         0%      0S, SMALLFONT
 3LB=  N2         0%      0S, SMALLFONT
 3LD=  EGT      0DEG      0S, SMALLFONT
 4LB= INDICATED VALUES:, SMALLFONT
 4LD=  N1         0%      0S, SMALLFONT
 5LB=  EGT      0DEG      0S, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUSPECIFIC
 VARPAGE=PWRMAXSET3
ENDPAGE

PAGE=ECUFUELUSED1
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 1CB=FUEL USED, SMALLFONT
 2CD=21790 KG
 5LD=<RESET VALUE
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUSPECIFIC
 LSK5L=ECUFUELUSED2
ENDPAGE

PAGE=ECUFUELUSED2
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 1CB=FUEL USED, SMALLFONT
 2CD=21790 KG
 4LD=<CONFIRM RESET
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUSPECIFIC
 LSK4L=ECUFUELUSED3
ENDPAGE

PAGE=ECUFUELUSED3
 VARPAGE2=ECUFUELUSED3
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 1CB=FUEL USED, SMALLFONT
 2CD=0 KG
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUSPECIFIC
ENDPAGE

PAGE=SCHEDULEDMAINTREPORT
 TLL=@VAR(1), #10
 TLC=@VAR(2), #15
 TLR=1/X
 1CB=SCHEDULED MAINT REPORT, SMALLFONT
 1LD=UTC    ATA
 2LD=----  ------
 3LB=------------------------
 3LD=------------------------
 4LD=----  ------
 5LB=------------------------
 5LD=------------------------
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=ECUSPECIFIC
ENDPAGE

;------------- EIVMU PAGES ----------------

PAGE=EIVMUTEST
 TLC=@VAR(1)
 1LB=LAST LEG, SMALLFONT
 1LD=<REPORT
 2LB=PREVIOUS LEGS, SMALLFONT
 2LD=<REPORT
 3LD=<LRU IDENT
 4LD=<GND SCANNING
 5LB=TROUBLE SHOOT, SMALLFONT
 5LD=<DATA
 6LD=<RETURN, CYAN
 1RB=CLASS 3,SMALLFONT
 1RD=FAULTS>
 2RD=TEST>
 5RB=GROUND,SMALLFONT
 5RD=REPORT>
 6RB=SPECIFIC,SMALLFONT
 6RD=DATA>
 LSK1L=LASTLEGRPT
 LSK1R=LASTLEGCL3
 LSK2L=PREVLEGFAULTDEF
 LSK3L=LRUIDENTDEF
 LSK4L=GNDSCANDATADEF
 LSK5R=GNDREPORTDEF
 LSK5L=TROUBLEDATADEF
 LSK6L=$RETURN
 LSK2R=TESTEIVMU1
 LSK6R=EIVMUSPECIFIC
ENDPAGE

PAGE=TESTEIVMU1
 TLC=@VAR(1)
 1CB=TEST
 2LB=INITIAL CONDITIONS:, SMALLFONT
 2LD=@VAR(1), #9, SMALLFONT
 2CD=-SELECT FADEC, #1, SMALLFONT
 2RD=GROUND, #17, SMALLFONT
 3LB= POWER ON, SMALLFONT
 5LD=<START TEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUTEST
 LSK5L=TESTEIVMU2
ENDPAGE

PAGE=TESTEIVMU2
 TLC=@VAR(1)
 1CB=TEST
 2CD=TEST IN PROGRESS 4 S, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 GOTO3SEC=TESTEIVMU3
ENDPAGE

PAGE=TESTEIVMU3
 TLC=@VAR(1)
 1CB=TEST
 2CD=TEST OK
 5LD=?, SMALLFONT, GRAY
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUTEST
 LSK5L=TESTRESULTFORMAT
ENDPAGE

PAGE=EIVMUSPECIFIC
 TLC=@VAR(1)
 1CB=SPECIFIC DATA, SMALLFONT
 2LB=FAN, SMALLFONT
 2LD=<UNBALANCE
 4LB=MAX FLIGHT, SMALLFONT
 4LD=<VIB DISPLAY
 5LB=FREQUENCY, SMALLFONT
 5LD=<ANALYSIS
 2RB=DISCRETE, SMALLFONT
 2RD=INPUTS>
 3RB=DISCRETE, SMALLFONT
 3RD=OUTPUTS>
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUTEST
 LSK4L=EIVMUMAXFLT1
 LSK5L=EIVMUFREQANAL
 LSK2R=EIVMUDISCRINP
 LSK3R=EIVMUDISCROUTP
 LSK2L=EIVMUFANUNBAL
ENDPAGE

PAGE=EIVMUMAXFLT1
 TLC=@VAR(1)
 1CB=MAX FLIGHT VIB DISPLAY, SMALLFONT
 3LB=ACCLRM A, SMALLFONT
 3LD=<N1
 4LB=ACCLRM A, SMALLFONT
 4LD=<N2
 3RB=ACCLRM B, SMALLFONT
 3RD=N1>
 4RB=ACCLRM B, SMALLFONT
 4RD=N2>
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUSPECIFIC
 LSK3L=EIVMUMAXFLT2, VAR(2)=N1 ACCLRM A
 LSK4L=EIVMUMAXFLT2, VAR(2)=N2 ACCLRM A
 LSK3R=EIVMUMAXFLT2, VAR(2)=N1 ACCLRM B
 LSK4R=EIVMUMAXFLT2, VAR(2)=N2 ACCLRM B
ENDPAGE

PAGE=EIVMUMAXFLT2
 TLC=@VAR(1)
 TLR=1/8, SMALLFONT
 1CB=MAX FLIGHT VIB DISPLAY, SMALLFONT
 1CD=@VAR(2), SMALLFONT
 2LB= ENG S/N:------   LEG:--, SMALLFONT
 2LD=DATE:NOV09    UTC:1008.2, SMALLFONT
 3LB=   SPEED        A    B, SMALLFONT
 3LD=N1: ---%  MILS --.- --.-, SMALLFONT
 4LB=          DEG  ---  ---, SMALLFONT
 4LD=N2: ---%  IPS  --.- --.-, SMALLFONT
 5LD=     BB   IPS  --.- --.-, SMALLFONT
 6LB=LONG TERM EXPOSURE:----S, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUMAXFLT1
ENDPAGE

PAGE=EIVMUFREQANAL
 TLC=@VAR(1)
 1CB=FREQUENCY ANALYSIS, SMALLFONT
 2LB=COMMENTS, SMALLFONT
 2LD=<LINES
 3LB=AQUISITION, SMALLFONT
 3LD=<REQUEST
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUSPECIFIC
 LSK2L=FREQCOMMENT1
 LSK3L=FREQANALYSIS1
ENDPAGE

PAGE=FREQCOMMENT1
 TLC=@VAR(1)
 1CB=FREQUENCY ANALYSIS, SMALLFONT
 1CD=COMMENTS LINES, SMALLFONT
 2LD=< ENTER 1ST LINE COMMENT
 3LD=< ENTER 2ND LINE COMMENT
 4LD=< ENTER 3RD LINE COMMENT
 5LB=    COMMENTS LINE 1, SMALLFONT
 5LD=    COMMENTS LINE 2, SMALLFONT
 6LB=    COMMENTS LINE 3, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUFREQANAL
ENDPAGE

PAGE=FREQANALYSIS1
 TLC=@VAR(1)
 1CB=FREQUENCY ANALYSIS, SMALLFONT
 1CD=ACQUISITION REQUEST, SMALLFONT
 2LB=FLIGHT PHASE (01-10), SMALLFONT
 2LD={06}
 3LB=SPEED VALUE (%), SMALLFONT
 3LD={090}
 4LB=SHAFT NUMBER (N1.N2), SMALLFONT
 4LD=N1
 5LB=ACCLRM IDENT (A OR B), SMALLFONT
 5LD=A
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUFREQANAL
 LSK2L=$SWAPSCRATCH
 LSK3L=$SWAPSCRATCH
 LSK4L=$N2
 LSK5L=$B
ENDPAGE

PAGE=EIVMUDISCRINP
 TLC=@VAR(1)
 1CB=DISCRETE INPUTS, SMALLFONT
 2LB=   0 1 2 3 4 5 6 7 8 9, SMALLFONT
 2LD=00   . 0 1 . . . 0 . ., SMALLFONT
 3LB=10 1 0 1 0 1 1 0 1 0 ., SMALLFONT
 3LD=20 0 0 1 1 1 0 0 0 1 1, SMALLFONT
 4LB=30 0 0 1 . 0 0 1 0 0 0, SMALLFONT
 4LD=40 0 0 . 0 0 1 1 0 0 1, SMALLFONT
 5LB=50 0 1 0 0 0 0 1 1 0 ., SMALLFONT
 5LD=60 . . . 1 1 . . . . ., SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUSPECIFIC
ENDPAGE

PAGE=EIVMUDISCROUTP
 TLC=@VAR(1)
 1CB=DISCRETE OUTPUTS, SMALLFONT
 2LB=   0 1 2 3 4 5 6 7 8 9, SMALLFONT
 2LD=00   . 0 . 0 0 0 0 1 1, SMALLFONT
 3LB=10 . . 0 . 1 0 0 . . 1, SMALLFONT
 3LD=20 0 0 . . 0 . . . . ., SMALLFONT
 4LB=30 . . 0 . . . . . . ., SMALLFONT 
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUSPECIFIC
ENDPAGE

PAGE=EIVMUFANUNBAL
 TLC=@VAR(1)
 1CB=FAN UNBALANCE, SMALLFONT
 2LB= GROUND RUN, SMALLFONT
 2LD=<ACQN
 4LB= FLT N1 SPD, SMALLFONT
 4LD=<SETS
 2RB=LAST , SMALLFONT
 2RD=CRUISE FLT>
 3RB=PREVIOUS , SMALLFONT
 3RD=CRUISE FLT>
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUSPECIFIC
 LSK2L=EIVMUFANUNBAL2, VAR(2)=GROUND RUN ACQN
 LSK2R=EIVMUFANUNBAL2, VAR(2)=LAST CRUISE FLT
 LSK3R=EIVMUFANUNBAL2, VAR(2)=PREVIOUS CRUISE FLT
 LSK4L=EIVMUFANUNBAL3
ENDPAGE

PAGE=EIVMUFANUNBAL2
 TLC=@VAR(1)
 TLR=1/8, SMALLFONT
 1CB=FAN UNBALANCE, SMALLFONT
 1CD=@VAR(2), SMALLFONT
 2CB=ENG S/N:------, SMALLFONT
 2LD=DATE:NOV09    UTC:1008.2, SMALLFONT
 3LB=   SPEED        A    B, SMALLFONT
 3LD=N1: ---%  MILS --.- --.-, SMALLFONT
 4LB=          DEG  ---  ---, SMALLFONT
 4LD=N2: ---%  IPS  --.- --.-, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUFANUNBAL
ENDPAGE

PAGE=EIVMUFANUNBAL3
 TLC=@VAR(1)
 1CB=FAN UNBALANCE, SMALLFONT
 1CD=FTL N1 SPD SETS, SMALLFONT
 2LD=N1 SPEEDS, SMALLFONT
 3LB=20 50 65 75 80, SMALLFONT
 3LD= 50/60/67/76
 4LB=80 85 90 95 99, SMALLFONT
 4LD= 84/88/92/96
 5CD=ENTER SPEED VALUES, SMALLFONT
 6LD=<RETURN,CYAN
 6RD=PRINT*,CYAN
 LSK6L=EIVMUFANUNBAL
ENDPAGE

37859-MCDU-A330-A340.zip

Имя файла Дата Размер
mcdu/A330 MCDU-PW/ 26.12.2009 04:28
mcdu/A330 MCDU-PW/ACMSPAGE.txt 30.12.2005 18:11 8 KB
mcdu/A330 MCDU-PW/ALPHACALL.TXT 14.02.2006 07:38 5 KB
mcdu/A330 MCDU-PW/ATSUPAGES.txt 20.03.2006 23:29 44 KB
mcdu/A330 MCDU-PW/CMCCLASS3.txt 14.02.2006 07:13 5 KB
mcdu/A330 MCDU-PW/CMSPAGES.TXT 22.03.2006 14:41 25 KB
mcdu/A330 MCDU-PW/CMSRPTTEST.txt 20.04.2006 01:30 21 KB
mcdu/A330 MCDU-PW/FMSPAGES.txt 02.03.2006 23:46 24 KB
mcdu/A330 MCDU-PW/MCDU-PW.exe 03.12.2005 15:43 436 KB
mcdu/A330 MCDU-PW/MCDU-SIM-help.doc 16.12.2005 02:50 110 KB
mcdu/A330 MCDU-PW/MCDUPAGE.txt 20.04.2006 00:09 4 KB
mcdu/A330 MCDU-PW/MCDU_chk_cms.doc 18.12.2005 13:31 24 KB
mcdu/A330 MCDU-PW/SATCOMPAGE.TXT 24.12.2005 20:47 10 KB
mcdu/A330 MCDU-PW/Shortcut to MCDU-PW.exe.lnk 26.10.2007 19:32 720 B
mcdu/A330 MCDU-PW/TEST21_23.txt 25.12.2005 19:12 35 KB
mcdu/A330 MCDU-PW/TEST22.txt 02.03.2006 23:13 13 KB
mcdu/A330 MCDU-PW/TEST_ATA26_30.txt 03.05.2006 14:49 27 KB
mcdu/A330 MCDU-PW/TEST_ATA27.txt 08.02.2006 15:23 20 KB
mcdu/A330 MCDU-PW/TEST_ATA28.txt 18.11.2005 19:38 11 KB
mcdu/A330 MCDU-PW/TEST_ATA31.txt 11.02.2006 13:24 58 KB
mcdu/A330 MCDU-PW/TEST_ATA34.txt 15.02.2006 07:16 64 KB
mcdu/A330 MCDU-PW/TEST_ATA49_50.txt 11.02.2006 16:37 9 KB
mcdu/A330 MCDU-PW/TEST_ATA7080.txt 21.04.2006 12:35 24 KB
mcdu/MCDU-340 RR Trent 500/ 26.12.2009 04:28
mcdu/MCDU-340 RR Trent 500/ACMSPAGE.txt 18.01.2008 13:43 14 KB
mcdu/MCDU-340 RR Trent 500/ALPHACALL.TXT 14.02.2006 07:38 5 KB
mcdu/MCDU-340 RR Trent 500/ATSUPAGES.txt 20.03.2006 23:29 44 KB
mcdu/MCDU-340 RR Trent 500/CMCCLASS3.txt 14.02.2006 07:13 5 KB
mcdu/MCDU-340 RR Trent 500/CMSPAGES.TXT 22.03.2006 14:41 25 KB
mcdu/MCDU-340 RR Trent 500/CMSRPTTEST.txt 04.12.2008 23:13 22 KB
mcdu/MCDU-340 RR Trent 500/FMSPAGES.txt 11.01.2008 19:08 24 KB
mcdu/MCDU-340 RR Trent 500/MCDU-A340 RR Trent500.exe 03.12.2005 15:43 436 KB
mcdu/MCDU-340 RR Trent 500/MCDU-A340 RR Trent500.exe.lnk 20.02.2009 17:37 782 B
mcdu/MCDU-340 RR Trent 500/MCDU-SIM-help.doc 16.12.2005 02:50 110 KB
mcdu/MCDU-340 RR Trent 500/MCDUPAGE.txt 21.12.2007 21:53 5 KB
mcdu/MCDU-340 RR Trent 500/MCDU_chk_cms.doc 18.12.2005 13:31 24 KB
mcdu/MCDU-340 RR Trent 500/SATCOMPAGE.TXT 24.12.2005 20:47 10 KB
mcdu/MCDU-340 RR Trent 500/TEST21_23.txt 19.05.2008 18:53 36 KB
mcdu/MCDU-340 RR Trent 500/TEST22.txt 02.03.2006 23:13 13 KB
mcdu/MCDU-340 RR Trent 500/TEST_ATA26_30.txt 05.12.2008 00:06 51 KB
mcdu/MCDU-340 RR Trent 500/TEST_ATA27.txt 14.12.2007 03:22 21 KB
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 PUMPS_1.txt 21.12.2007 21:51 1010 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 PUMPS_2.txt 21.12.2007 21:59 1002 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 PUMPS_3.txt 21.12.2007 21:58 840 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 VALVES_1.txt 15.01.2008 12:18 1017 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 VALVES_2.txt 15.01.2008 12:24 1011 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 VALVES_3.txt 15.01.2008 13:05 1017 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 VALVES_4.txt 15.01.2008 12:31 1017 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 VALVES_5.txt 31.01.2008 11:03 1005 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 VALVES_6.txt 15.01.2008 12:34 851 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 VALVES_7.txt 15.01.2008 12:41 857 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28 VALVES_8.txt 15.01.2008 12:45 617 B
mcdu/MCDU-340 RR Trent 500/TEST_ATA28.txt 21.07.2008 11:51 16 KB
mcdu/MCDU-340 RR Trent 500/TEST_ATA31.txt 11.02.2006 13:24 58 KB
mcdu/MCDU-340 RR Trent 500/TEST_ATA34.txt 15.02.2006 07:16 64 KB
mcdu/MCDU-340 RR Trent 500/TEST_ATA49_50.txt 17.01.2008 16:35 9 KB
mcdu/MCDU-340 RR Trent 500/TEST_ATA7080.txt 17.12.2008 22:20 46 KB
mcdu/ 01.05.2011 20:26
avsim_su.diz 02.05.2011 00:28 406 B
Итого: 2 MB
Software for MCDU training. Airbus 330 - 340.
→ Size: 651 KB
→ Date: 15 years ago (01.05.2011 21:05)
→ Author: Airbus
→ Uploaded by: A320Flieger (uploaded 3 files )
→ Approved by moderator: omega
→ License: Freeware - Free version, Unlimited Distribution
→ Downloaded: 3129 time(s)