Power Plant Indicating - General
 Figure 001

 F 『 EEFF : ALL E Page 277-00-00
 E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E

 Control and Indicating - Component Location
 Figure 002
 F EEFF :  ALL  『E 77-00-00 Page 3 
E  E  Feb 01/98
 E  E
 ECES  E

 Upper Display Unit of the ECAM System
 Figure 003

 F 『R EEFF : 001-049, 051-099, 101-105, 151-199, E Page 477-00-00
 E E201-299, 301-302, May 01/05 E E ECES ER **ON A/C 106-149, 303-399, 401-499,

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E 

 (Ref. Fig. 003A)
 **ON A/C ALL
 - Actual N1

 - N1 Command (Ref. 77-10-00)

 - Transient N1 (blue arc) (Ref. 77-10-00)

 - N1 TLA (white circle) (Ref. 77-10-00)

 - Max N1 (Ref. 77-10-00)

 - Max permissible N1 (Ref. 77-10-00)

 - N1 exceedance (Ref. 77-10-00)

 - REV indication (Ref. 78-00-00)

 - Bump or Boost indication (Ref. 73-25-00)

 - Thrust limit mode (Ref. 73-25-00)

 - N1 rating limit (Ref. 77-10-00)

 - Actual EGT (Ref. 77-20-00)

 - Max EGT (Ref. 77-20-00)

 - Max permissible EGT (Ref. 77-20-00)

 - EGT exceedance (Ref. 77-20-00)

 - HP rotor speed N2 (Ref. 77-10-00)

 - Fuel Flow (Ref. 73-30-00)

 - Eng Anti-Ice on (Ref. 30-21-00)

 (2) Lower Display Unit of the ECAM System
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 004)
R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 004A)
 **ON A/C ALL
 - Fuel used indication (Ref. 28-40-00)

 - Oil quantity Indication (Ref. 79-31-00)

 - Oil pressure indication (Ref 79-34-00) and 79-33-00)

 - Oil temperature indication (Ref. 79-32-00)

 - VIB indications (Ref. 77-30-00)

 F 『 EEFF : ALL E Page 577-00-00
 E E Aug 01/05 E E ECES E F 『 E C F M E E E E 56-5B E

 Upper Display Unit of the ECAM System
 Figure 003A

 F 『R EEFF : 106-149, 303-399, 401-499, E Page 677-00-00
 E E Aug 01/05 E E ECES E F 『 E C F M E E E

 E 56-5B E

 Lower Display Unit of the ECAM System - Engine Pages
 Figure 004

 F 『 EEFF : 001-049, 051-099, 101-105, 151-199, E Page 777-00-00
 E E201-299, 301-302, May 01/05 E E ECES E F 『 E C F M E E E E 56-5B E

 Lower Display Unit of the ECAM System - Engine Pages
 Figure 004A

 F 『R EEFF : 106-149, 303-399, 401-499, E Page 877-00-00
 E E Aug 01/05 E E ECES E E 56-5B E E E - Oil filter clog indication (Ref. 79-35-00)

 F  『
 E  C F M  E
 E  E

 - Fuel filter clog indication (Ref. 73-30-00)

 - Ignition indication - only during start sequence (Ref 74-10-00)

 - Starter shutoff valve position indication - only during start sequence (Ref. 80-10-00)

 - Engine bleed pressure - only during start sequence (Ref. 36-20-00)

 - Nacelle temperature indication - only when temperature reach 240 deg.C (Ref. 75-41-00)

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 E E May 01/05 E E ECES E

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 E C F M E
 E E
 E 56-5B E
 E E
 ENGINE INDICATING - GENERAL - ADJUSTMENT/TEST

_____________________________________________
 TASK 77-00-00-710-043
 Read of the N1, N2 and EGT Max Pointers
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST
 Menu Page
 31-60-00-860-001 EIS Start Procedure
 31-60-00-860-002 EIS Stop Procedure
 77-00-00-991-300 Fig. 501

 3. Job Set-up
__________
 Subtask 77-00-00-861-054
 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
　
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