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)
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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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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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