R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-51Page 49 1201-209, 1May 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Limit | Description of Report Item |V2500- |V2527- |SPARE |SPARE | Unit | |No | |A1 |A5 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 343 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 344 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 345 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 346 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 347 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 348 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 349 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 350 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 351 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 352 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 353 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 354 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 355 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 356 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 357 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 358 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 359 | Reserved | 0 | 0 | 0 | | | |------|--------------------------------|-------|-------|-------|------|------| | 360 | Reserved | 0 | 0 | 0 | | | +-----------------------------------------------------------------------------+
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AIDS - ENGINE REPORTS - DESCRIPTION AND OPERATION
_________________________________________________
1. General
_______ The AIDS Reports are results of the related AIDS monitored aircraft systems (refer to the list below for the list of reports which are available). The reports can be requested manually or are started automatically. The monitor functions have fixed trigger mechanisms, fixed data collection and output formatting. Collected monitored-aircraft-data is automatically supplied to the related systems during unusual aircraft operation. If a report is requested manually with the remote print button, it is generated immediately (independently of any other start logic). The manually or automatically generated reports (stored in the SSMM) can be transferred to the printer and/or the MDDU, and/or the ACARS and/or the DAR/SAR. Some parameters for customer requirements are re-programmable through the MCDU or by GSE (For more information refer to 31-36-00). The following Engine AIDS Reports are available:
-<01> Engine Cruise Report,
-<02> Cruise Performance Report,
-<04> Engine Take-Off Report,
-<05> Engine On-Request Report,
-<06> Engine Gas Path Advisory Report,
-<07> Engine Mech Advisory Report,
-<09> Engine Divergence Report,
-<10> Engine Start Report, R - <11> Engine Run Up Report.
2. Reports
_______
A. Engine Cruise Report <01> (Ref. Fig. 001) The engine cruise report is a collection of aircraft and engine information averaged over a period of time in which both the engine and the aircarft met the appropriate stability criteria. The engine cruise report is generated when one of the logic conditions 1000 to 7000 (for details see engine cruise report logic) is present.
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Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU)
Figure 001
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R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(1) Engine Cruise Report Data Field Description <01> (Engine Type CFMI with Advanced EVMU)
+---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | ESN | Engine Serial Number | | 999999 | (000000 to 999999) | | | Eng 1 param. 7C.1.046.01 digit 3, 2, 1 | | | 7C.1.047.01 digit 6, 5, 4 | | | Eng 2 param. 7C.2.046.01 digit 3, 2, 1 | | | 7C.2.047.01 digit 6, 5, 4 | |--------------|------------------------------------------------------| | EHRS | Engine Flight Hours | | 99999 | (00000 to 99999 hours) | | | DMU Engine 1 and Engine 2 | |--------------|------------------------------------------------------| | ERT | Engine Running Time | | 99999 | (00000 to 65536 hours) | | | Eng 1 param. 7C.1.050.01 | | | Eng 2 param. 7C.2.050.10 | |--------------|------------------------------------------------------| | ECYC | Engine Cycle | | 99999 | (00000 to 99999) | |--------------|------------------------------------------------------| | AP | Auto Pilot Status | | 99 | (00 to G8) | | | FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 | | | | | | XX Auto Pilot Modes: | | | || | | | ||__Lateral Modes: 0 = NO MODE | | | | 1 = HEADING | | | | 2 = TRACK | | | | 3 = NAV | | | | 4 = LOC CAPTURE | | | | 5 = LOC TRACK | | | | 6 = LAND TRACK | | | | 7 = RUNWAY | | | | 8 = ROLL GO AROUND | | | | | | | |__Longitudinal Modes: 0 = NO MODE | | | 1 = PITCH G/A | | | 2 = PITCH T/O |
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