R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A21 1401-499, 1Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | 19 7C.X.270.XX.19 = 1 No/Low fan speed for core | | | speed | | | 20 7C.X.270.XX.20 = 1 No Eng. light off detected| | | 21 7C.X.270.XX.21 = 1 Starter time limit exceed.| | | 22 7C.X.270.XX.22 = 1 Fuel schedule derich activ| | | 23 7C.X.270.XX.23 = 1 TLA not idle start initia.| | | 24 SPARE | | | 25 7C.X.270.XX.25 = 1 Low Sap detected | | | 26 7C.X.270.XX.28 = 1 50% thrust limit active | | | 27 SPARE | | | 28 SPARE | | | 29 SPARE | |--------------|------------------------------------------------------| | TAT/ALT/CAS/| For parameter description see "Standard Header for | | MN/GW/CG | Print Report" (Refer to 31-36-00). | | | | | | Parameter in Report Line C1/CE: Ambient Condition | | | at the time "S1"/"T1". | | | | | | Parameter in Report Line C3: Ambient Condition at | | | the time "V1"/"X1". | |--------------|------------------------------------------------------|
(2) Engine Report O/R Logic <05> (Engine Type CFMI with Advanced EVMU)
+----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |A | Report Format | | | | |B | Parameter Table | | | | |C | First three lines of Report | C | Blank | | |D | Print Out Rules | C | | | |E | Transfer to ACARS MU | C | Yes | | |F | Increment of the report counter if the | C | 1 | | | | report was triggered by a code number | | | | | | > 1000; 1=yes, 0=no | | | |----|------|-----------------------------------------|------|---------| |1000|1 | Manual selection via MCDU | | | |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | |
R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A22 1401-499, 1Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |2.1 | Remote Print Button assignment. | C | 4,5,5.1,| | | | | | 6,7,7.1,| | | | | | 8,9,10 | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | | | | | | progr. | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ05'| | | | | | The report <05> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
**ON A/C ALL
E. Engine Gas Path Advisory Report <06> (Ref. Fig. 006) The Engine Gath Path Advisory Report shall be a collection of engine related information when there has been an exceedance of one of the primary engine parameters. In practicular STALL, FRAME-OUT, SHUTDOWN, EGT, N1 and N2 shall be monitored for exceedance conditions. The report is generated when one of the logic conditions 1000 to 6000 (for details see Engine Gas Path Advisory Report logic) is present.
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Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) Figure 006 (SHEET 1)
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Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) Figure 006 (SHEET 2)
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R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(1) Engine Gas Path Advisory Report Data Field Description <06> (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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