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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| |----|------|-----------------------------------------|------|---------| | | | performed deltaTNref5 and deltaTNref6 | | | | | | are stored and used for the TNdiv | | | | | | calculation (Item 4.4.1): | | | | | | | | | | | | The same rules (analog to 4.3) as for | | | | | | EGT divergence applies except TN#1 is | | | | | | not corrected for deviations in N1. | | | |----|------|-----------------------------------------|------|---------| | |5 | In case of divergence detection and | | | | | | report generation, the search logic for | | | | | | the engine cruise report <01> CODE 7000 | | | | | | for stable frame is started at once. | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ09'| | | | | | The report <09> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----------------------------------------------------------------------| | A = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
**ON A/C ALL
H. Engine Start Report <10>
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(Ref. Fig. 009)
R **ON A/C 106-149, 159-199, 210-299, 301-399, 401-499,
(Ref. Fig. 009A)
1EFF : ALL 1 31-37-73Page A84 1 1 Aug 01/05 1 1 1CES 1
Engine Start Report <10>
(Engine Type CFMI with Advanced EVMU)
Figure 009
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A85 1201-209, 1May 01/05 1 1 1CES 1
Engine Start Report <10>
(Engine Type CFMI with Advanced EVMU)
Figure 009A
R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A86 1401-499, 1Aug 01/05 1 1 1CES 1
**ON A/C ALL
The Engine Start Report shall be a time series collection of engine related information as a function of number of flights and when an abnormal condition has been detected during a main engine start. The report is generated when one of the logic conditions 1000 to 7009 (for details see Engine Start report logic) is present.
R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(1) Engine Start Report Data Field Description <10> (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 |
R 1EFF : ALL 1 31-37-73Page A87 1 1 May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | | 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 | | | 3 = G/S TRACK | | | 4 = G/S CAPTURE | | | 5 = V/S | | | 6 = FPA | | | 7 = ALT | | | 8 = ALT ACQ | | | 9 = OPEN CLB | | | A = OPEN DES | | | B = IM CLB | | | C = IM DES | | | D = CLB | | | E = DES | | | F = FINAL DES | | | G = EXPEDITE | | | | | | AP1 | AP2 | | | Report Line EC: | Report Line EE: |Difinition: | | | -------------------|-------------------|------------ | | | / | / |No Mode Act. | | | -------------------|-------------------|------------ | | | 01.1.275.00.11 = 1 | 01.2.275.00.11 = 1|RUNWAY Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.12 = 1 | 01.2.275.00.12 = 1|NAV Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.13 = 1 | 01.2.275.00.13 = 1|LOC CAPTURE | | | | |Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.14 = 1 | 01.2.275.00.14 = 1|LOC TRACK | | | | |Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.15 = 1 | 01.2.275.00.15 = 1|Roll GO | | | | |AROUND Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.16 = 1 | 01.2.275.00.16 = 1|HEADING Mode | | | -------------------|-------------------|------------ |
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