R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-37-73Page B71 1201-210, 1May 01/05 1 1 1CES 1
(4) A319: CFMI Engines 56-5-B7
+-----------------------------------------------------------------------------+
R |Report| Limit | Description of Report Item |56-5-B7| SPARE | SPARE | Unit |
R |Item N| No. | | | | | |
R |------|-------|-------------------------------|-------|-------|-------|------|
R | 5.1 | 265 | EGTL limit | 725 | | | deg |
R |------|-------|-------------------------------|-------|-------|-------|------|
R | 6.1 | 266 | F10.1 cycle | 25 | | |nbcyc.|
R |------|-------|-------------------------------|-------|-------|-------|------|
R | 6.2 | 267 | N2 trigger value | 40 | | | % |
R |------|-------|-------------------------------|-------|-------|-------|------|
R | 7.2 | 268 | No of consecutive legs (X10) | 5 | | | |
+-----------------------------------------------------------------------------+
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-37-73Page B72 1201-210, 1May 01/05 1 1 1CES 1
T. Report Limits fpr Engine Run-up Report <11>.
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
+-----------------------------------------------------------------------------+ |Report| Description of Report Item |56-5-A1|56-5-A3|56-5-B4|SPARE | Unit | |Item N| | | | | | | |------|--------------------------------|-------|-------|-------|------|------|
| |
| N O T A P P L I C A B L E |
| |
+-----------------------------------------------------------------------------+
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-37-73Page B73 1201-210, 1May 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Limit | Description of Report Item |56-5-B1|56-5-B2|56-5-B3|SPARE | Unit | |No | | | | | | | |------|--------------------------------|-------|-------|-------|------|------|
| |
| N O T A P P L I C A B L E |
| |
+-----------------------------------------------------------------------------+
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-37-73Page B74 1201-210, 1May 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Limit | Description of Report Item |56-5-A5|56-5-B6|56-5-B5|56-5A4| Unit | |No | | | | | | | |------|--------------------------------|-------|-------|-------|------|------|
| |
| N O T A P P L I C A B L E |
| |
+-----------------------------------------------------------------------------+
(4) A319: CFMI Engines 56-5-B7
+-----------------------------------------------------------------------------+ |Limit | Description of Report Item |56-5-B7| SPARE | SPARE | SPARE| Unit | |No | | | | | | | |------|--------------------------------|-------|-------|-------|------|------| | | | N O T A P P L I C A B L E | | | +-----------------------------------------------------------------------------+
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-37-73Page B75 1201-210, 1May 01/05 1 1 1CES 1
R **ON A/C 106-149, 211-299, 301-399, 401-499,
K. Report Limits for Engine Cruise Report <01>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
+-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | CFM | SPARE | Unit | |Item | |56-5-A1|56-5-A3|56-5-B4| | | | | |-------|-------|-------|-------|------| | | |DMU/ID |DMU/ID |DMU/ID | | | | | | CFM #1| CFM #2| CFM #3| | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.1 |'Y01.1' flight hours | 0 | 0 | 0 | | hours| |------|-------------------------------|-------|-------|-------|-------|------| | 4.2 |'Y01.2' minutes after cruise | 10 | 10 | 10 | | min | | | entry | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.3 |'Y01.3' flight legs | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.1 |'P01' stable periods | 5 | 5 | 5 | | | | | ( 1 period = 20 sec) | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.2.1| HPTL1 valve position lower | 0 | 0 | 70 | | % | | | limit | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.2.2| HPTL2 valve position upper | 20 | 20 | 105 | | % | | | limit | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.3 | IALT stable frame variation | 150 | 150 | 150 | | ft | |------|-------------------------------|-------|-------|-------|-------|------| | 5.3.1| Weighting Factor Wa of IALT | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.4 | GS stable frame variation | 6 | 6 | 6 | | kts | |------|-------------------------------|-------|-------|-------|-------|------| | 5.4.1| Weighting Factor Wa of GS | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.5 | ROLL ANGLE stable frame | 4.0 | 4.0 | 4.0 | | deg | | | variation | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.5.1| Weighting Factor Wa of ROLL | 1 | 1 | 1 | | | | | ANGLE | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.6 | TAT stable frame variation | 2.0 | 2.0 | 2.0 | | deg C| |------|-------------------------------|-------|-------|-------|-------|------| | 5.6.1| Weighting Factor Wa of TAT | 1 | 1 | 1 | | |
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