R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 77 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 159-199, 210-210,
R (1) Cruise Performance Report Data Field Description <02> (Engine Type
R CFMI with Advanced EVMU)
R NOTE : Only the parts of the CRUISE PERFORMANCE REPORT <02> which are____
R not included in the ENGINE CRUISE REPORT <01> are given in the
R subsequent table.
R +---------------------------------------------------------------------+
R | Value | Content Description |
R |--------------|------------------------------------------------------|
R | TAT/ALT/CAS/| The average value for the F02 * 20 sec. of System1 |
R | MN/GW/CG | is printed in the report line CE. |
R | | |
R | | The average value for the F02 * 20 sec. of System2 |
R | | is printed in the report line CN. |
R |--------------|------------------------------------------------------|
R | QA | Aircraft Quality Number, Report Stability |
R | 99 | DMU (00 to 99) |
R |--------------|------------------------------------------------------|
R | QE | Engine Quality Number, Report Stability |
R | 99 | DMU (00 to 99) |
R |--------------|------------------------------------------------------|
R | WFQ | Fuel Quantity Inner Cell |
R | 99999 | FQIC (0 to 99999 kg) |
R | | 5A.2.257.10 Left Inner Cell Fuel Quantity |
R | | 5A.2.261.10 Right Inner Cell Fuel Quantity |
R |--------------|------------------------------------------------------|
R | ELEV | Elevator Position |
R | X999 | FCDC (-30 to 15 deg) |
R | | 6C.1.314.01 Left Elevator Position |
R | | 6C.2.314.10 |
R | | 6C.1.334.01 Right Elevator Position |
R | | 6C.2.334.10 |
R | | Negative values are shown with N in the first |
R | | position. Otherwise the first position has a 0. |
R |--------------|------------------------------------------------------|
R | AOA | Corrected Angle of Attack |
R | X999 | ADIRU (-30 to 85 deg) |
R | | 06.1.241.01 AOA System 1 |
R | | 06.2.241.10 AOA System 2 |
R | | Negative values are shown with N in the first |
R | | position. Otherwise the first position has a 0. |
R |--------------|------------------------------------------------------|
R | SLP | Side Slip Angle |
R 1EFF : 159-199, 210-210, 1 31-37-73Page 78 1 1 May 01/05 1 1 1CES 1
+---------------------------------------------------------------------+
| Value | Content Description |
|--------------|------------------------------------------------------|
R | X999 | FAC (-32.0 to 32.0 deg) |
R | | 0A.1.226.00 SLP System 1 |
R | | 0A.2.226.00 SLP System 2 |
R | | Negative values are shown with N in the first |
R | | position. Otherwise the first position has a 0. |
R |--------------|------------------------------------------------------|
R | CFPG | Calculated Flight Path Acceleration |
R | X9999 | DMU (-0.9999 to 4.0000 g) |
R | | Negative values are shown with N in the first |
R | | position. Otherwise the first position has a 0. |
R |--------------|------------------------------------------------------|
R | CIVV | Calculated Inertial Vertical Speed |
R | X999 | DMU (-999 to 999 ft/min) |
R | | Negative values are shown with N in the first |
R | | position. Otherwise the first position has a 0. |
R |--------------|------------------------------------------------------|
R | RUDD | Rudder Position |
R | X999 | SDAC (-30.0 to 30.0 deg) |
R | | 29.1.312.00 |
R | | 29.2.312.00 |
R | | Negative values are shown with N in the first |
R | | position. Otherwise the first position has a 0. |
R |--------------|------------------------------------------------------|
R | RUDT | Rudder Trim Position |
R | X999 | FAC (-25.0 to 25.0 deg) |
R | | 0A.1.313.00 |
R | | 0A.2.313.00 |
R | | Negative values are shown with N in the first |
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