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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