R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 71 1 1 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | Report line 'X5' shows SLAT System 2. | |--------------|------------------------------------------------------| | THDG | True Heading (BCD) | | 9999 | ADIRU (0 to 359.9 deg) | | | 04.1.044.01 THDG System 1 | | | 04.2.044.10 THDG System 1 | | | NOTE: Report line 'X6' shows THDG System 1. | | | Report line 'X7' shows THDG System 2. | |--------------|------------------------------------------------------| | LONP | Longitude Position | | X9999 | ADIRU (East 179.9 deg to West 179.9 deg) | | | 04.1.311.01 LONP System 1 | | | 04.2.311.10 LONP System 2 | | | NOTE: The first position shows E for an East | | | position and W for a West position. | | | NOTE: Report line 'X6' shows LONP System 1. | | | Report line 'X7' shows LONP System 2. | |--------------|------------------------------------------------------| | LATP | Latitude Position | | X999 | ADIRU (North 89.9 deg to South 89.9 deg) | | | 04.1.310.XX LATP System 1 | | | 04.2.310.XX LATP System 2 | | | NOTE: The first position shows N for a North | | | position and S for a South position. | | | NOTE: Report line 'X6' shows LATP System 1. | | | Report line 'X7' shows LATP System 2. | |--------------|------------------------------------------------------| | WS | Wind Speed | | 999 | ADIRU (0 to 100 kts) | | | 04.1.315.01 WS System 1 | | | 04.2.315.10 WS System 2 | | | NOTE: Report line 'X6' shows WS System 1. | | | Report line 'X7' shows WS System 2. | |--------------|------------------------------------------------------| | WD | Wind Direction - True | | 999 | ADIRU (0 to 359 deg) | | | 04.1.316.01 WD System 1 | | | 04.2.316.10 WD System 2 | |--------------|------------------------------------------------------| | FT | Wing Fuel Temperature | | X999 | FQIC (-60.0 to 170.0 C) | | | 5A.2.177.10 Fuel Temp. Left Wing Tank | | | 5A.2.210.10 Fuel Temp. Right Wing Tank | | | NOTE: Report line 'X6' shows the fuel temperature |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 72 1 1 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | from the Left Wing Tank. | | | Report line 'X7' shows the fuel temperature | | | from the Right Wing Tank. | |--------------|------------------------------------------------------| | FD | Fuel Density | | 0999 | FQIC (0 to 0.999 kg/l) | | | 5A.2.272.10 | +---------------------------------------------------------------------+
(2) Cruise Performance Report Logic <02> (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 | Yes | | |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 | | | | |G | Average intervals in seconds | A | 20 | | |H | Overall Average of 'F02' averages | A | 5 | | |I | OIQ values taken from 'taxi out' used | A | 5 | | | | for QIQH calculation the same program-| | | | | | ming as for Report <01> applies. | | | |----|------|-----------------------------------------|------|---------| |1000|1 | Manual selection via MCDU | | | |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | | | |2.1 | Remote Print Button assignment. | C | not | | | | | | assigned| |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | | | | | | prog. | |----|------|-----------------------------------------|------|---------| |5000| | The DMU generates the Cruise Performance| | |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 73 1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------|
| | | Report based on 'Flight Hours' or | | |
| | | 'Flight Legs' programmable via GSE. | | |
| | | | | |
| | | Logic based on Flight Hours: | | |
| | | | | |
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