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Config-2 Aug 01/02
+---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | X999 | (-9.0 to 40.0 deg) | | | param. 1B.1.137.01 System 1 | | | param. 1B.2.137.10 System 2 | |--------------|------------------------------------------------------| | SLAT | Slat Actual Position | | X999 | (-9.0 to 27.0 deg) | | | param. 1B.1.127.01 System 1 | | | param. 1B.2.127.10 System 2 | |--------------|------------------------------------------------------| | THDG | True Heading (BCD) | | X9999 | (0 to 359.9 deg) | | | param. 04.1.044.01 System 1 | | | param. 04.2.044.10 System 2 | |--------------|------------------------------------------------------| | LONP | Longitude Position | | X9999 | (East 179.9 deg to West 179.9 deg) | | | param. 04.1.311.XX System 1 | | | param. 04.2.311.XX System 2 | |--------------|------------------------------------------------------| | LATP | Latitude Position | | X9999 | (North 89.9 to South 89.9 deg) | | | param. 04.1.310.XX System 1 | | | param. 04.2.310.XX System 2 | |--------------|------------------------------------------------------| | WS | Wind Speed | | 999 | (0 to 100 kts) | | | param. 04.1.315.01 System 1 | | | param. 04.2.315.10 System 2 | |--------------|------------------------------------------------------| | WD | WIND Direction - True | | 999 | (0 to 359 deg) | | | param. 04.1.316.01 System 1 | | | param. 04.2.316.10 System 2 | |--------------|------------------------------------------------------| | FT | Fuel Temperature | | X999 | (-60.0 to 170.0 C) | | | param. 5A.2.177.10 Fuel Temp. Left Wing Tank | | | param. 5A.2.201.10 Fuel Temp. Right Wing Tank | |--------------|------------------------------------------------------| | FD | Fuel Temperature | | 0999 | (0 to 0.999 kg/l) | | | param. 5A.2.272.10 | +---------------------------------------------------------------------+
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Config-2 Aug 01/02
(2) Cruise Performance Report Logic (Engine Type IAE)
+----------------------------------------------------------------------+ |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 | 2 | | |E | Transfer to ACARS MU | C | No | | |F | Increment of the report counter if the | C | 1 | | | | report was triggered by a code number | | | | | | > 1000; 1=yes, 0=no | | | | |G | Averange intervales in seconds | AI | 20 | | |H | Overall Average of .F02. averages | AI | 5 | | |I | OIQ values taken from .taxi out. used | | | | | | for QIQH calculation the same program-| | | | | | ming as for Report <01> is apply. | | | |----|------|-----------------------------------------|------|---------| |1000|1 | Manual selection via MCDU | | | |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | | | |2.1 | Logic algorithm | | | | |2.2 | Remote Print Button assignment | C | not | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Logic algorithm | C | | | |3.2 | Trigger condition | C | not | |----|------|-----------------------------------------|------|---------| |5000| | The DMU generates the Cruise Performance| | | | | | Report based on .Flight Hours. or | | | | | | .Flight Legs. programmable via GSE. | | | | | | | | | | | | Logic based on Flight Hours: | | | | | | | | | | | | During a time frame of .Y02.1. flight | | | | | | hours the DMU search in flight phase 6 | | | | | | for report generation with stable frame | | | | | | criteria where the best aircraft quality| | | | | | number QA is calculated. The report with| | | | | | the best quality number QA is stored in | | | | | | the report buffer: | | | | | | | | |
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本文链接地址：getting to grips with aircraft performance monitoring(88)
