R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page 97 1201-209, 1May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | |_______________ 29, 28, 27 0...7 | | | --------------------------------------------| | | Bit Label Parameter Description | | | 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable | | | 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable | | | 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable | | | 14 7C.X.272.XX.22 = 1 MTO. GA limit mode select.| | | 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode | | | selected | | | 16 SPARE | | | 17 SPARE | | | 18 SPARE | | | 19 SPARE | | | 20 SPARE | | | 21 SPARE | | | 22 SPARE | | | 23 SPARE | | | 24 SPARE | | | 25 SPARE | | | 26 SPARE | | | 27 SPARE | | | 28 SPARE | | | 29 SPARE | |--------------|------------------------------------------------------|

 |  PSEL  |  Status of different FADEC sensors  |
 |  XXXX  |  X X X X  Label:  Selected:  (Bit 11 --> 15)  |
 |  |  I I I I___ 211  TST  |
 |  |  I I I ____ 344  N2 actual  |
 |  |  I I_______ 345  EGT  |
 |  |  I_________ 346  N1 actual  |
 |  |  (All labels Bit 11 --> 15)  |
 |  |  Source: ECU, different labels  |
 |  |  The indicated values shall be coded as follows:  |
 |  |  Bit: 15  14  13  12  11  | indicated value  |
 |  |  --------------------|---------------- |
 |  |  0  0  0  0  0  |  0  |
 |  |  0  0  0  0  1  |  1  |
 |  |  0  0  0  1  0  |  2  |
 |  |  0  0  0  1  1  |  3  |
 |  |  0  0  1  0  0  |  4  |
 |  |  0  0  1  0  1  |  5  |
 |  |  0  0  1  1  0  |  6  |
 |  |  0  0  1  1  1  |  7  |
 |  |  0  1  0  0  0  |  8  | 

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page 98 1201-209, 1May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | 0 1 0 0 1 | 9 | | | 0 1 0 1 0 | A | | | 0 1 0 1 1 | B | | | 0 1 1 0 0 | C | | | 0 1 1 0 1 | D | | | 0 1 1 1 0 | E | | | 0 1 1 1 1 | F | | | 1 0 0 0 0 | G | | | 1 0 0 0 1 | H | | | 1 0 0 1 0 | I | | | 1 0 0 1 1 | J | | | 1 0 1 0 0 | K | | | 1 0 1 0 1 | L | | | 1 0 1 1 0 | M | | | 1 0 1 1 1 | N | | | 1 1 0 0 0 | O | | | 1 1 0 0 1 | P | | | 1 1 0 1 0 | Q | | | 1 1 0 1 1 | R | | | 1 1 1 0 0 | S | | | 1 1 1 0 1 | T | | | 1 1 1 1 0 | U | | | 1 1 1 1 1 | V | | | | |--------------|------------------------------------------------------| | PT2 | Total Air Pressure at Position 2 | | 99999 | (0.0 to 25.000 psia) | | | Eng 1 param. 7C.1.131.01 | | | Eng 2 param. 7C.2.131.10 | |--------------|------------------------------------------------------| | FT | Fuel Temperature Inner Cell | | X99 | (-55.0 to 170.0 C) | | | param. 5A.2.177.10 Left Wing Tank | | | 5A.2.201.10 Right Wing Tank | |--------------|------------------------------------------------------| | HPT | High-Pressure Turbine Clearance Position | | X99 | (-10 to 100 %) | | | Eng 1 param. 7C.1.306.01 | | | Eng 2 param. 7C.2.306.10 | |--------------|------------------------------------------------------| | LPT | Low-Pressure Turbine Position | | X99 | (-10 to 100 %) | | | Eng 1 param. 7C.1.307.01 | | | Eng 2 param. 7C.2.307.10 |

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page 99 1201-209, 1May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| |--------------|------------------------------------------------------| | RALT | Radio Height | | X999 | (-20 to 2500 ft) | | | param 25.1.164.01 Radio Altimeter #1 printed in | | | 25.2.164.01 report line X1 | | | param 25.1.164.10 Radio Altimeter #2 printed in | | | 25.2.164.10 report line X2 | +---------------------------------------------------------------------+

 (2) Engine Take Off Report Logic <04> (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 | 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 | 'Y04.2' Avergange intervals in seconds | C | 2 | | | | for OIT, OIP, VB1, VB2 and PHA. | | | |----|------|-----------------------------------------|------|---------| |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 | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | |----|------|-----------------------------------------|------|---------| |4000|4 | The report is generated and stored every| | | | | | 'F04' Take-Off and is triggered when | | | | | | during a searching time period of 20 | | | | | | seconds the sum of both engines the EGT | | | | | | is maximal. The searching time period | | | | | | is started 'Y04.1' seconds after enter- | | |
　
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