|  |  | with stable frame criteria where the  |  |  |
 |  |  | best aircraft quality number QA is cal- |  |  |
 |  |  | culated. The report with the best quali-|  |  |
 |  |  | ty number QA is stored in the report  |  |  |
 |  |  | buffer and the report stored according  |  |  |
 |  |  | to logic 4000 is deleted.  |  |  |
 |  |  |  |  |  |
 |  |5  | The default programming is 'Flight Legs'| C  | Legs  |
 |  |  |  |  |  |
 |  |  | Parameter for stable frame criteria  |  |  |
 |  |5.1  | 'P01' stable period  | C  | T22/T23 |
 |  |  | (5 subperiodes=100 sec.)  |  |  |
 |  |  | Stable frame basic condition in order  |  |  |
 |  |  | to avoid report triggering in flight  |  |  |
 |  |  | phases where parameters are of no use.  |  |  |
 |  |5.2  | HPTL1 < HPT < HPTL2  |  |  |
 |  |  | HPT = 7C.1.306.01 Eng 1  |  |  |
 |  |  |  7C.2.306.10 Eng 2  |  |  |
 |  |5.2.1 | HPTL1 lower limit in %  | C  | T22/T23 |
 |  |  |  |  |  |
 |  |5.2.2 | HPTL2 upper limit in %  | C  | T22/T23 |
 |  |  |  |  |  |
 |  |  | Stable frame conditions:  |  |  |
 |  |  | During 'P01' seconds the following  |  |  |
 |  |  | parameters are stable as defined below: |  |  |
 |  |  |  |  |  |
 |  |5.3  | IALT  04.1.361.-- ft  | C  | T22/T23 |
 |  |  |  04.2.361.-- |  |  |
 |  |5.3.1 | WA of IALT  | C  | T22/T23 |
 |  |  |  |  |  |
 |  |5.4  | GS  04.1.312.01  kts  | C  | T22/T23 |
 |  |  |  04.2.312.10  |  |  |
 |  |5.4.1 | WA of GS  | C  | T22/T23 |
 |  |  |  |  |  |
 |  |5.5  | ROLL  04.1.325.01  degr.  | C  | T22/T23 |
 |  |  | ANGLE  04.2.325.10  |  |  |
 |  |5.5.1 | WA of ROLL ANGLE  | C  | T22/T23 |
 |  |  |  |  |  |
 |  |5.6  | TAT  06.1.211.01  C  | C  | T22/T23 |
 |  |  |  06.2.211.10  |  |  |
 |  |5.6.1 | WA of TAT  | C  | T22/T23 |
 |  |  |  |  |  | 

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page 14

1201-209, 1May 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |5.7 | N2 7C.1.344.01 Eng.1 % | C | T22/T23 | | | | 7C.2.344.10 Eng.2 | | | | |5.7.1 | WA of N2 | C | T22/T23 | | | | | | | | |5.8 | EGT 7C.1.345.01 Eng.1 C | C | T22/T23 | | | | | | | | |5.8.1 | WA of EGT | C | T22/T23 | | | | | | | | |5.9 | VACC 04.1.364.01 g | C | T22/T23 | | | | 04.2.364.10 | | | | |5.9.1 | WA of VACC | C | T22/T23 | | | | | | | | |5.10 | MN 06.1.205.01 Mach | C | T22/T23 | | | | 06.2.205.10 | | | | |5.10.1| WA of MN | C | T22/T23 | | | | | | | | |5.11 | N1 7C.1.346.01 Eng.1 % | C | T22/T23 | | | | 7C.2.346.10 Eng.2 | | | | |5.11.1| WA of N1 | C | T22/T23 | | | | | | | | |5.12 | PT2 7C.1.131.91 Eng.1 psia | C | T22/T23 | | | | 7C.2.131.10 Eng.2 | | | | |5.12.1| WA of PT2 | C | T22/T23 | | | | | | | | |5.13 | FF 7C.1.244.01 Eng.1 kg/h | C | T22/T23 | | | | 7C.2.244.10 Eng.2 | | | | |5.13.1| WA of FF | C | T22/T23 | | | | | | | | |5.14 | HPT 7C.1.306.01 Eng.1 % | C | T22/T23 | | | | 7C.2.306.10 Eng.2 | | | | |5.14.1| WA of HPT | C | T22/T23 | | | | | | | | |5.15 | LPT 7C.1.307.01 Eng.1 % | C | T22/T23 | | | | 7C.2.307.10 Eng.2 | | | | |5.15.1| WA of LPT | C | T22/T23 | | | | | | | | | | HPT and LPT variation are programmable | | | | | | in the range from 0.0 to 99.9 %. | | | |----|------|-----------------------------------------|------|---------| |6001|6 | Independant from the other logic a best | | | |6002| | stable frame search logic for a Eng. | | | |6003| | Cruise Rep.<01> is started as long as | | |
　
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