| | | 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 | | | 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 指示/记录系统 4(162)
