A320飞机维护手册 AMM 指示/记录系统 5(58)

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 |  |4.3.6 | KL limit | C  | T22/T23 |
 |  |4.3.7 | C09.1 limit for climb PH5 in C/%N1 | C  | T22/T23 |
 |  |4.3.8 | C09.2 limit for cruise PH6 in C/%N1 | C  | T22/T23 |
 |  |4.3.9 | M programmed limit | C  | T22/T23 |
 |  | | - deltaEGTref is calculated twice per |  |  |
 |  | | flight leg independently after enter- |  |  |
 |  | | ing the PH 5.1 and 6, when conditions |  |  |
 |  | | 1-10 are met. |  |  |
 |  | | - deltaEGTref-1 is the deltaEGTref cal- |  |  |
 |  | | culated in the last flight. |  |  |
 |  | | - K is incremented by one for each |  |  |
 |  | | flight leg until KL is reached. Then |  |  |
 |  | | K = KL is remained as long as: |  |  |
 |  | | - Engine S/N is not changed |  |  |
 |  | | - A/C-ID is not changed |  |  |
 |  | | - The defined values of KL, C09.1,|  |  |
 |  | | C09.2 and the threshold values |  |  |
 |  | | under item 4.1.1 and 4.1.10 are |  |  |
 |  | | not changed. |  |  |
 |  | | - If there is a change as a.m. items |  |  |
 |  | | then the K and deltaEGTref-1 is set |  |  |
 |  | | to 0. |  |  |
 |  | | - K and deltaEGTref-1 values can be |  |  |
 |  | | reset via MCDU menu. |  |  |
 |  | | |  |  |
 |  |4.3.10| actual K value printed in AIDS report |  |  | 

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A76

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| |----|------|-----------------------------------------|------|---------| | | | limit list | | | | |4.3.11| actual EGT ref value for PH 5.1 printed | | | | | | in AIDS report limit list | | | | |4.3.12| actual EGT ref value for PH 6 printed | | | | | | in AIDS report limit list | | | | |4.3.13| actual TN ref value for PH 5.1 printed | | | | | | in AIDS report limit list | | | | |4.3.14| actual TN ref value for PH 6 printed | | | | | | in AIDS report limit list | | | | |4.4 | TN Divergence Calculation | | | | |4.4.1 | TNdiv = deltaTNdiff - deltaTNref | | | | | | The deltaTNref calculation is represen- | | | | | | ted in mathematical form as below: | | | | |4.4.2 | deltaTNdiff = TN#1 - TN#2 | | | | |4.4.3 | This calculation is done 'M' consecutive| | | | | | times once per socond i.e. during 10 | | | | | | seconds. | | | | |4.4.4 | deltaTNdef = deltaTNref-1 + 1/K+1 * | | | | | | (deltaTNm - deltaTNref-1) | | | | | | deltaTNref-1 = deltaTNref from the | | | | | | previous flight leg. | | | | |4.4.5 | After the deltaTNref calculation the | | | | | | following TNdiff calculation is perform-| | | | | | ed. | | | | |4.4.6 | deltaTN = TN#1 - TN#2 | | | | | | deltaTNref PH 5.1 | | | | | | DMU | | | | | | deltaTNref PH 6 | | | | | | DMU | | | | | | The same rules as for EGT divergence is | | | | | | applied, except TN#1 is not corrected | | | | | | for deviations in N1. | | | |----|------|-----------------------------------------|------|---------| | |5 | In case of divergence detection and | | | | | | report generation, the search logic for | | | | | | the engine cruise report <01> CODE 7000 | | | | | | for stable frame is started at once. | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ09'| | | | | | The report <09> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----------------------------------------------------------------------|

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A77 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| |----|------|-----------------------------------------|------|---------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+

 

R **ON A/C 106-149, 159-199, 210-299, 301-399, 401-499,
 (2) Engine Divergence Report Logic <09> (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 | | | |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 | | | |----|------|-----------------------------------------|------|---------| |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 | | | | | | progr. | |----|------|-----------------------------------------|------|---------| | |4 | If during flight phase climb and cruise | | | | | | (5.1 and 6) the condition as defined | | | | | | under item 4.2 are met the EGT Divergen-| | | | | | ce (EGTdiv) and TN Divergence (TNdiv) | | | | | | monitoring functions are performed as | | | | | | defined under item 4.3 to 4.4. | | |
　
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