曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

On the CAPT and F/O PFDs, compare andwrite the altitude and airspeed values for the ADIRU 3 (in relation to the applicable Trim) and the ADIRU 1.
The rate of descent must not be morethan 6000 ft/mn.
R 1EFF : 151-199, 1 34-13-00Page 573 1 1 May 01/05 1 1 1CES 1

 (1) ADIRUs 1 and 2

 ------------------------------------------------------------------------------| | CAPT PFD and F/O PFD | | Pressure generator | AIR DATA switch at | AIR DATA switch | | | NORM |at CAPT/3 or F/O/3 | |------------------------------|-----------------------|---------------------| | Ps | Pt | QC |Hp 1/2| Vc 1/2|Mach 1/2| | | (ft)|(hpa)| (ft)|(hpa)|Pt-Ps | (ft) |(Kts) | | | | | | | | (hpa)| | +/- 2| | | |-----|-----|-----|-----|------|------|-------|--------| | | 5257| 835 | 1827|948.1|113.1 |5000 | 250 |0.413(*)| For ADIRU 3 values, | | | | | | |+/-12 | |+/-0.004| | |-----|-----|-----|-----|------|------|-------|--------| refer to the tables | |10253| 690 | 6335|801.8|111.8 |10000 | 250 |0.452(*)| | | | | | | |+/-15 | |+/-0.004| that follow | |-----|-----|-----|-----|------|------|-------|--------| | |20192|461.9|13009|619.2|157.3 |20000 | 300 | 0.651 | (in relation to the | | | | | | |+/- 22| |+/-0.004| | |-----|-----|-----|-----|------|------|-------|--------| applicable Trim) | |30058|300.1|20576|454.5|154.4 |30000 | 300 | 0.791 | | | | | | | |+/- 30| |+/-0.003| | |-----|-----|-----|-----|------|------|-------|--------| | |40004|187.5|30620|292.5| 105 |39995 | 250 | 0.823 | | | | | | | |+/- 42| |+/-0.003| | ------------------------------------------------------------------------------
R 1EFF : 151-199, 1 34-13-00Page 574 1 1 May 01/05 1 1 1CES 1

 (2) ADIRU 3
 (a) Aircraft with Trim = +250ft
 --------------------------------------------------------| | CAPT PFD and F/O PFD | | Pressure generator | AIR DATA switch | | | at CAPT/3 or F/O/3 | |------------------------------|-----------------------| | Ps | Pt | QC | Hp 3 | Vc 3 | Mach 3 | | (ft)|(hpa)| (ft)|(hpa)|Pt-Ps | (ft) |(Kts) | | | | | | | (hpa)| | +/-2 | | |-----|-----|-----|-----|------|------|------|---------| | 5257| 835 | 1827|948.1|113.1 | 5305 | 261 |0.433 (*)| | | | | | |+/- 12| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |10253| 690 | 6335|801.8|111.8 | 10370| 261 |0.475 (*)| | | | | | |+/- 15| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |20192|461.9|13009|619.2|157.3 | 20940| 316 | 0.697 | | | | | | |+/- 22| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |30058|300.1|20583|454.5|154.4 | 31630| 319 | 0.863 | | | | | | |+/- 30| |+/-0.003 | |-----|-----|-----|-----|------|------|------|---------| |40004|187.5|30618|292.5| 105 | 41595| 265 | 0.896 | | | | | | |+/- 42| |+/-0.003 | --------------------------------------------------------
R 1EFF : 151-199, 1 34-13-00Page 575 1 1 May 01/05 1 1 1CES 1 (b) Aircraft with Trim = +150ft

 --------------------------------------------------------| | CAPT PFD and F/O PFD | | Pressure generator | AIR DATA switch | | | at CAPT/3 or F/O/3 | |------------------------------|-----------------------| | Ps | Pt | QC | Hp 3 | Vc 3 | Mach 3 | | (ft)|(hpa)| (ft)|(hpa)|Pt-Ps | (ft) |(Kts) | | | | | | | (hpa)| | +/-2 | | |-----|-----|-----|-----|------|------|------|---------| | 5257| 835 | 1827|948.1|113.1 | 5305 | 261 |0.433 (*)| | | | | | |+/- 12| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |10253| 690 | 6335|801.8|111.8 | 10370| 261 |0.475 (*)| | | | | | |+/- 15| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |20192|461.9|13009|619.2|157.3 | 20860| 315 | 0.694 | | | | | | |+/- 22| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |30058|300.1|20583|454.5|154.4 | 31520| 318 | 0.859 | | | | | | |+/- 30| |+/-0.003 | |-----|-----|-----|-----|------|------|------|---------| |40004|187.5|30618|292.5| 105 | 41485| 264 | 0.891 | | | | | | |+/- 42| |+/-0.003 | --------------------------------------------------------
R 1EFF : 151-199, 1 34-13-00Page 576 1 1 May 01/05 1 1 1CES 1 (c) Aircraft with Trim = 0ft

 --------------------------------------------------------| | CAPT PFD and F/O PFD | | Pressure generator | AIR DATA switch | | | at CAPT/3 or F/O/3 | |------------------------------|-----------------------| | Ps | Pt | QC | Hp 3 | Vc 3 | Mach 3 | | (ft)|(hpa)| (ft)|(hpa)|Pt-Ps | (ft) |(Kts) | | | | | | | (hpa)| | +/-2 | | |-----|-----|-----|-----|------|------|------|---------| | 5257| 835 | 1827|948.1|113.1 | 5305 | 261 |0.433 (*)| | | | | | |+/- 12| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |10253| 690 | 6335|801.8|111.8 |10370 | 261 |0.475 (*)| | | | | | |+/- 15| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |20192|461.9|13009|619.2|157.3 |20790 | 314 | 0.690 | | | | | | |+/- 22| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |30058|300.1|20583|454.5|154.4 |31340 | 316 | 0.851 | | | | | | |+/- 30| |+/-0.003 | |-----|-----|-----|-----|------|------|------|---------| |40004|187.5|30618|292.5| 105 |41320 | 263 | 0.883 | | | | | | |+/- 42| |+/-0.003 | --------------------------------------------------------
　
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