------------------------------------------------------------------------------
Pressure | CAPT PFD and F/O PFD 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| Hp 3 | Vc 3| Mach 3 (ft)|(hpa)| (ft)|(hpa)|Pt-Ps | (ft) |(Kts) | | (ft) |(Kts) | | | | | (hpa)| | +/- 2| | | +/-2 | -----|-----|-----|-----|------|------|-------|--------|------|------|----------5308|833.4| 1828|948 |114.6 |5000 | 250 |0.413(*)| 5405 | 264 | 0.439 (*)
| | | | |+/-12 | |+/-0.004|+/- 12| |+/-0.004 -----|-----|-----|-----|------|------|-------|--------|------|------|----------10345|687.5| 6335|801.8|114.3 |10000 | 250 |0.452(*)| 10485| 265 | 0.482 (*)
| | | | |+/-15 | |+/-0.004|+/- 15| |+/-0.004 -----|-----|-----|-----|------|------|-------|--------|------|------|----------20498|456.0|13009|619.2|163.2 |20000 | 300 | 0.651 | 21135| 319 | 0.706
| | | | |+/- 22| |+/-0.004|+/- 22| |+/-0.004 -----|-----|-----|-----|------|------|-------|--------|------|------|----------30515|293.9|20579|454.4|160.5 |30000 | 300 | 0.790 | 31845| 321 | 0.873
| | | | |+/- 30| |+/-0.003|+/- 30| |+/-0.003 -----|-----|-----|-----|------|------|-------|--------|------|------|----------40489|183.2|30618|292.5|109.3 |40000 | 250 | 0.823 | 41764| 267 | 0.903
| | | | |+/- 42| |+/-0.003|+/- 42| |+/-0.003 -------------------------------------------------------------------------------
(*) These indications are not shown when the Mach value is less than 0.5.
R **ON A/C 151-158,
Subtask 34-13-00-720-061-B
A. Functional Test of the Altitude and Airspeed Data
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
On the ground pressure generator, On the CAPT and F/O PFDs, compare and set a static pressure and a total write the altitude and airspeed values pressure as given in the table for the ADIRU 1 and 2. below.
2.
On the SWITCHING panel 8VU:
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 34-13-00Page 549 1201-209, 1May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
- set the AIR DATA selector to On the CAPT and F/O PFDs, compare and
CAPT/3. write the altitude and airspeed values
for the ADIRU 3 and 2.
- set the AIR DATA selector to On the CAPT and F/O PFDs, compare and
F/O/3. write the altitude and airspeed values
for the ADIRU 1 and 3.
3. At the end of the test, on the
ground pressure generator:
- slowly balance the pressure in The rate of descent must not be more
the static and total pressure than 6000 ft/mn.
lines.
- open the lines to get the
atmospheric pressure.
4. Stop the pressure generator.
R 1EFF : 151-158, 1 34-13-00Page 550 1 1 May 01/05 1 1 1CES 1
------------------------------------------------------------------------------Pressure | CAPT PFD and F/O PFD 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| Hp 3 | Vc 3| Mach 3 (ft)|(hpa)| (ft)|(hpa)|Pt-Ps | (ft) |(Kts) | | (ft) |(Kts) | | | | | (hpa)| | +/- 2| | | +/-2 | -----|-----|-----|-----|------|------|-------|--------|------|------|----------5257| 835 | 1827|948.1|113,1 |5000 | 250 |0.413(*)|5305 | 261 |0.433 (*)
| | | | |+/-12 | |+/-0.004|+/- 12| |+/-0.004 -----|-----|-----|-----|------|------|-------|--------|------|------|----------10253| 690 | 6335|801.8|111.8 |10000 | 250 |0.452(*)|10372 | 261 |0.475 (*)
| | | | |+/-15 | |+/-0.004|+/- 15| |+/-0.004 -----|-----|-----|-----|------|------|-------|--------|------|------|----------20192|461,9|13009|619.2|157.3 |20000 | 300 | 0.651 |20789 | 314 | 0.690
| | | | |+/- 22| |+/-0.004|+/- 22| |+/-0.004 -----|-----|-----|-----|------|------|-------|--------|------|------|----------30058|300.1|20583|454.5|154.4 |30000 | 300 | 0.791 |31342 | 316 | 0.851
| | | | |+/- 30| |+/-0.003|+/- 30| |+/-0.003 -----|-----|-----|-----|------|------|-------|--------|------|------|----------40004|187.5|30618|292.5| 105 |39995 | 250 | 0.823 |41318 | 263 | 0.883
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