--------------------------------------------------------| | 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 | 20720| 313 | 0.686 | | | | | | |+/- 22| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |30058|300.1|20583|454.5|154.4 | 31210| 314 | 0.845 | | | | | | |+/- 30| |+/-0.003 | |-----|-----|-----|-----|------|------|------|---------| |40004|187.5|30618|292.5| 105 | 41160| 261 | 0.877 | | | | | | |+/- 42| |+/-0.003 | --------------------------------------------------------
R 1EFF : 151-199, 1 34-13-00Page 578 1 1 May 01/05 1 1 1CES 1 (e) 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 | 20680| 312 | 0.685 | | | | | | |+/- 22| |+/-0.004 | |-----|-----|-----|-----|------|------|------|---------| |30058|300.1|20583|454.5|154.4 | 31110| 313 | 0.840 | | | | | | |+/- 30| |+/-0.003 | |-----|-----|-----|-----|------|------|------|---------| |40004|187.5|30618|292.5| 105 | 41060| 260 | 0.872 | | | | | | |+/- 42| |+/-0.003 | --------------------------------------------------------
(*) These indications are not shown when the Mach value is less than 0.5.
R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
5. Close-up
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R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
Post SB 34-1252 For A/C 154-158,207-209,
Subtask 34-13-00-080-052
A. Remove the ground support and maintenance equipment, the special and standard tools and all other items. Make sure that there is no remaining piece of plastic and/or adhesive tape on the pitot probes and AOA sensors. Make sure the pitot drain holes are operational and that the AOA sensors move freely.
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-13-00Page 579 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 34-13-00-865-102
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11 122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16 122VU ANTI ICE/PROBES/3/STATIC 5DA3 Z14 122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13
Subtask 34-13-00-860-093
C. Put the aircraft back to its initial configuration.
(1)
Do a reset of each ELAC:
- on the panel 49VU, open then close the ELAC1 C/B,
- on the panel 121VU, open then close the ELAC2 C/B.
(2)
Install the slip on covers on the static probes and on the pitot probes.
(3)
Make sure that the drain holes on the pitot probes are not blocked by unwanted materials. (Ref. TASK 34-11-15-200-001)
(4)
Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).
(5)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-13-00Page 580 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL
TASK 34-13-00-790-002
Leak Test of the Principal Static and Total Air Data System
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
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YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
CAUTION : OBEY THESE PRECAUTIONS WHEN YOU DO THE TEST TO PREVENT DAMAGE TO
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INSTRUMENTS:
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