(3)
Do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).
(4)
On the SWITCHING panel 8VU, make sure that the AIR DATA selector switch is at NORM.
(5)
Make sure that the flaps are fully retracted (Ref. TASK 27-50-00-866-009).
(6)
On the FCU, set the CAPT (F/O) Baro-Correction to display STD below the altitude scale on the CAPT (F/O) PFD .
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-13-00Page 554 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 34-13-00-865-101
B. Open, safety and tag 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 34-13-00-480-052
C. Install the Ground Pressure Generator
NOTE : For this test, use a ground pressure generator with these minimum
____
requirements: R - Static (altitude): -1000ft to 50,000ft (accuracy +/-0,31mb R (0.00453psi)),
-Pitot (speed) : 0 to 500Kts,
-Mach Nbr : 0 to 1.000,
-Climb Rate : 0 to +/- 6000ft/mn (accuracy +/- 7%).
(1) Remove the slip on covers from the static probes and the pitot probes.
R (2) Connect the GENERATOR - GROUND PRESSURE MINI. 100 MB (1.45 PSI) TO R 1400 MB (20.3 PSI) to the static and pitot probes of the aircraft:
For CAPT circuit (ADIRU 1) and F/O circuit (ADIRU 2), connect the ground pressure generator to the static probes with the ADAPTER COVER-STATIC PORT (98D34003500102):
-
L static probe 1 7DA1, zone 127, STA 8750, for the L static pressure ADM (19FP5)
-
L static probe 2 7DA2, zone 127, STA 8700, for the L static
pressure ADM (19FP7)
and
-
R static probe 1 8DA1, zone 128, STA 9300, for the R static pressure ADM (19FP4)
-
R static probe 2 8DA2, zone 128, STA 9350, for the R static pressure ADM (19FP6)
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-13-00Page 555 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 For the standby circuit (ADIRU 3), connect the ground pressure generator to the static probes with the ADAPTER COVER-STATIC PORT (98D34003500100):
-L static probe 3 7DA3, zone 121, STA 4250, for the static pressure ADM (19FP8) or
-R static probe 3 8DA3, zone 122, STA 4250, for the static pressure ADM (19FP8).
Connect the ground pressure generator to the pitot probes with the
ADAPTOR-CHARGING,PITOT PROBE or equivalent:
For CAPT circuit:
-
pitot probe 1 9DA1, zone 125, for the L total pressure ADM (19FP1).
For F/O circuit:
-
pitot probe 2 9DA2, zone 126, for the R total pressure ADM (19FP2).
For the standby circuit:
-
pitot probe 3 9DA3, zone 125, for the standby total pressure ADM (19FP3).
(3) Seal the drain holes of the pitot probes with colored adhesive tape.
CAUTION : WHEN YOU SEAL THE DRAIN HOLE IN THE PITOT PROBE, DO NOT
_______ SEAL THE HOLE DIRECTLY WITH THE COLORED ADHESIVE TAPE. ALWAYS PUT A PIECE OF PLASTIC ON THE HOLE AND USE THE TAPE TO ATTACH THE PLASTIC. IF YOU SEAL THE DRAIN HOLE DIRECTLY WITH THE ADHESIVE TAPE, THERE IS A RISK THAT SOME OF THE ADHESIVE WILL STAY ON THE HOLE AND COLLECT PARTICLES. THIS CAN SUBSEQUENTLY CAUSE BLOCKAGE OF THE HOLE AND THUS INCORRECT OPERATION OF THE PROBE.
(a) Seal the opposite static probe of the standby ADM with the ADAPTER COVER-STATIC PORT (98D34003500103).
(4)
Move the vane of the three AOA sensors to the upper position. Keep the AOA sensors in position with colored adhesive tape.
(5)
Start the ground pressure generator.
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-13-00Page 556 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
4. Procedure
_________
**ON A/C 106-149, 210-299,
Subtask 34-13-00-720-063-B
A. Functional Test of the Altitude and Airspeed Data
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
On the ground pressure generator, set a static pressure and a total pressure as given in the tables below.
2.
On the SWITCHING panel 8VU:
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 NAVIGATION 导航1(166)