- Airspeed (CAS) above 200Kts
NOTE : In case an operator wishes to monitor the AOA accuracy in
____ the flight enveloppe where the FACs compute the aircraft Weight (FL<150 and CAS<250Kts), a Level-off should be performed below the FL150 (ALT hold), with a stabilized Airspeed between 200 and 250Kts (SPD/MACH mode).
The analysis of the End-of-Flight AIDS printed report will allow the maintenance crews to clearly determine whether a given AOA sensor is healthy or not. The AIDS report represents a 30 seconds dynamic recording of the programmed parameters: This equals 60 snapshots or 120 lines of data.
(2) On the MCDU:
- on the MCDU MENU page, push the line key adjacent to the AIDS indication.
(a) On the AIDS page, push the line key adjacent to the PROGRAMMING indication.
(b) On the AIDS DMU PROGRAMMING page:
- enter your level 2 access code via the MCDU keyboard and push the 1L line key.
NOTE : If the password is correct, the number under the CUST item
____ changes from green to blue and the PASS indication comes into view in the MCDU scratchpad.
- push the line key adjacent to the PROGRAMMING MENUS indication.
(c) On the AIDS DMU PROGRAMMING page:
- push the line key adjacent to the CALL UP indication.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 211-299, 301-399, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 287
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Aircraft in Climb Phase
Figure 201/TASK 34-11-00-991-001
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 211-299, 301-399, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 288
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(d) On the AIDS CALL UP MODIFY page:
- push the line key adjacent to the ALPHA CALL UP indication to enter new Alpha call ups.
(e) On the AIDS ALPHA PROGRAM page:
- enter the parameters below:
--------------------------------------------------------------------------| Computer Parameter Name EQ/SYS/LAB/SDI | |------------------------------------------------------------------------| | FWC CORRECTED ANGLE OF ATTACK 26. 1 .241.11 | | THS STAB 6C. 1 .315.01 | | FAC WEIGHT (Kgs) 0A. 1 .074.00 | | FAC WEIGHT (Kgs) 0A. 2 .074.00 | --------------------------------------------------------------------------
1 AOA3 for CORRECTED ANGLE OF ATTACK NO.3 parameter (label 241
_
from FWC) ---------------------------------------------| AIDS ALPHA PROGRAM | | | | ALPHA EUC | | AOA3 0.04390 | | | | EQ SYS LAB SDI LSB BITS | | 26 1 241 11 17 12 | | | | EQ SYS LAB SDI | | 26 1 241 11 17 12 | | | | PRINT FORMAT | | INTEGER FRACTION SIGN | | DIGITS DIGITS (Y/N) | | 3 1 Y | ---------------------------------------------
2 THS for STAB parameter (label 315 from THS).
_
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 211-299, 301-399, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 289
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---------------------------------------------
| AIDS ALPHA PROGRAM | | | | ALPHA EUC | | STAB .0879 | | | | EQ SYS LAB SDI LSB BITS | | 6C 1 315 01 18 11 | | | | EQ SYS LAB SDI | | 6C 2 315 10 | | PRINT FORMAT | | INTEGER FRACTION SIGN | | DIGITS DIGITS (Y/N) | | 2 1 Y | ---------------------------------------------
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 211-299, 301-399, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 290
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3 GWF for WEIGHT (1bs) parameter (label 074 from FAC 1&2)
_ ---------------------------------------------| AIDS ALPHA PROGRAM | | | | ALPHA EUC | | GWF 18.16 | | | | EQ SYS LAB SDI LSB BITS | | 0A 1 074 00 14 15 | | | | EQ SYS LAB SDI | | 0A 2 074 00 | | PRINT FORMAT | | INTEGER FRACTION SIGN | | DIGITS DIGITS (Y/N) | | 5 0 N | ---------------------------------------------
(f) Push the line key adjacent to the RETURN indication to get the AIDS DMU PROGRAMMING page:
- push the line key adjacent to the TRIGGER CONDITIONS indication
- enter the parameters below:
--------------------------------------------------------------------------| Computer Parameter Name EQ/SYS/LAB/SDI | |------------------------------------------------------------------------| | ADIRU1 ROLL ANGLE 04. 1 .325.01 | | FMGCG DISCRETE STATUS 1 FMGC 01. 1 .274.00 | | FMGCG DISCRETE WORD ATS MODES 01. 1 .270.00 | | ADIRU1 COMPUTED AIRSPEED 06. 1 .206.01 | | SFCC1 SLAT AND FLAP SYSTEM STATUS 1B. 1 .046.01 | --------------------------------------------------------------------------
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本文链接地址：A320 Trouble Shooting Manual 排故手册 导航 NAVIGATION 1(35)
