------------------------------------------------------
(k) Push the line key adjacent to the RETURN indication to get the AIDS PRINT REPORT page:
- push the line key adjacent to the INDIVIDUAL REP PROG indication.
(l) On the AIDS INDIV REP PROG page:
- enter the report number 16
- push the line key adjacent to the HEADER indication
- on the AIDS REPORT HEADER page, push the line key adjacent to the title of the report as shown below:
------------------------------------------------------| AIDS REPORT HEADER | | | | REPORT | | 16 | | | | 12345678901234567890 | | | | L1 IN FLIGHT AOA | | MONITORING | | L2 | | | | L3 | | | ------------------------------------------------------
(m) Push the line key adjacent to the RETURN indication to get the AIDS INDIV REP PROG page:
- push the line key adjacent to the START LOGIC 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 A200
401-499, Aug 01/05 CES (n) On the AIDS REP START LOGIC page:
- enter the conditions below: ------------------------------------------------------
| AIDS REP START LOGIC |
| |
| REPORT |
| 16 |
| |
| 1.AND.2.AND.3.AND.4.AND.5.AND.6. |
| |
| |
| |
------------------------------------------------------
(o) Push the line key adjacent to the RETURN indication to get the AIDS INDIV REP PROG page:
- push the line key adjacent to the INHIB indication.
(p) On the AIDS REP NUM INHIBIT page:
- enter the data below: ---------------------------------------------| AIDS REP NUM INHIBIT | | | | REPORT | | 16 | | | | MAX GENERATED | | 1 --| | STORED | | 1 --| | PRINTED | | 1 --| | LINKED | | 0 --| | | ---------------------------------------------
(q) When the report programming is completed, push the MCDU MENU mode key to get the MCDU MENU page and do the report analysis (Ref. Para. (2)).
NOTE : The AIDS TIME OUT message comes into view on the MCDU.
____ The DMU is fully operational again after approximately 45 seconds.
「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 A201
401-499, Aug 01/05 CES
(3) Report analysis
(a) Relation between the Pitch Angle, the FPA (Flight Path Angle) and the AOAref (Reference Angle of Attack). (Ref. Fig. 201/TASK 34-11-00-991-001) The following page depicts an instance of AIDS report, and provides instructions on how to analyse the recorded parameters. (Ref. Fig. 202/TASK 34-11-00-991-002)
(b) Conclusion Remove the Angle of Attack sensor that exceeds these tolerances (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
1_ On the printout of report No16, select an area of 24 lines in
row (12 snapshots) where the following conditions are met:
. Total Altitude variation not exceeding 20 feet versus
initial value
. Total Roll Angle variation not exceeding 1 deg. versus
initial value
. No abrupt AOA change between 2 snapshots (0.2 deg. max.)
2_ In stabilized flight conditions the relation is:
AOA ref = PITCH - FPA
For the 12 selected snapshots in the report, calculate AOAref.
3_ For each snapshot compare the AOAref with the 3 AOA values
(AOA1, AOA2, AOA3) and make sure that the difference does not
exceed the following tolerances:
. (AOA1 - AOAref) is less than or equal plus or minus 0.5 deg.
. (AOA2 - AOAref) is less than or equal plus or minus 0.5 deg.
. (AOA3 - AOAref) is less than or equal plus or minus 0.5 deg.
「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 A202
401-499, Aug 01/05 CES
In Flight Angle of Attack Sensor Monitoring - Progammable Report - Example Figure 202/TASK 34-11-00-991-002
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