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1401-499, 1 Config-3 Aug 01/05
1 1
1CES 1
----------------------------------------------------------------| LABEL | PARAMETER | SELF TEST VALUE | |--------------------------------------------------------------| | 315 | WIND SPEED | 100 Kts | | 316 | WIND DIRECTION-TRUE | 30. | | 317 | TRACK ANGLE-MAG | 5. | | 320 | MAGNETIC HEADING | 15. | | 321 | DRIFT ANGLE | -10. (Left) | | 322 | FLIGHT PATH ANGLE | -5. | | 323 | FLIGHT PATH ACCEL | 0.02g | | 324 | PITCH ANGLE | 5. | | 325 | ROLL ANGLE | 45. (Right) | | 326 | BODY AXIS PITCH RATE | 10./s | | 327 | BODY AXIS ROLL RATE | 10./s | | 330 | BODY AXIS YAW RATE | 10./s | | 331 | BODY LONGIT ACCEL | 0.02g | | 332 | BODY LATERAL ACCEL | 0.10g | | 333 | BODY NORMAL ACCEL | 0.10g | | 334 | PLATFORM HEADING | 22.50. | | 335 | TRACK ANGLE RATE | 4.0./s | | 336 | PITCH ATT RATE | 10./s | | 337 | ROLL ATT RATE | 10./s | | 340 | TRACK ANGLE GRID | 10. | | 341 | GRID HEADING | 20. | | 343 | DESTINATION HIL | 1.0 NM | | 345 | HYBRID VERTICAL VELOCITY| -600 ft/mn | | 347 | ALT WAYPOINT HIL | 2.0 NM | | 360 | POTENTIAL VERT SPEED | -600 ft/mn | | 361 | INERTIAL ALTITUDE | 10,000 ft | | 362 | ALONG TRACK HORIZ ACCEL | 0.02g | | 363 | CROSS TRACK HORIZ ACCEL | 0.02g | | 364 | VERTICAL ACCEL | 0.1g | | 365 | INERTIAL VERT SPEED | -600 ft/mn | | 366 | N-S VELOCITY | 200 Kts (N) | | 367 | E-W VELOCITY | 200 Kts (E) | ----------------------------------------------------------------
Table 3 : Binary Output Labels
(i)
GROUND REPORT (Ref. Fig. 024) This item reports all internal faults detected since the last landing.
(j)
INPUT STATUS (Ref. Fig. 025) This item describes the current state/value of the selected IR inputs (discrete and binary inputs).
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ADIRS BITE - IR Main Menu 6/7
Figure 024
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ADIRS BITE - IR Main Menu 7/7
Figure 025
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(3) ADR interactive function
(a)
LAST LEG REPORT
(Ref. Fig. 026)
This item describes the in-flight class 1 and 2 fault status of
the selected ADR and related LRUs during the last leg (flight leg
00).
(b)
PREVIOUS LEGS REPORT
(Ref. Fig. 026)
This item describes the in-flight class 1 and 2 fault status of
the selected ADR and related LRUs during the previous legs
(flight legs 01-62).
(c)
LRU IDENTIFICATION (Ref. Fig. 027) This item describes the Part Number and Serial Number of the selected ADIRU, as well as the Part Number of the ADMs.
(d)
GROUND SCANNING (Ref. Fig. 027) This item describes the current on-the-ground fault status of the selected ADR.
(e)
TROUBLE SHOOTING DATA (Ref. Fig. 028) This item provides, for each fault message stored in the LAST LEG or PREVIOUS LEGS REPORT, additional data required by the maintenance for failure investigation.
(f)
CLASS 3 FAULTS (Ref. Fig. 028) This item reports all class 3 faults recorded since the last takeoff.
(g)
SYSTEM TEST
(Ref. Fig. 028)
This item activates a complete test of the ADR system and
presents a report to the user.
(h)
INTERFACE TEST (OUTPUT TESTS MENU)
(Ref. Fig. 029, 030)
This item controls the functional test modes of the selected ADR.
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ADIRS BITE - ADR Main Menu 1/8
Figure 026
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ADIRS BITE - ADR Main Menu 2/8
Figure 027
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ADIRS BITE - ADR Main Menu 3/8
Figure 028
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ADIRS BITE - ADR Main Menu 4/8
Figure 029
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ADIRS BITE - ADR Main Menu 5/8
Figure 030
R 1EFF : 051-099, 106-149, 204-299, 301-399, 1 34-18-00Page 45 1401-499, 1Config-3 Aug 01/05 1 1 1CES 1 The text displayed describes the various steps of the interface test; when you push the line key adjacent to the START TEST indication, the following test sequence is run: 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護(hù)手冊 AMM NAVIGATION 導(dǎo)航2(94)
