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1 1 Config-1 May 01/05 1 1 1CES 1

 -----------------------------------------------------------------------
| LABEL | PARAMETER | SELF TEST VALUE | |----------------------------------------------------------------------| 120 | GPS PRES POS-LAT FRAC | N00.00. | | 121 | GPS PRES POS-LONG FRAC | E00.00. | | 130 | GPS INTEGRITY LIMIT | 8 | | 131 | HYBRID INTEGRITY LIMIT | 8 | | 132 | HYBRID TRUE HEADING | 10. | | 135 | HYBRID VERT FIGURE OF MERIT | 512 | | 136 | GPS VERT FIGURE OF MERIT | 512 | | 137 | HYBRID TRACK ANGLE TRUE-BNR | 00.0. | | 150 | UTC-BNR | 12:00:00 | | 165 | GPS VERT SPEED | -600 FT/MIN | | 166 | GPS N-S VELOCITY | 200 KTS | | 174 | GPS E-W VELOCITY | 200 KTS | | 175 | HYBRID GROUND SPEED-BNR | 200 KTS | | 247 | GPS HORIZ FIGURE OF MERIT | 1.0 | | 254 | HYBRID PRES POS-LAT | N22.50. | | 255 | HYBRID PRES POS-LONG | E22.50. | | 256 | HYBRID PRES POS-LAT FRAC | N00.00. | | 257 | HYBRID PRES POS-LONG FRAC | E00.00. | | 261 | HYBRID ALTITUDE | 10,000 FT | | 263 | HYBRID FLIGHT PATH ANGLE | -5.0. | | 264 | HYBRID HORIZ FIGURE OF MERIT | 1.0 | | 266 | HYBRID N-S VELOCITY | 200 KTS | | 267 | HYBRID E-W VELOCITY | 200 KTS | | 273 | GPS SENSOR STATUS | Not Applicable | | 274 | GPADIRS STATUS | Not Applicable | | 345 | HYBRID VERT SPEED | -600 FT/MIN | -----------------------------------------------------------------------
Table 6 : Binary Output Labels
 ----------------------------------------------------------------| | | SELF TEST VALUE | | LABEL | PARAMETER |--------------------------| | | | 0 to 2 s. | Over 2 s. | |--------------------------------------------------------------| | 010 | PRESENT POSITION LAT | 188.88.8' | N 22.30.0' | | 011 | PRESENT POSITION LONG | 188.88.8' | E 22.30.0' | | 012 | GROUND SPEED | 6888 Kts | 200 Kts | | 013 | TRACK ANGLE TRUE | 688.8. | 00.0. | | 014 | MAGNETIC HEADING | 688.8. | 15. | | 015 | WIND SPEED | 688 Kts | 100 Kts | | 016 | WIND DIRECTION TRUE | 688. | 30. | | 041 | SET LATITUDE | 188.88.8' | N 22.30.0' | | 042 | SET LONGITUDE | 188.88.8' | E 22.30.0' | | 043 | SET MAGNETIC HEADING | 688. | 15. |
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 60 1 1 Config-1 May 01/05 1 1 1CES 1

 ----------------------------------------------------------------| | | SELF TEST VALUE | | LABEL | PARAMETER |--------------------------| | | | 0 to 2 s. | Over 2 s. | |--------------------------------------------------------------| | 044 | TRUE HEADING | 688.8. | 10. | | 125 | GPS UTC | 78:88.8 | 12:00:00 | | 260 | GPS DATE | 38/18/88 | 01/01/88 | ----------------------------------------------------------------Table 8 : Output BCD Words
 (i)
 Ground Report
 (Ref. Fig. 043)

 (j)
 Current Status (Ref. Fig. 045) The Current Status function displays on 8 pages the state (as read by the computer) of the discrete inputs, digital inputs (Set Lat and Long from FMGC), power condition.

 (k)
 GPIRS REPORT (Ref. Fig. 046) The GPIRS Report function displays GPS primary (AIME) parameters which are stored either in case of GPS primary failure or routinely at the end of each flight (historic on several flights).

 (l)
 GPIRS HISTORY (Ref. Fig. 047) The GPIRS HISTORY function displays the number of events stored in memory and their accumulated durations.

 -CNT: Number of produced events (approximately 10).
 -HRS: Total event durations.
 C. Power-up Test Initialization and Cockpit Repercussions
 (1) Conditions of power-up test initialization
 -How long the computer must be de-energized: >20 s.
 -A/C configuration:
 -A/C on ground and OFF/NAV/ATT selector switch related to IR 1 (2)
 (3) (located on the ADIRS panel) set to OFF for 20 s at least then to NAV.
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 61 1 1 Config-1 May 01/05 1 1 1CES 1

 ADIRS BITE - IR Current Status
 Figure 045

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 GPIRS REPORT Figure 046 
R 1EFF : 1 1 1CES  001-049, 101-105, 151-199, 201-203,  1 111 Page 6334-18-00 Config-1 May 01/05

 ADIRS BITE - IR Main Menu 3/3
 Figure 047

R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-18-00Page 64 1 1 Config-1 May 01/05 1 1 1CES 1

 (2)
 Progress of power-up tests

 (a)
 Duration: 5 s

 (b)
 Cockpit repercussions directly linked to power-up test accomplishment (some other repercussions may occur depending on the A/C configuration but these can be disregarded):

 -ADIRS panel:
 -ON BAT legend annunciator on for 5 s, 2 s after power-up test initialization.

 (3)
　
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