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3FP1  SENSOR-ANGLE OF ATTACK, 1  127  824  34-11-19
 3FP2  SENSOR-ANGLE OF ATTACK, 2  128  824  34-11-19
 3FP3  SENSOR-ANGLE OF ATTACK, 3  127  824  34-11-19
 11FP1  SENSOR-TAT, 1  121  34-11-18
 11FP2  SENSOR-TAT, 2  122  34-11-18
 9DA1  PROBE-PITOT, 1  125  812  34-11-15
 9DA2  PROBE-PITOT, 2  126  822  34-11-15
 9DA3  PROBE-PITOT, 3  125  812  34-11-15
 7DA1  PROBE-L STATIC, 1  127  824  34-11-16
 7DA2  PROBE-L STATIC, 2  127  824  34-11-16
 7DA3  PROBE-L STATIC, 3  121  811  34-11-16
 8DA1  PROBE-R STATIC, 1  128  824  34-11-16
 8DA2  PROBE-R STATIC, 2  128  824  34-11-16
 8DA3  PROBE-R STATIC, 3  122  811  34-11-16
 19FP1  ADM-L TOTAL PRESSURE  NONE 125  812  34-11-17
 19FP2  ADM-R TOTAL PRESSURE  126  822  34-11-17
 19FP3  ADM-STBY TOTAL PRESSURE  125  812  34-11-17
 19FP4  ADM-R STATIC PRESSURE  128  824  34-11-17
 19FP5  ADM-L STATIC PRESSURE  127  824  34-11-17
 19FP6  ADM-R STATIC PRESSURE  128  824  34-11-17
 19FP7  ADM-L STATIC PRESSURE  127  824  34-11-17
 19FP8  ADM-STBY STATIC PRESSURE  121  811  34-11-17 

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1401-499,  1 Config-3 Aug 01/05
 1  1
 1CES  1

 

 3. System Description
__________________
 A. Reporting Function Each ADIRS BITE message is described in the following pages, with the corresponding fault description and the consequences on the system and in the cockpit.
 (1)
 General

 -IR and ADR faults are classified as follows: . class 1: faults with cockpit effect . class 2: non-critical faults . class 3: minor faults without cockpit effects.
 -use of indexes in BITE messages: ADIRUi stands for ADIRU 1, ADIRU 2 or ADIRU 3.
 -ECAM messages: . xxx stands for CAPT or F/O, depending on the ADIRU side (1 or 2) . the letter in parentheses indicates the color used to display the text: (A) Amber, (C) Cyan and (W) White.
 -IR FAULT: the FAULT legend of the IR pushbutton switch flashes in NAV mode and is steady in ATT mode.

 (2)
 Inertial reference faults
 (Ref. Fig. 002, 003, 004, 005, 006, 007, 008)

 

 **ON A/C 204-228,
R
 (Ref. Fig. 008A)

R **ON A/C 051-099, 106-149, 204-299, 301-399, 401-499,
 (Ref. Fig. 009)
 Some IR faults resulting in warnings (fault annunciation, invalid
 outputs) are due to an incorrect operational use of the system and
 not to a system fault.
 These tests are:

 -align in air
 -position-entry (comparison with the last stored position and computed latitude).
 -Test on motion.
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 ADIRS BITE - Inertial Reference System - Class 1 Internal Faults 1/5
 Figure 002

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 ADIRS BITE - Inertial Reference System - Class 1 Internal Faults 2/5
 Figure 003

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 ADIRS BITE - Inertial Reference System - Class 1 Internal Faults 3/5
 Figure 004

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 ADIRS BITE - Inertial Reference System - Class 1 Internal Faults 4/5
 Figure 005

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 ADIRS BITE - Inertial Reference System - Class 1 Internal Faults 5/5
 Figure 006

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 ADIRS BITE - Inertial Reference System - Class 1 External Faults
 Figure 007

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 ADIRS BITE - Inertial Reference System - Class 3 Faults
 Figure 008

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