FCTM ADIRS/IRS FAULT Flashcards
Each ADIRS has two parts (ADR and IRS), that may fail:
Independently of each other.
Additionally the IRS part may fail totally or may be available in ATT mode.
Single NAV ADR FAULT or NAV IRS FAULT are simple procedures, and only require action on the:
switching panel as indicated by the ECAM.
Dual NAV ADR or NAV IRS failures will cause the loss of:
AP, A/THR and flight controls revert to ALTN law.
Due to the low probability of a triple ADR failure, the associated procedure will not be displayed on the ECAM. In this case, the crew will refer to:
QRH procedure for ADR 1 + 2 + 3 failure.
There is no procedure for IRS 1 + 2 + 3 failure but the ECAM status page will give approach procedure and inoperative systems. In this unlikely event, the standby instruments are the only attitude, altitude, speed and heading references.
In the case of a triple ADR failure, AP and A/THR are lost and the flight controls revert to ALTN law. The NAV ADR 1+2+3 FAULT warning is triggered and the:
ECAM procedure requires that the 3 ADRs be switched OFF, to replace the PFD’s normal speed scale and altitude indication by the Back-Up Speed Scale (BUSS) and GPS altitude information.
There is no procedure for IRS 1 + 2 + 3 failure but the ECAM status page will give approach procedure and inoperative systems. In this unlikely event, the standby instruments are the only attitude, altitude, speed and heading references
To switch off an ADR, the flight crew must use the:
ADR pb. Do not use the rotary selector, because this would also cut off the electrical supply to the IR part.