Windshield heat for pf is non fmgs monitored required equipment for cat2/3 landings — see eqrh ops. Other than that, there is no immediate operational eﬀect.
[ anti ice l(r)(l+r) windshield(window), fcom pro.aep.a-ice ]
The issue with loss of anti-ice on more than one pitot probe is that it is possible that the two unprotected pitot probes will ice up at the same time and provide erroneous but coherent data. This leads to a situation where the adr associated with the remaining protected probe is locked out despite being the single correct source.
Obviously, the ﬁrst thing to do is to avoid icing conditions.
If there is a working adr connected to a protected probe, turn one of the adrs associated with an unprotected probe oﬀ. This ensures that an adr disagree ecam caution is triggered by signiﬁcant speed discrepancies and ensures that the protected adr will not be automatically deselected.
If pitot heat is lost on all probes, one of the adrs should, again, be turned oﬀ to ensure the adr disagree ecam caution is provided. If icing is expected, turn oﬀ a second adr and be ready to apply unreliable airspeed procedures (see Section 2.3).
[ anti ice all(capt(f/o)+f/o(stby)) pitot, fcom pro.aep.a-ice ]
The adr associated with the failed probe or port should be considered unreliable. adr1 or adr2 can be replaced with adr3 using air data switching. If using standby instruments with adr3 unreliable, air data information must be monitored closely.
[ anti ice capt(f/o)(stby) pitot(l(r) stat), fcom pro.aep.a-ice ]
If two aoa probes are aﬀected by icing, the computers may erroneously deselect the remaining good adr. Switching oﬀ one of the aﬀected adrs leaves the system in the state described in Section 11.6.
[ qrh aep.a-ice, fcom pro.aep.a-ice ]
No immediate operational eﬀect.
[ anti ice capt(f/o)(stby) aoa(tat), fcom pro.aep.a-ice ]
If applicable, deselect the aﬀected ADR.
[ anti ice capt(f/o)(stby) probes, fcom pro.aep.a-ice ]
If a valve fails to open when commanded, avoid icing conditions. If it fails to close when commanded, a thrust limit penalty applies.
[ anti ice eng 1(2) valve open(clsd), fcom pro.aep.a-ice ]
If a wing anti-ice valve is open when commanded closed:
If a wing anti-ice valve is closed when commanded open, the wing anti-ice must be turned oﬀ to avoid asymmetrically de-icing the wings. Avoid icing conditions. If ice accretion does occur, landing distances and VAPP adjustments are in qrh and speed must be maintained above either VLS + 10kt or Green Dot.
[ wing anti ice sys fault, fcom pro.aep.a-ice, fcom pro.nor.sup.aw ]