Cirrus SR22

811 parts applicable to this airframe — ga_single

Part NumberStatus
0110040110
10146005OEM
10281AOEM
10400615BOEM
10500556101OEM
11168002OEM
11169002OEM
11443004OEM
11443005OEM
116118001OEM
11626002
11898002PMA
12545001OEM
12635002
13431004OEM
13432002OEM
13909002PMA
14059001PMA
14522191015OEM
14522191017OEM
14571003OEM
14571004OEM
14572002OEM
14573002OEM
14605001OEM
14605010OEM
14610002OEM
14836001OEM
15070001
15074001OEM
16615001
18583002OEM
20139001OEM
51020001unknown
51381001OEM
642083OEM
642083A10
649OEM
6521718OEM
653387788OEM
653888OEM
654585
6566161OEM
657046OEM
70000004002OEM
A20742OEM
BA24OEM
BC4101OEM
MCU120OEM
MS24775222OEM

Airworthiness Directive activity

FAA / EASA public regulatory data

1airworthiness directives affecting this fleet — recurring compliance demand for the parts and shops that serve it
Most recent
  • FAA AD 2024-24-11effective Dec 23, 2024Mixed actions

    The FAA is adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (Cirrus) Model SR20, SR22, and SR22T airplanes. This AD was prompted by a report of failure of the upper power lever. This AD requires repetitively inspecting (visual) the upper power lever for any crack(s) and depending on the results of any visual inspection, either inspecting (fluorescent penetrant) or replacing the upper power lever. This AD also requires reporting all inspection results to the FAA. The FAA is issuing this AD to address the unsafe condition on these products.

Directives linked to this airframe family in the FAA / EASA regulatory corpus we have processed — not a complete historical AD list. An AD is a compliance requirement that drives scheduled work (inspections, replacements, modifications) across the fleet; inspection directives are not replacement directives, and none of this is a prediction that any part will fail.