Cirrus SR22

811 parts applicable to this airframe — ga_single

Part NumberStatus
1042367419REVHOEM
11315004PMA
11797008OEM
11799003COEM
11839002OEM
12018002OEM
1245200112452002OEM
12546003SOEM
12635004OEM
14059005OEM
14082004OEM
14571008OEM
15073001OEM
15080001OEM
15660001OEM
156E061OEM
15710002OEM
16546001OEM
20791OEM
226150026OEM
226150038OEM
246OEM
29556001OEM
3052OEM
317A386OEM
50207001unknown
505T081OEM
646426OEM
64990OEM
655911OEM
6559213A1OEM
656802OEM
656990OEM
6570681234OEM
6570686231OEM
658017OEM
BAPR84810NOEM
CS24ST5OEM
ETISR22100OEM
ETISR221002OEM
IO550NOEM
J111FCMANDDIODEOEM
MS178258OEM
MS210425OEM
PGAL11918OEM
R642085A17OEM
RA16402504PMA
S550014OEM
S6RSC25P10500556OEM
SR221033OEM

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.