Cirrus SR22

811 parts applicable to this airframe — ga_single

Part NumberStatus
011923461TOEM
0923080
105005561OEM
11796002OEM
12635001OEM
12739001OEM
12980001OEM
13431003OEM
13549002OEM
135600025
13594002OEM
14251001OEM
14880001
151415001OEM
15222004OEM
16678001OEM
220045510
226850002OEM
302013400OEM
430OEM
4663040003OEM
5217003OEM
6420831A2OEM
645843
646404OEM
646421OEM
646717OEM
649304ROEM
649900
6533538A1OEM
6533538A1EOEM
654084OEM
655465A5OEM
655932A3OEM
656181OEM
656991OEM
657199EOEM
6576682234OEM
658178A2BPOEM
7000006000OEM
AB357586OEM
C28150OEM
C4BOEM
ETISR221004OEM
ETISR22212OEM
G156006OEM
NAS514P4407POEM
P2070009520
S00202OEM
TR20OEM

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.