Cirrus SR20

542 parts applicable to this airframe — ga_single

Part NumberStatus
003N0001-1PMA
003N0001-2PMA
01-0790901-51PMA
110-53-1000PMA
110-76-1001PMA
115-04599-01PMA
115-04600-00PMA
115-04604-00PMA
115-04605-00PMA
115-04606-00PMA
115-04607-00PMA
115-04617-00PMA
115-04618-00PMA
117-02416-00PMA
210128SRK-1PMA
210302-3PMA
210302-5PMA
220301-11PMA
220301-17PMA
508358-421PMA
508794-401PMA
508978-207PMA
509320-201PMA
700-00212-010PMA
700-00212-110PMA
96355-01PMA
AA116A10001-06PMA
AAD5-77-1PMA
AF11799-004PMA
DWG1029-031PMA
K12212-003PMA
K12216-002unknown
K12217-002PMA
K12221-004PMA
K12228-005PMA
K12228-006PMA
K12235-005PMA
K12235-006PMA
K12258-002PMA
K13099-001PMA
K13099-002PMA
K13104-002PMA
K13105-002PMA
LS03-01022PMA
LSM-500-082PMA
Model 600 WPPMA
RA066-10500OEM
RA066-10500-8KOEM
RA105-00200PMA
SS1001

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.