Cirrus SR20

542 parts applicable to this airframe — ga_single

Part NumberStatus
0700-00001-001PMA
12212-003OEM
12216-002OEM
12217-002OEM
12221-004OEM
12228-005OEM
12228-006OEM
12235-005OEM
12235-006OEM
12258-002OEM
13099-001OEM
13099-002OEM
13104-002OEM
13105-002OEM
18050-2B8OEM
24737-007OEM
24737-010OEM
Dukes Inc. 5217-00-3OEM
KAT-14-003PMA
Lord J-9613-58PMA
NCK-05-001PMA
RA-B3-5-1PMA
RA-D9-18-1 Cont.PMA
RA1K31-4-6-4OEM
RA1K8-6-10PMA
SA593CHOEM
TSF3165PMA
W-2268-II-RHPMA
W-2399PMA
W-2400-LHPMA
W-2400-RHPMA
W/B-2267-RHPMA
W/B-2268-II-LHPMA
W/B-2399PMA
W/B-2400-LHPMA
W/B-2400-RHPMA
W/G-2268-RHPMA
W/G-2399PMA
W/G-2400-2064-LHPMA
W/G-2400-2064-RHPMA
W/G-2400-2538-LHPMA
W/G-2400-2538-RHPMA
W/G-2400-LHPMA
W/G-2400-RHPMA
W/T-2399PMA
W/T-2400-LHPMA
W/T-2400-RHPMA
W/XT-2268-LHPMA
W/XT-2400-LHPMA
W/XT-2400-RHPMA

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.