Cirrus SR20

542 parts applicable to this airframe — ga_single

Part NumberStatus
0025-5200PMA
0116-00004-001PMA
0116-00006-001PMA
0134-00002-001PMA
0212-00001-001PMA
0242-00001-002PMA
0512-00001-001PMA
0512-00001-002PMA
0512-00001-003PMA
0512-00003-003PMA
0512-00003-004PMA
0512-00006-001PMA
0512-00006-002PMA
0512-00013-001PMA
07010003OEM
0720-00001-001PMA
0720-00001-002PMA
0720-00001-003PMA
0720-00001-004PMA
0720-00001-005PMA
0720-00001-006PMA
10351002
110-76-1000PMA
11799002BOEM
11907004
11907005
12446105OEM
12744001OEM
5049074058013OEM
646880
654358OEM
AK-950PMA
AK-950-F1PMA
AK-950-F2PMA
AK-950-F3PMA
AK-950-F4PMA
AK-950-F5PMA
AK-950-FTRPMA
AK-950-FTR1PMA
C24ST3OEM
ES4024LPOEM
H50002OEM
K-1001PMA
S4024LPOEM
TASF3165PMA
W/B-2269PMA
W/G-2268-II-2064-LHPMA
W/G-2269-2064PMA
W/T-2268-II-RHPMA
W/T-2268-LHPMA

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.