Cirrus SR22

811 parts applicable to this airframe — ga_single

Part NumberStatus
066-001PMA
1743570-08PMA
1743570-09PMA
1743570-14PMA
1743570-16PMA
1763768PMA
1763768-02PMA
1763770PMA
1763770-02PMA
22-5880001PMA
509300-202PMA
509300-203PMA
756500052PMA
9060-17000-01 (straight RF)PMA
9060-17000-02 (right angle RF)PMA
9060-17250-01PMA
9060-17500-01PMA
9060-17500-02 (right angle RF)PMA
9100-001-APMA
9100-001-DPMA
9200-000-APMA
9200000BOEM
APV-1.50-16-1PMA
APV-1.50-16-2PMA
APV-1.50-16-3PMA
APV-1.50-16-4PMA
APV-1.50-WAS-ZZZPMA
APV-SA1-4PMA
APV-SA1-5PMA
APV-SA1-5BPMA
APV-SA1-6PMA
APV-SA1-6BPMA
APV-SA2-1PMA
APV-SA2-1BPMA
APV-SA2-2PMA
APV-SA2-3PMA
DA15077-001PMA
DA15077-003PMA
K12212-003PMA
K12221-004PMA
K12228-005PMA
K12235-006PMA
K12258-002PMA
K13104-002PMA
K13105-002PMA
LS03-01022PMA
LSM-500-095PMA
LSM-500-122PMA
SS1001
SS1002OEM

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.