Cirrus SR22

811 parts applicable to this airframe — ga_single

Part NumberStatus
011923461T30OEM
0512-00002-003OEM
068-01100OEM
100N21281OEM
10146008OEM
10357546OEM
11797006OEM
11799-002OEM
11799-003OEM
11799-004OEM
12634001OEM
127180518OEM
14082404OEM
1457300414572004OEM
15077-001OEM
15077-002OEM
15077-003OEM
16578001OEM
16600001OEM
22610004OEM
51377001OEM
633397OEM
642083A2OEM
656031OEM
657596OEM
70000006000OEM
AC-02470PMA
AC-02471PMA
AC-02474PMA
ALE13AOEM
ALE3045BSOEM
CR8017OEM
ETI621031OEM
ETISR221001OEM
FS167OEM
FUSEHOLDERCAPOEM
PN687181A24VVN11OEM
SA02511SESTC
SA02558CHOEM
SA02738CH (PAGE 1)OEM
SA02924CHSTC
SA04046CH Page 1OEM
SA04378CHOEM
SA04837NYOEM
SA12027IBSTC
SA12080BOSTC
SA12084BOSTC
SA12273IBSTC
SA5581SWOEM
TATI226850002OEM

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.