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Airworthiness Directive

AD 2024-24-11 89 FR 96863 Active

Federal Aviation Administration · 14 CFR part 39

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.

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FR document
2024-28552
Amendment
39-22902
Published
2024-12-06
Effective
2024-12-23
Models covered
2

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2024-24-11 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2024-24-11

FR doc 2024-28552 · 89 FR 96863

AD 2024-24-11Published 2024-12-06Effective 2024-12-23

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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.

Full official abstract

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.

More directives for Cirrus SR20

  1. AD 2008-14-13 Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 ... Effective 2008-08-14
  2. AD 2008-11-18 Airworthiness Directives; Cirrus Design Corporation Model SR20 Airplanes Effective 2008-07-07
  3. AD 2008-03-16 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... Effective 2008-03-11
  4. AD 2007-14-03 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... Effective 2007-08-16
  5. AD 2006-21-03 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... Effective 2006-11-17

All Cirrus SR20 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 2 models in our index