AD 2024-24-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cirrus | Design Corporation | Airworthiness Directives; Cirrus Design Corporation Airplanes |
Unsafe Condition
Cracks in the upper power lever, which could result in loss of engine thrust control and reduced control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect (visual) the upper power lever for any crack(s) and depending on the results of any visual inspection, either inspect (fluorescent penetrant) or replace the upper power lever. Report all inspection results to the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before an upper power lever accumulates 1,200 hours time-in-service (TIS), within 10 hours TIS on the upper power lever after the effective date of this AD, or within 15 days after the effective date of this AD, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Model SR20, SR22, and SR22T airplanes, certificated in any category, that are equipped with upper power lever part number (P/N) 19181-001, 19181-002, or 46505-001.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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