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Airworthiness Directive

AD 2006-19-10 71 FR 54755 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E6-15432
Amendment
39-14767
Published
2006-09-19
Effective
2006-10-24
Models covered
2
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2006-19-10 · 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

2006-19-10

FR doc E6-15432 · 71 FR 54755

AD 2006-19-10Published 2006-09-19Effective 2006-10-24

Supersedes 2005-17-19

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 you to measure and adjust the crew seat break-over bolts and to replace the crew seat recline locks on both crew seats.

Full official abstract

We are adopting a new airworthiness directive (AD) that supersedes AD 2005-17-19, which applies to certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. AD 2005-17-19 currently requires you to measure and adjust the crew seat break-over bolts and to replace the crew seat recline locks on both crew seats. Since we issued AD 2005-17-19, CDC developed new crew seat break-over pins to replace the old crew seat break-over bolts. Consequently, this AD retains the action from AD 2005-17-19 of replacing the crew seat recline locks on both seats and adds the action of replacing the crew seat break-over bolts with the new crew seat break-over pins on both seats. We are issuing this AD to prevent the crew seats from folding forward during emergency landing dynamic loads with consequent occupant injury.

More directives for Cirrus SR20

  1. AD 2024-24-11 Airworthiness Directives; Cirrus Design Corporation Airplanes 2024-12-06
  2. AD 2008-14-13 Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 ... 2008-07-10
  3. AD 2008-11-18 Airworthiness Directives; Cirrus Design Corporation Model SR20 Airplanes 2008-06-02
  4. AD 2008-03-16 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... 2008-02-05
  5. AD 2007-14-03 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... 2007-07-12

All Cirrus SR20 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 2 models in our index