Airworthiness Directive

AD 2005-17-19 70 FR 51999 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-16980
Amendment
39-14240
Published
2005-09-01
Effective
2005-10-13
Models covered
2
Last live check
2026-10-03
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AD

2005-17-19

FR doc 05-16980 · 70 FR 51999

AD 2005-17-19Published 2005-09-01Effective 2005-10-13

Superseded by 2006-19-10

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

The FAA adopts a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to measure and adjust the crew seat break-over bolts and to replace the crew seat recline locks on both crew seats. This AD results from CDC discovering that the crew seats, under emergency landing dynamic loads, may fold forward at less than the 26 g required by the regulations. 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

Applies to 2 models in our index