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Airworthiness Directive

AD 2002-24-08 67 FR 75809 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-30685
Amendment
39-12973
Published
2002-12-10
Effective
2003-01-24
Models covered
2
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2002-24-08 · 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

2002-24-08

FR doc 02-30685 · 67 FR 75809

AD 2002-24-08Published 2002-12-10Effective 2003-01-24

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 incorporate temporary operating limitations into the Limitation Section of the airplane flight manual (AFM) for certain affected airplanes and install a cable clamp external to the cone adapter on the Cirrus…

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 2002- 05-05, which currently applies to certain Cirrus Design Corporation (Cirrus) Models SR20 and SR22 airplanes. AD 2002-05-05 currently requires you to incorporate temporary operating limitations into the Limitation Section of the airplane flight manual (AFM) for certain affected airplanes and install a cable clamp external to the cone adapter on the Cirrus Airplane Parachute System (CAPS) activation cable for all affected airplanes. AD 2002-05-05 resulted from a report from the manufacturer that certain CAPS may not activate in an emergency situation. This AD is the result of the manufacturer redesigning the CAPS activation system. This AD requires you to modify the CAPS activation system. The actions specified by this AD are intended to prevent failure of the CAPS activation system in an emergency situation. Failure of this system could result in occupant injury and/ or loss of life and loss of aircraft.

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