Airworthiness Directive

AD 2007-14-03 72 FR 37999 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E7-13248
Amendment
39-15125
Published
2007-07-12
Effective
2007-08-16
Models covered
2
Last live check
2026-10-03
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AD

2007-14-03

FR doc E7-13248 · 72 FR 37999

AD 2007-14-03Published 2007-07-12Effective 2007-08-16

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 replace the pick-up collar support and nylon screws, of the Cirrus Airplane Parachute System (CAPS), with a new design pick-up collar support and custom tension screws.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to replace the pick-up collar support and nylon screws, of the Cirrus Airplane Parachute System (CAPS), with a new design pick-up collar support and custom tension screws. This AD results from a CDC report of an in-flight CAPS activation where the parachute failed to successfully deploy. We are issuing this AD to correct pick-up collar support fasteners of the CAPS, which could result in the premature separation of the collar. This condition, if not corrected, could result in the parachute failing to successfully deploy (CAPS failure).

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 2006-21-03 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... 2006-10-13

All Cirrus SR20 directives

Applies to 2 models in our index