AD 2007-14-03

Airworthiness directive · Cirrus Airplane Parachute System (CAPS) · Cirrus Design SR20 and SR22

Effective
August 16, 2007
Published
July 12, 2007 · 72 FR 37999–38000
Issued
June 29, 2007
Models
SR20, SR22
Data sheet
TCDSA00009CH
Registered aircraft
5,649 matched by model
Product
Aircraft · Small airplane
Amendment
39-15125
Docket
FAA-2007-27976
Project
2007-CE-042-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document E7-13248. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

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).

The airworthiness directive

2007-14-03 Cirrus Design Corporation: Amendment 39-15125; Docket No. FAA-2007-27976; Directorate Identifier 2007-CE-042-AD.

(a) Effective Date

PDF page 1

(a) This AD becomes effective on August 16, 2007.

(b) Affected ADs

PDF page 1

(b) None.

(c) Applicability

PDF page 1

(c) This AD applies to Model SR20 airplanes, serial numbers (SN) 1005 through 1798, and Model SR22 airplanes, SN 0002 through 2437, that:

(1) Are certificated in any category; and

(2) have not incorporated the actions in their entirety of Cirrus Alert Service Bulletin No. SB A2X-95-10 R1, Issued April 2, 2007, Revised: April 10, 2007.

(d) Unsafe Condition

PDF page 1

(d) This AD results from a Cirrus Design Corporation (CDC) report of an in-flight Cirrus Airplane Parachute System (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).

(e) Compliance

PDF page 1

(e) To address this problem, you must do the following, unless already done:

ActionsComplianceProcedures
Replace the pick-up collar support of the CAPS with the new design pick-up collar support and the two nylon collar support screws with new custom aluminum tension screws. One of the following must do the replacement:Within the next 25 hours time-in-service (TIS) after August 16, 2007 (the effective date of this AD) or within 60 days after August 16, 2007 (the effective date of this AD), whichever occurs firstFollow Cirrus Alert Service Bulletin No. SB A2X-95-10 R2, Issued April 2, 2007, Revised: April 24, 2007.
(1) A CDC trained and authorized parachute system technician who also holds an Airframe and Powerplant (A&P) mechanic certificate; or
(2) A CDC trained and authorized parachute system technician who is supervised by an A&P mechanic.

(f) Alternative Methods of Compliance (AMOCs)

PDF page 1

(f) The Manager, Chicago Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Wess Rouse, Aerospace Engineer, FAA, 2300 East Devon Avenue, Room 107, Des Plaines, Illinois 60018; telephone: (847) 294-8113; fax: (847) 297-7834. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.

(g) Material Incorporated by Reference

PDF page 1

(g) You must use Cirrus Alert Service Bulletin No. SB A2X-95-10 R2, Issued April 2, 2007, Revised: April 24, 2007, or Cirrus Alert Service Bulletin No. SB A2X-95-10 R1, Issued April 2, 2007, Revised: April 10, 2007, to do the actions required by this AD, unless the AD specifies otherwise.

(1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) For service information identified in this AD, contact Cirrus Design Corporation, 4515 Taylor Circle, Duluth, Minnesota 55811; telephone: (218) 727-2737; Internet address: www.cirrusdesign.com.

(3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

This AD becomes effective on August 16, 2007.

On August 16, 2007, the Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD.

AddressesPage 1

For service information identified in this AD, contact Cirrus Design Corporation, 4515 Taylor Circle, Duluth, Minnesota 55811; telephone: (218) 727-2737; Internet address: http://www.cirrusdesign.com.

To view the AD docket, go to U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at http://dms.dot.gov. The docket number is FAA-2007-27976; Directorate Identifier 2007-CE-042-AD.

For further information contactPage 1

Wess Rouse, Aerospace Engineer, 2300 East Devon Avenue, Room 107, Des Plaines, Illinois 60018; telephone: (847) 294-8113; fax: (847) 297-7834.

DiscussionPage 1

On May 11, 2007, we issued a proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to certain CDC Models SR20 and SR22 airplanes. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on May 17, 2007 (72 FR 27766). The NPRM proposed to require you to replace the pick-up collar support and nylon screws, of the CAPS, with a new design pick-up collar support and custom tension screws.

CommentsPage 1

We provided the public the opportunity to participate in developing this AD. We received no comments on the proposal or on the determination of the cost to the public.

ConclusionPage 1

We have carefully reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed except for minor editorial corrections. We have determined that these minor corrections:

• Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and

• Do not add any additional burden upon the public than was already proposed in the NPRM.

Costs of CompliancePage 1

We estimate that this AD affects 2,677 airplanes in the U.S. registry.

We estimate the following costs to do the replacement of the pick-up collar support of the CAPS:

Labor costParts costTotal cost per airplaneTotal cost on U.S. operators
2 work-hours × $80 per hour = $160$17$177$473,829

Note:

CDC will provide warranty credit to the extent noted in Cirrus Alert Service Bulletin No. SB A2X-95-10 R2, Issued April 2, 2007, Revised: April 24, 2007.

Authority for This RulemakingPage 1

Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, Section 106 describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the agency's authority.

We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, “General requirements.” Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this AD.

Regulatory findingsPage 1

We have determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.

For the reasons discussed above, I certify that this AD:

1. Is not a “significant regulatory action” under Executive Order 12866;

2. Is not a “significant rule” under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and

3. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

We prepared a summary of the costs to comply with this AD (and other information as included in the Regulatory Evaluation) and placed it in the AD Docket. You may get a copy of this summary by sending a request to us at the address listed under ADDRESSES. Include “Docket No. FAA-2007-27976; Directorate Identifier 2007-CE-042-AD” in your request.

Adoption of the amendmentPage 1

Accordingly, under the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:

1. The authority citation for part 39 continues to read as follows:

2. FAA amends § 39.13 by adding the following new AD:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 5,649

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Cirrus Design5,649 aircraft
By year built
19992026
Registered aircraft by year built: 5,185 aircraft
19994
200048
2001124
2002274
2003298
2004394
2005409
2006475
2007428
2008320
2009113
2010103
201165
201256
201355
201478
2015112
2016105
2017121
2018126
2019135
2020128
2021155
2022180
2023196
2024230
2025283
2026170

464 with no year recorded

By model

Aircraft

See all 5,649 aircraft

NTSB investigations that cite this AD · 1

Their narratives or probable cause name AD 2007-14-03, often to say whether the aircraft complied with it.