AD 2008-02-18

Airworthiness directive · Pick-up collar support and nylon screws · BRS-172 parachute recovery system (Ballistic Recovery Systems STC SA01679CH or SA01999CH)

Effective
February 28, 2008
Published
January 24, 2008 · 73 FR 4051–4053
Issued
January 16, 2008
Models
172, 172A, 172B, 172C, 172D, 172E and 28 more
Registered aircraft
30,787 matched by model
Product
Aircraft · Small airplane
Amendment
39-15348
Docket
FAA-2007-29317
Project
2007-CE-079-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document E8-1130. 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 Cessna Aircraft Company 172 series airplanes with the BRS-172 Parachute System installed via Supplemental Type Certificate (STC) No. SA01679CH and Cessna Aircraft Company 182 series airplanes that are equipped with the BRS-182 Parachute System installed via STC No. SA01999CH. This AD requires you to replace the pick-up collar support and nylon screws for the BRS-172 and BRS-182 Parachute System. This AD results from notification by Ballistic Recovery Systems, Inc. (BRS) that the pick-up collar assembly may prematurely move off the launch tube and adversely affect rocket trajectory during deployment. We are issuing this AD to prevent premature separation of the collar, which could result in the parachute failing to successfully deploy.

The airworthiness directive

2008-02-18 Cessna Aircraft Company: Amendment 39-15348; Docket No. FAA-2007-29317; Directorate Identifier 2007-CE-079-AD.

(a) Effective Date

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(a) This AD becomes effective on February 28, 2008.

(b) Affected ADs

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(b) None.

(c) Applicability

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(c) This AD applies to the following airplane models, all serial numbers, certificated in any category, that are equipped with:

(1) BRS-172 Parachute System installed via Supplemental Type Certificate (STC) No. SA01679CH, or

(2) BRS-182 Parachute System installed via STC No. SA01999CH.

Cessna 172 modelsCessna 182 models
172182G
172A182H
172B182J
172C182K
172D182L
172E182M
172F (USAF T-41A)182N
172G182P
172H (USAF T-41A)182Q
172I182R
172K182S
172L182T
172MT182
172NT182T
172P
172Q
172R
172S
R172J
R172K

(d) Unsafe Condition

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(d) This AD results from notification by Ballistic Recovery Systems, Inc. (BRS) that the pick-up collar assembly may prematurely move off the launch tube and adversely affect rocket trajectory during deployment. We are issuing this AD to prevent premature separation of the collar. This condition could result in the parachute failing to successfully deploy.

(e) Compliance

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

—
ActionsComplianceProcedures
Remove and replace the pick-up collar support and two retaining screwsWithin the next 25 hours time-in-service after February 28, 2008 (the effective date of this AD)(i) For Cessna 172 series airplanes follow BRS SB 07-01, dated June 8, 2007. (ii) For Cessna 182 series airplanes, follow BRS SB 07-02, dated June 8, 2007.

(f) Alternative Methods of Compliance (AMOCs)

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(f) The Manager, Chicago Aircraft Certification Office, 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: Gregory Michalik, Senior Aerospace Engineer, FAA, 2300 East Devon Avenue, Des Plaines, Illinois, 60018; telephone: (847) 294-7135; fax: (847) 294-7834; e-mail: gregory.michalik@faa.gov. 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

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(g) You must use Ballistic Recovery Systems, Inc. Service Bulletin No. 07-01, dated June 8, 2007, for Cessna 172 series airplanes; or Ballistic Recovery Systems, Inc. Service Bulletin No. 07-02, dated June 8, 2007, for Cessna 182 series airplanes; 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 Ballistic Recovery Systems, Inc., 300 Airport Road, South Saint Paul, MN 55075-3551; telephone: (651) 457-7491; fax: (651) 457-8651.

(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 February 28, 2008.

On February 28, 2008, 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 Ballistic Recovery Systems, Inc., 300 Airport Road, South Saint Paul, MN 55075-3551; telephone: (651) 457-7491; fax: (651) 457-8651.

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://www.regulations.gov. The docket number is FAA-2007-29317; Directorate Identifier 2007-CE-079-AD.

For further information contactPage 1

Gregory Michalik, Senior Aerospace Engineer, 2300 East Devon Avenue, Room 107, Des Plaines, Illinois 60018; telephone: (847) 294-7135; fax: (847) 294-7834.

DiscussionPage 2

On November 2, 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 Cessna Aircraft Company 172 and 182 series airplanes that are equipped with the BRS-172 and BRS-182 Parachute System. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on November 2, 2007 (72 FR 62143). The NPRM proposed to require the replacement of the pick-up collar support and screws for the BRS-172 and BRS-182 Parachute System.

CommentsPage 2

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 2

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 2

We estimate that this AD affects 54 airplanes in the U.S. registry.

We estimate the following costs to do the modification:

—
Labor costParts costTotal cost per airplaneTotal cost on U.S. operators
1 work-hour × $80 per hour = $80Not Applicable$80$4,320

Note:

BRS will provide warranty credit to the extent noted in Ballistic Recovery Systems, Inc. Service Bulletins SB 07-01 and SB 07-02, both dated June 8, 2007.

Authority for This RulemakingPage 2

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 2

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-2007-29317; Directorate Identifier 2007-CE-079-AD” in your request.

Adoption of the amendmentPage 2

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 · 3

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

Registered aircraft · 30,787

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
  • Cessna29,103 aircraft
  • Textron1,682 aircraft
  • Cessna Wren2 aircraft
By year built
19412026
Registered aircraft by year built: 26,984 aircraft
19411
19431
19511
19521
19531
195560
1956566
1957338
1958314
1959337
1960361
1961319
1962304
1963491
1964895
19651,025
19661,103
1967678
1968977
1969817
1970427
1971499
1972778
19731,131
19741,052
19751,419
19761,472
19771,441
19781,193
19791,131
1980474
1981532
1982203
198384
1984127
1985184
198687
19882
19961
1997185
1998434
1999386
2000409
2001335
2002273
2003263
2004338
2005427
2006373
2007303
2008252
2009123
201085
201191
2012113
201342
201484
2015101
201682
201790
201864
2019106
2020137
2021135
2022139
2023213
2024213
2025205
2026156

3,803 with no year recorded

By model

See all 39 models

Aircraft

See all 30,787 aircraft