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AGENCY:
Federal Aviation Administration (FAA), Department of Transportation (DOT).
ACTION:
Final rule.
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.
DATES:
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.
ADDRESSES:
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.
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.
Comments
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.
Conclusion
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 Compliance
We estimate that this AD affects 54 airplanes in the U.S. registry.
We estimate the following costs to do the modification:
—
Labor cost
Parts cost
Total cost per airplane
Total cost on U.S. operators
1 work-hour × $80 per hour = $80
Not 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 Rulemaking
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 Findings
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:
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.
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:
PART 39—AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
(a) This AD becomes effective on February 28, 2008.
Affected ADs
(b) None.
Applicability
(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 models
Cessna 182 models
172
182G
172A
182H
172B
182J
172C
182K
172D
182L
172E
182M
172F (USAF T-41A)
182N
172G
182P
172H (USAF T-41A)
182Q
172I
182R
172K
182S
172L
182T
172M
T182
172N
T182T
172P
172Q
172R
172S
R172J
R172K
Unsafe Condition
(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
( printed page 4053)
result in the parachute failing to successfully deploy.
Compliance
(e) To address this problem, you must do the following, unless already done:
—
Actions
Compliance
Procedures
Remove and replace the pick-up collar support and two retaining screws
Within 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.
Alternative Methods of Compliance (AMOCs)
(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.
Material Incorporated by Reference
(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.