Published 2008-11-04 · Federal Register document E8-25762
Airworthiness Directives; Cessna Aircraft Company 150 Series Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) 150 series airplanes with the BRS-150 Parachute System installed via Supplemental Type Certificate (STC) SA64CH. This AD requires you to replace the pick-up collar support and nylon screws for the BRS-150 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. This condition could result in the parachute failing to successfully deploy.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:26.953736+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2008-e9cf118935fdae82
- Source row
- results[399]
- Raw source SHA-256
- e9cf118935fdae82a000e2c01764c770bd79679c1dd4c2b00fdcd3b030f92fe5
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2008-22-18
- Effective date printed in this edition
- 2008-12-09
Read 7 complete recorded clauses
Effective Date
Effective Date
(a) This AD becomes effective on December 9, 2008.
Exact source excerpt. Text positions 7228–7300, end exclusive, in the original decoded publication. SHA-256: b5f60719ded966581edc515a943221e68e889d1abf312543225422adecda2a04
Affected ADs
Affected ADs
(b) None.
Exact source excerpt. Text positions 7300–7329, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b
Applicability wording · Applicability
Applicability
(c) This AD applies to Models 150, 150A, 150B, 150C, 150D, 150E,
150F, 150G, 150H, 150J, 150K, A150K, 150L, A150L, 150M, A150M, 152,
and A152 airplanes that:
(1) Have a BRS-150 Parachute System with a serial number in the
range of 50001 through 50006 installed via Supplemental Type
Certificate (STC) SA64CH; and
(2) Are certificated in any category.
Exact source excerpt. Text positions 7329–7712, end exclusive, in the original decoded publication. SHA-256: a4404d05841ade20637b9a66add7a03380ccaae4d9ef47f70668fe833b3435aa
Unsafe Condition
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 result in the
parachute failing to successfully deploy.
Exact source excerpt. Text positions 7712–8099, end exclusive, in the original decoded publication. SHA-256: 3ffb4e4f894457f059a18cb2a7a239e73285d6425b4f67ae35467c882f7253b1
Compliance
Compliance
(e) To address this problem, you must do the following, unless
already done:
[[Page 65509]]
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
Remove the pick-up collar Within the next 25 Follow BRS Service
support, nylon screws, and hours time-in- Bulletin SB 2008-04-
launch tube and replace service after 01 R1, issued April
with a new pick-up collar December 9, 2008 24, 2008.
support, custom tension (the effective date
screws, and new launch tube. of this AD).
------------------------------------------------------------------------
Exact source excerpt. Text positions 8099–8876, end exclusive, in the original decoded publication. SHA-256: d63c6c21e813ed3d69648ac94b829e55efd1b7c4a29985ff671d3340a6812f4d
Alternative Methods of Compliance (AMOCs)
Alternative Methods of Compliance (AMOCs)
(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: Gregory Michalik, Senior Aerospace Engineer, Chicago ACO, FAA,
2300 East Devon Avenue, Des Plaines, Illinois 60018; telephone:
(847) 294-7135; fax: (847) 294-7834; e-mail:
[email protected]. 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.
Exact source excerpt. Text positions 8876–9531, end exclusive, in the original decoded publication. SHA-256: cd8bedfb490e432c4f21a8ad6aa07f72ef11b21b46831e4ed3e037d3a905639b
Material Incorporated by Reference
Material Incorporated by Reference
(g) You must use BRS Service Bulletin SB 2008-04-01 R1, issued
April 24, 2008, 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., 380 Airport Road, South Saint
Paul, MN 55075-3551; telephone: (651) 457-7491; fax: (651) 457-8651;
e-mail: [email protected]; Internet: http://www.brsparachutes.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.
Exact source excerpt. Text positions 9531–10526, end exclusive, in the original decoded publication. SHA-256: 21086279d6bb8a230520071246380ae5711a5c78efb71991ddd0768753d19b79
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2008-22-18 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: b199054f547301d90f1ac23877aced6323d852bbe5332b1f296248a3019ba2f8. Source manifest: 3723e8a4156ca77a42766fdc002ccd0fd2167d8574883e6a440fec9c69c1bd24.
Official source · 2008-11-04
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 73, Number 214 (Tuesday, November 4, 2008)]
[Rules and Regulations]
[Pages 65507-65509]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E8-25762]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0790; Directorate Identifier 2008-CE-042-AD;
Amendment 39-15715; AD 2008-22-18]
RIN 2120-AA64
Airworthiness Directives; Cessna Aircraft Company 150 Series
Airplanes
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 (Cessna) 150 series airplanes with the BRS-150
Parachute System installed via Supplemental Type Certificate (STC)
SA64CH. This AD requires you to replace the pick-up collar support and
nylon screws for the BRS-150 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. This condition could result
in the parachute failing to successfully deploy.
DATES: This AD becomes effective on December 9, 2008.
On December 9, 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
[[Page 65508]]
Recovery Systems, Inc., 380 Airport Road, South Saint Paul, MN 55075-
3551; telephone: (651) 457-7491; fax: (651) 457-8651; e-mail:
[email protected]; Internet: http://www.brsparachutes.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://www.regulations.gov. The docket number is FAA-2008-0790;
Directorate Identifier 2008-CE-042-AD.
FOR FURTHER INFORMATION CONTACT: Gregory Michalik, Senior Aerospace
Engineer, Chicago Aircraft Certification Office, FAA, 2300 East Devon
Avenue, Des Plaines, Illinois 60018; telephone: (847) 294-7135; fax:
(847) 294-7834; e-mail: [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
On June 30, 2008, 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 Model 150 Series airplanes. This proposal was
published in the Federal Register as a notice of proposed rulemaking
(NPRM) on July 18, 2008 (73 FR 41305). The NPRM proposed to replace the
pick-up collar support and nylon screws for the BRS-150 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:
<bullet> Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
<bullet> 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 6 airplanes in the U.S. registry.
We estimate the following costs to do the modification:
----------------------------------------------------------------------------------------------------------------
Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
----------------------------------------------------------------------------------------------------------------
5 work-hours x $80 per hour = $400......... Not applicable............... $400 $2,400
----------------------------------------------------------------------------------------------------------------
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:
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-2008-0790; Directorate Identifier 2008-CE-042-AD'' in your
request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
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
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. FAA amends Sec. 39.13 by adding the following new AD:
2008-22-18 Cessna Aircraft Company: Amendment 39-15715; Docket No.
FAA-2008-0790; Directorate Identifier 2008-CE-042-AD.
Effective Date
(a) This AD becomes effective on December 9, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Models 150, 150A, 150B, 150C, 150D, 150E,
150F, 150G, 150H, 150J, 150K, A150K, 150L, A150L, 150M, A150M, 152,
and A152 airplanes that:
(1) Have a BRS-150 Parachute System with a serial number in the
range of 50001 through 50006 installed via Supplemental Type
Certificate (STC) SA64CH; and
(2) Are certificated in any category.
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 result in the
parachute failing to successfully deploy.
Compliance
(e) To address this problem, you must do the following, unless
already done:
[[Page 65509]]
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
Remove the pick-up collar Within the next 25 Follow BRS Service
support, nylon screws, and hours time-in- Bulletin SB 2008-04-
launch tube and replace service after 01 R1, issued April
with a new pick-up collar December 9, 2008 24, 2008.
support, custom tension (the effective date
screws, and new launch tube. of this AD).
------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(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: Gregory Michalik, Senior Aerospace Engineer, Chicago ACO, FAA,
2300 East Devon Avenue, Des Plaines, Illinois 60018; telephone:
(847) 294-7135; fax: (847) 294-7834; e-mail:
[email protected]. 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 BRS Service Bulletin SB 2008-04-01 R1, issued
April 24, 2008, 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., 380 Airport Road, South Saint
Paul, MN 55075-3551; telephone: (651) 457-7491; fax: (651) 457-8651;
e-mail: [email protected]; Internet: http://www.brsparachutes.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.
Issued in Kansas City, Missouri, on October 21, 2008.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-25762 Filed 11-3-08; 8:45 am]
BILLING CODE 4910-13-P
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The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:27:21.215531+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
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