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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


Why this text is shown

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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f935f6cc883c3e5f0fce259c302a6b2f4632dfe24118411c4ff6f023e3b8632a
Text SHA-256
b199054f547301d90f1ac23877aced6323d852bbe5332b1f296248a3019ba2f8

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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.