Published 2007-04-13 · Federal Register document E7-6913
Airworthiness Directives; British Aerospace Regional Aircraft Models HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model 3201 Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:23.906952+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2007-daaa03e810180273
- Source row
- results[159]
- Raw source SHA-256
- daaa03e81018027354d93b79e2a5f918dd4e1ce116086c5ab24f0dfd782528aa
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2007-08-06
- Effective date printed in this edition
- 2007-05-18
Read 9 complete recorded clauses
Effective Date
Effective Date
(a) This airworthiness directive (AD) becomes effective May 18,
2007.
Exact source excerpt. Text positions 8266–8358, end exclusive, in the original decoded publication. SHA-256: dce50ef263c5f08a2c4a0cff5b242dbc0c53ce4ba1f0894b3aabbf46c9b416d7
Affected ADs
Affected ADs
(b) None.
Exact source excerpt. Text positions 8358–8387, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b
Applicability wording · Applicability
Applicability
(c) This AD applies to Models HP.137 Jetstream Mk.1, Jetstream
Series 200, Jetstream Series 3101, and Jetstream Model 3201
airplanes, all serial numbers, certificated in any category.
Exact source excerpt. Text positions 8387–8593, end exclusive, in the original decoded publication. SHA-256: 02899993d81855a32c8537e0940d1da89a298e706adc9f3810e15dd7191541f9
Subject
Subject
(d) Air Transport Association of America (ATA) Code 32: Landing
Gear.
Exact source excerpt. Text positions 8593–8678, end exclusive, in the original decoded publication. SHA-256: 04c646b47f337af91d71c4e07f7d2370454add13447fb1407b8cea8db5e1159e
Reason
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
This Airworthiness Directive * * * is published in order to
maintain the structural integrity of the applicable aircraft. The
Service Bulletin provides life limits for critical landing gear
components. Failure of such items could lead to unsafe conditions.
Exact source excerpt. Text positions 8678–9026, end exclusive, in the original decoded publication. SHA-256: aa089c6c2438f03b3fa5e519aa2998d80bf909a8cccf610cb33bf71fdf4ffc7e
Actions and Compliance
Actions and Compliance
(f) Unless already done, within 60 days after May 18, 2007 (the
effective date of this AD), comply with the requirements given in
BAE Systems British Aerospace Jetstream Series 3100 and 3200 Service
Bulletin 32-JA981042 Rev 5, dated November 1, 2005.
Note 1: The compliance times of this AD are presented in cycles
(landings) since new (CSN). If you do not keep the total CSN, then
you may multiply the total number of airplane hours time-in-service
by 0.75.
FAA AD Differences
Note 2: This AD differs from the MCAI and/or service information
as follows: We allow a different method for calculating the CSN of a
component listed in this AD.
Exact source excerpt. Text positions 9026–9715, end exclusive, in the original decoded publication. SHA-256: 27c541883304dd849d5fa522d60e4b1b57bb537e9ca0c5a5c31dfc0817acb0b8
Other FAA AD Provisions
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Staff, FAA, ATTN: Taylor Martin, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4138; fax: (816) 329-4090, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. 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.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act (44
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has
approved the information collection requirements and has assigned
OMB Control Number 2120-0056.
Exact source excerpt. Text positions 9715–11064, end exclusive, in the original decoded publication. SHA-256: 101fea1b4950a1ce3ee48e2d6223cd5072c0af686143cb4509b76b96b827b9f9
Related Information
Related Information
(h) Refer to MCAI European Aviation Safety Agency (EASA) AD No.:
2006-0087, dated April 18, 2006, and BAE Systems British Aerospace
Jetstream Series 3100 and 3200 Service Bulletin 32-JA981042 Rev 5,
dated November 1, 2005, for related information.
Exact source excerpt. Text positions 11064–11341, end exclusive, in the original decoded publication. SHA-256: ccd34357d81ed3ed063b78ab67ff777374ed3ba087317ae9fdf10ea3e3d0c5c8
Material Incorporated by Reference
Material Incorporated by Reference
(i) You must use BAE Systems British Aerospace Jetstream Series
3100 and 3200 Service Bulletin 32-JA981042 Rev 5, dated November 1,
2005, 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
Customer Information Department, BAE Systems, Prestwick
International Airport, Ayshire, KA9 2RW, Scotland; telephone:
(01292) 675207; fax: (01292) 675704.
(3) You may review copies at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Room 506, 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/cfr/ibr-locations.html.
Exact source excerpt. Text positions 11341–12337, end exclusive, in the original decoded publication. SHA-256: d2bf7726a57d26ffc52b2deb355426569df29ddd4fa563d27432745005f171e9
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 2007-08-06 · 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: 0e3fcb0cc0dbdbd724b0ced0992b781b9023eaf5070b8cc1f2819f3620ac7c27. Source manifest: 4dcc5619d376809acaae204094c9fe70c5a164893bc9d9b07f21d13a06911050.
Official source · 2007-04-13
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 72, Number 71 (Friday, April 13, 2007)]
[Rules and Regulations]
[Pages 18565-18566]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-6913]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-27070 Directorate Identifier 2007-CE-003-AD;
Amendment 39-15023; AD 2007-08-06]
RIN 2120-AA64
Airworthiness Directives; British Aerospace Regional Aircraft
Models HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series
3101, and Jetstream Model 3201 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) issued by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as:
This Airworthiness Directive * * * is published in order to
maintain the structural integrity of the applicable aircraft. The
Service Bulletin provides life limits for critical landing gear
components. Failure of such items could lead to unsafe conditions.
We are issuing this AD to require actions to correct the unsafe
condition on these products.
DATES: This AD becomes effective May 18, 2007.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of May 18, 2007.
ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Taylor Martin, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4138; fax: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Streamlined Issuance of AD
The FAA is implementing a new process for streamlining the issuance
of ADs related to MCAI. The streamlined process will allow us to adopt
MCAI safety requirements in a more efficient manner and will reduce
safety risks to the public. This process continues to follow all FAA AD
issuance processes to meet legal, economic, Administrative Procedure
Act, and Federal Register requirements. We also continue to meet our
technical decision-making responsibilities to identify and correct
unsafe conditions on U.S.-certificated products.
This AD references the MCAI and related service information that we
considered in forming the engineering basis to correct the unsafe
condition. The AD contains text copied from the MCAI and for this
reason might not follow our plain language principles.
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on February 12, 2007
(72 FR 6500). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
This Airworthiness Directive * * * is published in order to
maintain the structural integrity of the applicable aircraft. The
Service Bulletin provides life limits for critical landing gear
components. Failure of such items could lead to unsafe conditions.
The MCAI requires:
From the effective date of this AD, it is mandatory to comply
with the requirements given in Jetstream Series 3100 and 3200
Service Bulletin 32-JA981042 Rev 5. Landing Gear--Main and Nose
Landing Gears--To introduce life limitations and provide means of
establishing total flight cycles since new for critical components *
* *
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
We reviewed the available data and determined that air safety and
the public interest require adopting the AD as proposed.
Differences Between This AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ substantively from the information
provided in the MCAI and related service information.
We might also have required different actions in this AD from those
in the MCAI in order to follow FAA policies. Any such differences are
highlighted in a Note within the AD.
Costs of Compliance
We estimate that this AD will affect 149 products of U.S. registry.
We also estimate that it will take about 2 work-hours per product to
comply with basic requirements of this AD. The average labor rate is
$80 per work-hour. Based on these figures, we estimate the cost of this
AD to the U.S. operators to be $23,840, or $160 per product.
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
rulemaking action.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on
[[Page 18566]]
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 this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under 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 regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD Docket.
Examining the AD Docket
You may examine the AD docket on the Internet at http://dms.dot.gov; or in person at the Docket Management Facility between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains the NPRM, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (telephone (800) 647-5227) is in the ADDRESSES section. Comments
will be available in the AD docket shortly after receipt.
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 FAA amends 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. The FAA amends Sec. 39.13 by adding the following new AD:
2007-08-06 British Aerospace Regional Aircraft: Amendment 39-15023;
Docket No. FAA-2007-27070; Directorate Identifier 2007-CE-003-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective May 18,
2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Models HP.137 Jetstream Mk.1, Jetstream
Series 200, Jetstream Series 3101, and Jetstream Model 3201
airplanes, all serial numbers, certificated in any category.
Subject
(d) Air Transport Association of America (ATA) Code 32: Landing
Gear.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
This Airworthiness Directive * * * is published in order to
maintain the structural integrity of the applicable aircraft. The
Service Bulletin provides life limits for critical landing gear
components. Failure of such items could lead to unsafe conditions.
Actions and Compliance
(f) Unless already done, within 60 days after May 18, 2007 (the
effective date of this AD), comply with the requirements given in
BAE Systems British Aerospace Jetstream Series 3100 and 3200 Service
Bulletin 32-JA981042 Rev 5, dated November 1, 2005.
Note 1: The compliance times of this AD are presented in cycles
(landings) since new (CSN). If you do not keep the total CSN, then
you may multiply the total number of airplane hours time-in-service
by 0.75.
FAA AD Differences
Note 2: This AD differs from the MCAI and/or service information
as follows: We allow a different method for calculating the CSN of a
component listed in this AD.
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Staff, FAA, ATTN: Taylor Martin, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4138; fax: (816) 329-4090, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. 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.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act (44
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has
approved the information collection requirements and has assigned
OMB Control Number 2120-0056.
Related Information
(h) Refer to MCAI European Aviation Safety Agency (EASA) AD No.:
2006-0087, dated April 18, 2006, and BAE Systems British Aerospace
Jetstream Series 3100 and 3200 Service Bulletin 32-JA981042 Rev 5,
dated November 1, 2005, for related information.
Material Incorporated by Reference
(i) You must use BAE Systems British Aerospace Jetstream Series
3100 and 3200 Service Bulletin 32-JA981042 Rev 5, dated November 1,
2005, 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
Customer Information Department, BAE Systems, Prestwick
International Airport, Ayshire, KA9 2RW, Scotland; telephone:
(01292) 675207; fax: (01292) 675704.
(3) You may review copies at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Room 506, 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/cfr/ibr-locations.html.
Issued in Kansas City, Missouri, on April 6, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-6913 Filed 4-12-07; 8:45 am]
BILLING CODE 4910-13-P
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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.
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