Published 2009-09-14 · Federal Register document E9-21741
Airworthiness Directives; British Aerospace Regional Aircraft Model HP.137 Jetstream Mk.1, Jetstream Series 200 and 3101, and Jetstream Model 3201 Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for the products listed above that will supersede an existing AD. This AD results from mandatory continuing airworthiness information (MCAI) issued by the 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 2026-09-03T22:23:30.011257+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2009-cb57e588bd107238
- Source row
- results[249]
- Raw source SHA-256
- cb57e588bd10723805ef0ea28ddc0685de14711012023c7e7d12178879efaeed
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2009-19-03
- Effective date printed in this edition
- 2009-10-05
Read 10 complete recorded clauses
Effective Date
Effective Date
(a) This airworthiness directive (AD) becomes effective October
5, 2009.
Exact source excerpt. Text positions 12218–12313, end exclusive, in the original decoded publication. SHA-256: fdc885bd8ca5ef60b19e345b5d566894b2a9ae405e1053a78ef0ceca8a7a8cdc
Affected ADs
Affected ADs
(b) This AD supersedes AD 2009-13-10; Amendment 39-15949.
Exact source excerpt. Text positions 12313–12390, end exclusive, in the original decoded publication. SHA-256: 581b3d22162cbd01029cb303a5a2b701188fe22d24d7ebae0bc02486f9874330
Applicability wording · Applicability
Applicability
(c) This AD applies to Model HP.137 Jetstream Mk.1, Jetstream
Series 200 and 3101, and Jetstream Model 3201 airplanes, all serial
numbers, certificated in any category.
Exact source excerpt. Text positions 12390–12581, end exclusive, in the original decoded publication. SHA-256: 8de1c00b09bed3fcea508d1a13ad137ec3071709f55cfabe5445ecf2c56a4394
Subject
Subject
(d) Air Transport Association of America (ATA) Code 32: Landing
Gear.
Exact source excerpt. Text positions 12581–12666, end exclusive, in the original decoded publication. SHA-256: 04c646b47f337af91d71c4e07f7d2370454add13447fb1407b8cea8db5e1159e
Reason
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
BAE Systems have been notified by the main landing gear (MLG)
radius rod manufacturer, APPH Ltd, that a batch of incorrectly
manufactured Buffer Springs (part number 184818) has been supplied
to their parts distributor and maintenance- and repair organisation
(MRO) facilities in North America.
There is a risk that any radius rod fitted with one of these
incorrectly manufactured Buffer Springs could jam in an unlocked
position. This condition, if not corrected, could result in MLG
collapse and consequent injury to occupants of the aeroplane. EASA
issued AD 2009-0121-E to require the replacement of the affected
radius rods.
BAE Systems (Operations) Ltd Alert Service Bulletin (ASB) 32-A-
JA090640 Revision 2 (the ASB) has now been issued, which identifies
an additional seven affected radius rods by serial number (s/n).
For the reasons described above, this AD retains the
requirements of AD 2009-0121-E, which is superseded, and expands the
applicability to include the replacement of the additional units.
Exact source excerpt. Text positions 12666–13794, end exclusive, in the original decoded publication. SHA-256: 64adfa5a1b68adba3924845921ece9e638ea351f80dfc96f365b42e13ec3e8d6
Actions and Compliance
Actions and Compliance
(f) Unless already done, do the following actions:
(1) Before further flight after October 5, 2009 (the effective
date of this AD) inspect the main landing gear (MLG) radius rods to
identify if you have part number (P/N) 1847/D through 1847/N and
1862/D through 1862/N with one of the affected serial numbers listed
in British Aerospace Jetstream Series 3100 and 3200 Alert Service
Bulletin 32-A-JA090640, Revision 2, dated August 11, 2009. Perform
the inspection following British Aerospace Jetstream Series 3100 and
3200 Alert Service Bulletin 32-A-JA090640, Revision 2, dated August
11, 2009. Only paragraphs (f)(3) and (f)(4) of this AD apply to you
if one or both of the following exists:
(i) If you do not have one of the affected P/Ns installed; and/
or
(ii) If you can positively show (maintenance records) that,
during the inspection required by AD 2009-13-10, none of the serial
number radius rods listed in
[[Page 46890]]
British Aerospace Jetstream Series 3100 and 3200 Alert Service
Bulletin 32-A-JA090640, Revision 2, dated August 11, 2009, are
installed.
(2) If as a result of the inspection required in paragraph
(f)(1) of this AD you find one of the affected P/N MLG radius rods
installed on the airplane, before further flight, install one of the
following MLG radius rods:
(i) A serviceable MLG radius rod that is not in one of the
following P/N ranges: 1847/D through 1847/N or 1862/D through 1862/
N; or
(ii) An affected P/N MLG radius rod that has already been
inspected following APPH Ltd. Service Bulletin 1847-32-14 or 1862-
32-14, as applicable, both dated June 2009, and found to be
serviceable.
(3) As of October 5, 2009 (the effective date of this AD), do
not install an affected part number MLG radius rod unless it has
been inspected following APPH Ltd. Service Bulletin 1847-32-14 or
1862-32-14, as applicable, both dated June 2009, and found to be
serviceable.
Note 1: The inspection requirements of paragraph (f)(3) above
apply to any replacement required per AD 2007-21-17.
(4) Within 30 days after the inspection required in paragraph
(f)(1) of this AD, send an Accomplishment (Inspection) Report to BAE
Systems following the instructions in paragraph 2.C of British
Aerospace Jetstream Series 3100 and 3200 Alert Service Bulletin 32-
A-JA090640, Revision 2, dated August 11, 2009. Include the details
of any radius rods removed.
FAA AD Differences
Note 2: This AD differs from the MCAI and/or service information
as follows: No differences.
Exact source excerpt. Text positions 13794–16376, end exclusive, in the original decoded publication. SHA-256: ff2396e78e7d035e667874f57b49d1fcc9b41d9cf3af766029e6e12e857048ca
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 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: Taylor Martin, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4138; fax: (816) 329-4090. 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 16376–17746, end exclusive, in the original decoded publication. SHA-256: 34f0f9638c47b2f2ae3d6c8b9878012b1c6e46be5614c8d4de3b9ec2b7782051
Special Flight Permit
Special Flight Permit
(h) Under 14 CFR 39.23, we are limiting special flight permits
for the purpose of compliance with this AD under the following
conditions:
(1) Operate the airplane only with the MLG in the down and
verified locked position throughout the entire flight; and
(2) Coordinate additional flight restrictions with British
Aerospace Regional Aircraft using the contact information provided
in paragraph (j)(2) of this AD.
Exact source excerpt. Text positions 17746–18201, end exclusive, in the original decoded publication. SHA-256: 73d6bf6e7e49aeae92a550007acd0e664d7c56782cc94bb5b1225bdd0c61e831
Related Information
Related Information
(i) Refer to MCAI EASA Emergency AD No. 2009-0181-E, dated
August 12, 2009; British Aerospace Jetstream Series 3100 and 3200
Alert Service Bulletin 32-A-JA090640, Revision 2, dated August 11,
2009 (includes an attached Accomplishment Report); and APPH Ltd.
Service Bulletins 1847-32-14 and 1862-32-14, both dated June 2009,
for related information.
Exact source excerpt. Text positions 18201–18581, end exclusive, in the original decoded publication. SHA-256: d30e4cc06ed1843950656814567698d2ec7287b5b83941d2e599b6ee822df328
Material Incorporated by Reference
Material Incorporated by Reference
(j) You must use British Aerospace Jetstream Series 3100 and
3200 Alert Service Bulletin 32-A-JA090640, Revision 2, dated August
11, 2009 (includes an attached Accomplishment Report); and APPH Ltd.
Service Bulletins 1847-32-14 and 1862-32-14, both dated June 2009,
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 British Aerospace Jetstream Series
3100 and 3200 Alert Service Bulletin 32-A-JA090640, Revision 2,
dated August 11, 2009 (includes an attached Accomplishment Report)
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) On June 26, 2009 (74 FR 29936, June 24, 2009), the Director
of the Federal Register previously approved the incorporation by
reference of APPH Ltd. Service Bulletins 1847-32-14 and 1862-32-14,
both dated June 2009.
(3) For service information identified in this AD, contact BAE
Systems (Operations) Ltd., Customer Information Department,
Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United
Kingdom; telephone: +44 1292 675207; fax: +44 1292 675704; e-mail:
[email protected]; Internet: http://www.baesystems.com/Capabilities/Air/.
(4) You may review copies of the service information
incorporated by reference for this AD at the FAA, Central Region,
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri
64106. For information on the availability of this material at the
Central Region, call (816) 329-3768.
(5) You may also review copies of the service information
incorporated by reference for this AD 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 18581–20473, end exclusive, in the original decoded publication. SHA-256: 32811efeb730aa48e019e8d210214305b1b35a63395e127f2736392341980718
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 2009-19-03 · 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: a92b4ab00ddac04dfd23c982e15932b16f584af2ca490732a7417780aee63366. Source manifest: 842e617bb04c98a4999688a79c45ba041c56ae887154bda68d364f1fed48058e.
Official source · 2009-09-14
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 74, Number 176 (Monday, September 14, 2009)]
[Rules and Regulations]
[Pages 46888-46890]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E9-21741]
[[Page 46888]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0817; Directorate Identifier 2009-CE-046-AD;
Amendment 39-16020; AD 2009-19-03]
RIN 2120-AA64
Airworthiness Directives; British Aerospace Regional Aircraft
Model HP.137 Jetstream Mk.1, Jetstream Series 200 and 3101, and
Jetstream Model 3201 Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above that will supersede an existing AD. This AD
results from mandatory continuing airworthiness information (MCAI)
issued by the aviation authority of another country to identify and
correct an unsafe condition on an aviation product. The MCAI describes
the unsafe condition as:
BAE Systems have been notified by the main landing gear (MLG)
radius rod manufacturer, APPH Ltd, that a batch of incorrectly
manufactured Buffer Springs (part number 184818) has been supplied
to their parts distributor and maintenance and repair organisation
(MRO) facilities in North America.
There is a risk that any radius rod fitted with one of these
incorrectly manufactured Buffer Springs could jam in an unlocked
position. This condition, if not corrected, could result in MLG
collapse and consequent injury to occupants of the aeroplane. EASA
issued AD 2009-0121-E to require the replacement of the affected
radius rods.
BAE Systems (Operations) Ltd Alert Service Bulletin (ASB) 32-A-
JA090640 Revision 2 (the ASB) has now been issued, which identifies
an additional seven affected radius rods by serial number (s/n).
This AD requires actions that are intended to address the unsafe
condition described in the MCAI.
DATES: This AD becomes effective October 5, 2009.
On October 5, 2009, the Director of the Federal Register approved
the incorporation by reference of British Aerospace Jetstream Series
3100 and 3200 Alert Service Bulletin 32-A-JA090640, Revision 2, dated
August 11, 2009, listed in this AD.
As of June 26, 2009 (74 FR 29936, June 24, 2009), the Director of
the Federal Register approved the incorporation by reference of British
Aerospace Jetstream Series 3100 and 3200 Alert Service Bulletin 32-A-
JA090640, dated June 2009 (includes an attached Accomplishment Report),
and APPH Ltd. Service Bulletins 1847-32-14 and 1862-32-14, as
applicable, both dated June 2009, listed in this AD.
We must receive comments on this AD by October 29, 2009.
ADDRESSES: You may send comments by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
<bullet> Fax: (202) 493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
<bullet> Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.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 this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (telephone (800) 647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Taylor Martin, Aerospace Engineer, 901
Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-
4138; fax: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Discussion
On June 18, 2009, we issued AD 2009-13-10, Amendment 39-15949 (74
FR 29936; June 24, 2009). That AD required actions intended to address
an unsafe condition on the products listed above.
Since we issued AD 2009-13-10, British Aerospace Regional Aircraft
has issued revised service information which identifies an additional
seven affected radius rods by serial number.
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
Emergency AD No. 2009-0181-E, dated August 12, 2009 (referred to after
this as ``the MCAI''), to correct an unsafe condition for the specified
products. The MCAI states:
BAE Systems have been notified by the main landing gear (MLG)
radius rod manufacturer, APPH Ltd, that a batch of incorrectly
manufactured Buffer Springs (part number 184818) has been supplied
to their parts distributor and maintenance and repair organisation
(MRO) facilities in North America.
There is a risk that any radius rod fitted with one of these
incorrectly manufactured Buffer Springs could jam in an unlocked
position. This condition, if not corrected, could result in MLG
collapse and consequent injury to occupants of the aeroplane. EASA
issued AD 2009-0121-E to require the replacement of the affected
radius rods.
BAE Systems (Operations) Ltd Alert Service Bulletin (ASB) 32-A-
JA090640 Revision 2 (the ASB) has now been issued, which identifies
an additional seven affected radius rods by serial number (s/n).
For the reasons described above, this AD retains the
requirements of AD 2009-0121-E, which is superseded, and expands the
applicability to include the replacement of the additional units.
You may obtain further information by examining the MCAI in the AD
docket.
Relevant Service Information
British Aerospace Regional Aircraft has issued:
<bullet> British Aerospace Jetstream Series 3100 and 3200 Alert
Service Bulletin 32-A-JA090640, dated June 2009 (includes an attached
Accomplishment Report);
<bullet> British Aerospace Jetstream Series 3100 and 3200 Alert
Service Bulletin 32-A-JA090640, Revision 2, dated August 11, 2009
(includes an attached Accomplishment Report); and
<bullet> APPH Ltd. Service Bulletins 1847-32-14 and 1862-32-14,
both dated June 2009.
The actions described in this service information are intended to
correct the unsafe condition identified in the MCAI.
FAA's Determination and Requirements of the AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with this State of Design Authority, they
have notified us of the unsafe condition described in the MCAI and
service information referenced above. We are issuing this AD because we
evaluated all information provided by the State of Design Authority and
determined the unsafe condition exists and is likely to exist or
develop on other products of the same type design.
Differences Between This AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
[[Page 46889]]
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 have also required different actions in this AD from those
in the MCAI in order to follow FAA policies. Any such differences are
described in a separate paragraph of the AD. These requirements take
precedence over those copied from the MCAI.
FAA's Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD. The FAA has found that the risk to the flying public justifies
waiving notice and comment prior to adoption of this rule because we
evaluated all information provided by the State of Design Authority and
determined the unsafe condition exists and is likely to exist or
develop on other products of the same type design. Therefore, we
determined that notice and opportunity for public comment before
issuing this AD are impracticable and that good cause exists for making
this amendment effective in fewer than 30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2009-0817; Directorate
Identifier 2009-CE-046-AD'' at the beginning of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this AD. We will consider all
comments received by the closing date and may amend this AD because of
those comments.
We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.
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 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 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.
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 removing Amendment 39-15949 (74 FR
29936; June 24, 2009), and adding the following new AD:
2009-19-03 British Aerospace Regional Aircraft: Amendment 39-16020;
Docket No. FAA-2009-0817; Directorate Identifier 2009-CE-046-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective October
5, 2009.
Affected ADs
(b) This AD supersedes AD 2009-13-10; Amendment 39-15949.
Applicability
(c) This AD applies to Model HP.137 Jetstream Mk.1, Jetstream
Series 200 and 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:
BAE Systems have been notified by the main landing gear (MLG)
radius rod manufacturer, APPH Ltd, that a batch of incorrectly
manufactured Buffer Springs (part number 184818) has been supplied
to their parts distributor and maintenance- and repair organisation
(MRO) facilities in North America.
There is a risk that any radius rod fitted with one of these
incorrectly manufactured Buffer Springs could jam in an unlocked
position. This condition, if not corrected, could result in MLG
collapse and consequent injury to occupants of the aeroplane. EASA
issued AD 2009-0121-E to require the replacement of the affected
radius rods.
BAE Systems (Operations) Ltd Alert Service Bulletin (ASB) 32-A-
JA090640 Revision 2 (the ASB) has now been issued, which identifies
an additional seven affected radius rods by serial number (s/n).
For the reasons described above, this AD retains the
requirements of AD 2009-0121-E, which is superseded, and expands the
applicability to include the replacement of the additional units.
Actions and Compliance
(f) Unless already done, do the following actions:
(1) Before further flight after October 5, 2009 (the effective
date of this AD) inspect the main landing gear (MLG) radius rods to
identify if you have part number (P/N) 1847/D through 1847/N and
1862/D through 1862/N with one of the affected serial numbers listed
in British Aerospace Jetstream Series 3100 and 3200 Alert Service
Bulletin 32-A-JA090640, Revision 2, dated August 11, 2009. Perform
the inspection following British Aerospace Jetstream Series 3100 and
3200 Alert Service Bulletin 32-A-JA090640, Revision 2, dated August
11, 2009. Only paragraphs (f)(3) and (f)(4) of this AD apply to you
if one or both of the following exists:
(i) If you do not have one of the affected P/Ns installed; and/
or
(ii) If you can positively show (maintenance records) that,
during the inspection required by AD 2009-13-10, none of the serial
number radius rods listed in
[[Page 46890]]
British Aerospace Jetstream Series 3100 and 3200 Alert Service
Bulletin 32-A-JA090640, Revision 2, dated August 11, 2009, are
installed.
(2) If as a result of the inspection required in paragraph
(f)(1) of this AD you find one of the affected P/N MLG radius rods
installed on the airplane, before further flight, install one of the
following MLG radius rods:
(i) A serviceable MLG radius rod that is not in one of the
following P/N ranges: 1847/D through 1847/N or 1862/D through 1862/
N; or
(ii) An affected P/N MLG radius rod that has already been
inspected following APPH Ltd. Service Bulletin 1847-32-14 or 1862-
32-14, as applicable, both dated June 2009, and found to be
serviceable.
(3) As of October 5, 2009 (the effective date of this AD), do
not install an affected part number MLG radius rod unless it has
been inspected following APPH Ltd. Service Bulletin 1847-32-14 or
1862-32-14, as applicable, both dated June 2009, and found to be
serviceable.
Note 1: The inspection requirements of paragraph (f)(3) above
apply to any replacement required per AD 2007-21-17.
(4) Within 30 days after the inspection required in paragraph
(f)(1) of this AD, send an Accomplishment (Inspection) Report to BAE
Systems following the instructions in paragraph 2.C of British
Aerospace Jetstream Series 3100 and 3200 Alert Service Bulletin 32-
A-JA090640, Revision 2, dated August 11, 2009. Include the details
of any radius rods removed.
FAA AD Differences
Note 2: This AD differs from the MCAI and/or service information
as follows: No differences.
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards 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: Taylor Martin, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4138; fax: (816) 329-4090. 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.
Special Flight Permit
(h) Under 14 CFR 39.23, we are limiting special flight permits
for the purpose of compliance with this AD under the following
conditions:
(1) Operate the airplane only with the MLG in the down and
verified locked position throughout the entire flight; and
(2) Coordinate additional flight restrictions with British
Aerospace Regional Aircraft using the contact information provided
in paragraph (j)(2) of this AD.
Related Information
(i) Refer to MCAI EASA Emergency AD No. 2009-0181-E, dated
August 12, 2009; British Aerospace Jetstream Series 3100 and 3200
Alert Service Bulletin 32-A-JA090640, Revision 2, dated August 11,
2009 (includes an attached Accomplishment Report); and APPH Ltd.
Service Bulletins 1847-32-14 and 1862-32-14, both dated June 2009,
for related information.
Material Incorporated by Reference
(j) You must use British Aerospace Jetstream Series 3100 and
3200 Alert Service Bulletin 32-A-JA090640, Revision 2, dated August
11, 2009 (includes an attached Accomplishment Report); and APPH Ltd.
Service Bulletins 1847-32-14 and 1862-32-14, both dated June 2009,
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 British Aerospace Jetstream Series
3100 and 3200 Alert Service Bulletin 32-A-JA090640, Revision 2,
dated August 11, 2009 (includes an attached Accomplishment Report)
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) On June 26, 2009 (74 FR 29936, June 24, 2009), the Director
of the Federal Register previously approved the incorporation by
reference of APPH Ltd. Service Bulletins 1847-32-14 and 1862-32-14,
both dated June 2009.
(3) For service information identified in this AD, contact BAE
Systems (Operations) Ltd., Customer Information Department,
Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United
Kingdom; telephone: +44 1292 675207; fax: +44 1292 675704; e-mail:
[email protected]; Internet: http://www.baesystems.com/Capabilities/Air/.
(4) You may review copies of the service information
incorporated by reference for this AD at the FAA, Central Region,
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri
64106. For information on the availability of this material at the
Central Region, call (816) 329-3768.
(5) You may also review copies of the service information
incorporated by reference for this AD 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 September 1, 2009.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. E9-21741 Filed 9-11-09; 8:45 am]
BILLING CODE 4910-13-P
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