Airworthiness Directives; British Aerospace Regional Aircraft Jetstream Model 3201 Airplanes, 27953-27955 [07-2472]

Download as PDF Federal Register / Vol. 72, No. 96 / Friday, May 18, 2007 / Rules and Regulations Federal Reserve Office Number of business days following the banking day funds are deposited FOR FURTHER INFORMATION CONTACT: 3 3 Utica: 0210, 0280 .................... Kansas City: 0865, 2865 .................... 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 By order of the Board of Governors of the Federal Reserve System, acting through the Secretary of the Board under delegated authority, May 14, 2007. Jennifer J. Johnson, Secretary of the Board. [FR Doc. E7–9558 Filed 5–17–07; 8:45 am] BILLING CODE 6210–01–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2006–26284; Directorate Identifier 2006–CE–68–AD; Amendment 39– 15057; AD 2007–10–16] RIN 2120–AA64 Airworthiness Directives; British Aerospace Regional Aircraft Jetstream Model 3201 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: 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: 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 March 13, 2007 (72 FR 11300). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: cprice-sewell on PRODPC61 with RULES The Airworthiness Limitations Section of the Aircraft Maintenance Manual (AMM) applicable to the British Aerospace Jetstream 3200 has been revised. Some lives have been amended and new lives introduced. Compliance with these requirements is necessary to maintain airworthiness. We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective June 22, 2007. ADDRESSES: You may examine the AD docket on the Internet at https:// 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. The Airworthiness Limitations Section of the Aircraft Maintenance Manual (AMM) applicable to the British Aerospace Jetstream 3200 has been revised. Some lives have been amended and new lives introduced. Compliance with these requirements is necessary to maintain airworthiness. From the effective date of this Airworthiness Directive (AD), comply with the requirements of BAE Jetstream Series 3200 Aircraft Maintenance Manual, Chapter 05–10–05, Airworthiness Limitations Description and Operation Section*, Revision 14 or later EASA approved revision. *Only the structural fatigue tasks are mandated by this AD, the following tasks are not addressed by this AD: All the tasks recorded in Tables 2, 4, 5 and 8. Together with the Table No 3—task 27–70–000 Gust lock system. Comments VerDate Aug<31>2005 15:21 May 17, 2007 Jkt 211001 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. PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 27953 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 20 products of U.S. registry. We also estimate that it will take about 1 workhour per product to comply with basic requirements of this AD (inserting the document into the Airworthiness Limitations section of the Instructions for Continued Airworthiness or other FAA-approved maintenance document). The average labor rate is $80 per workhour. Based on these figures, we estimate the cost of this AD on U.S. operators to be $1,600, or $80 per product. We have no way of determining the costs associated with having to replace certain parts at an earlier time due to reduced life limits. 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. E:\FR\FM\18MYR1.SGM 18MYR1 27954 Federal Register / Vol. 72, No. 96 / Friday, May 18, 2007 / Rules and Regulations 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 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 https://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 Reason Air transportation, Aircraft, Aviation safety, Safety. (e) The mandatory continuing airworthiness information (MCAI) states: The Airworthiness Limitations Section of the Aircraft Maintenance Manual (AMM) applicable to the British Aerospace Jetstream 3200 has been revised. Some lives have been amended and new lives introduced. Compliance with these requirements is necessary to maintain airworthiness. From the effective date of this Airworthiness Directive (AD), comply with the requirements of BAE Jetstream Series 3200 Aircraft Maintenance Manual, Chapter 05–10–05, Airworthiness Limitations Description and Operation Section*, Revision 14 or later EASA approved revision. *Only the structural fatigue tasks are mandated by this AD, the following tasks are not addressed by this AD: All the tasks recorded in Tables 2, 4, 5 and 8. Together with the Table No 3—task 27–70–000 Gust lock system. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: I PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: I Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new AD: I 2007–10–16 British Aerospace Regional Aircraft Jetstream: Amendment 39– 15057; Docket No. FAA–2006–26284; Directorate Identifier 2006–CE–68–AD. Effective Date (a) This airworthiness directive (AD) becomes effective June 22, 2007. Affected ADs (b) None. Applicability (c) This AD applies to Jetstream Model 3201 airplanes, all serial numbers, certificated in any category. Subject (d) Air Transport Association of America (ATA) Code 55: Structures. Actions and Compliance (f) Within the next 60 days after June 22, 2007 (the effective date of this AD) do the following, unless already done: (1) Incorporate the information referenced below from Aircraft Maintenance Manual 05– 10–05 001—AIRWORTHINESS LIMITATIONS—DESCRIPTION AND OPERATION—BAe Jetstream 32, dated January 11, 2006, for Recurring Mandatory Inspections and Maintenance Actions into the Airworthiness Limitations section of the Instructions for Continued Airworthiness or other FAA-approved maintenance document. You may use a later European Aviation Safety Agency (EASA)-approved revision that incorporates these same life limits. Table number in document Affected areas (i) Table No. 1 ........................................................................... Wing, Fuselage, Fin, Tailplane, Engine mounting, Flap system. Electrical Power (all Items) ....................................................... Rudder pedal/brake master cylinder attachment brackets ...... Gust lock system ...................................................................... Ice and rain protection (all items) ............................................. Landing gear (all items) ............................................................ Lighting (all items) .................................................................... Doors (all items) ....................................................................... Fuselage (all items) .................................................................. Stabilizers (all items) ................................................................ Wings (all items) ....................................................................... cprice-sewell on PRODPC61 with RULES (ii) Table No. 2 ........................................................................... (iii) Table No. 3 .......................................................................... (iv) Table No. 3 .......................................................................... (v) Table No. 4 and Table No. 5 ............................................... (vi) Table No. 6 and Table No. 7 .............................................. (vii) Table No. 8 ......................................................................... (viii) Table No. 9 ........................................................................ (ix) Table No. 10 ........................................................................ (x) Table No. 11 ........................................................................ (xi) Table No. 12 ........................................................................ (2) The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may do the actions of this AD. Make an entry into the aircraft records showing compliance with this AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). FAA AD Differences Note: This AD differs from the MCAI and/ or service information as follows: (1) The MCAI requires you to comply with a version of a maintenance manual that VerDate Aug<31>2005 15:21 May 17, 2007 Jkt 211001 changes life limits. The FAA requires such changes through a change to the Airworthiness Limitations section of the Instructions for Continued Airworthiness or other FAA-approved maintenance document, and the FAA is mandating this through this AD. (2) We added information in paragraph (f) that allows the owner/operator to insert this information into the Airworthiness Limitations section of the Instructions for Continued Airworthiness or other FAAapproved maintenance document. Without PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 AD applies Yes. No. Yes. No. No. Yes. No. Yes. Yes. Yes. Yes. this information, a licensed mechanic would be required to do the action. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, FAA, Small Airplane Directorate, 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, E:\FR\FM\18MYR1.SGM 18MYR1 Federal Register / Vol. 72, No. 96 / Friday, May 18, 2007 / Rules and Regulations 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. Related Information (h) Refer to MCAI Civil Aviation Authority AD No. G–2004–0024, Issue Date: September 22, 2004, EASA approved on September 16, 2004, under approval number 2004–9648, for related information. Issued in Kansas City, Missouri, on May 9, 2007. Charles L. Smalley, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 07–2472 Filed 5–17–07; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF HEALTH AND HUMAN SERVICES Food and Drug Administration 21 CFR Part 510 New Animal Drugs; Change of Sponsor’s Address AGENCY: Food and Drug Administration, HHS. ACTION: Final rule. SUMMARY: The Food and Drug Administration (FDA) is amending the animal drug regulations to reflect a change of sponsor’s address for Modern Veterinary Therapeutics, LLC. DATES: This rule is effective May 18, 2007. cprice-sewell on PRODPC61 with RULES FOR FURTHER INFORMATION CONTACT: David R. Newkirk, Center for Veterinary Medicine (HFV–100), Food and Drug Administration, 7500 Standish Pl., Rockville, MD 20855, 301–827–6967, email: david.newkirk@fda.hhs.gov. SUPPLEMENTARY INFORMATION: Modern Veterinary Therapeutics, LLC, 18301 SW. 86th Ave., Miami, FL 33157, has VerDate Aug<31>2005 15:21 May 17, 2007 Jkt 211001 27955 informed FDA of a change of address to 1550 Madruga Ave., suite 329, Coral Gables, FL 33146. Accordingly, the agency is amending the regulations in 21 CFR 510.600(c) to reflect the change. This rule does not meet the definition of ‘‘rule’’ in 5 U.S.C. 804(3)(A) because it is a rule of ‘‘particular applicability.’’ Therefore, it is not subject to the congressional review requirements in 5 U.S.C. 801–808. Dated: May 7, 2007. Bernadette Dunham, Deputy Director, Center for Veterinary Medicine. [FR Doc. E7–9555 Filed 5–17–07; 8:45 am] List of Subjects in 21 CFR Part 510 21 CFR Parts 510 and 520 Administrative practice and procedure, Animal drugs, Labeling, Reporting and recordkeeping requirements. Therefore, under the Federal Food, Drug, and Cosmetic Act and under authority delegated to the Commissioner of Food and Drugs and redelegated to the Center for Veterinary Medicine, 21 CFR part 510 is amended as follows: I BILLING CODE 4160–01–S DEPARTMENT OF HEALTH AND HUMAN SERVICES Food and Drug Administration Oral Dosage Form New Animal Drugs; Phenylbutazone Powder AGENCY: Food and Drug Administration, HHS. ACTION: Final rule. SUMMARY: The Food and Drug Administration (FDA) is amending the animal drug regulations to reflect approval of an abbreviated new animal drug application (ANADA) filed by Superior Equine Pharmaceuticals, Inc. PART 510—NEW ANIMAL DRUGS The ANADA provides for the veterinary prescription use of phenylbutazone I 1. The authority citation for 21 CFR powder administered to horses in feed part 510 continues to read as follows: for the relief of inflammatory conditions Authority: 21 U.S.C. 321, 331, 351, 352, associated with the musculoskeletal 353, 360b, 371, 379e. system. I 2. In § 510.600, in the table in DATES: This rule is effective May 18, paragraph (c)(1) revise the entry for 2007. ‘‘Modern Veterinary Therapeutics, FOR FURTHER INFORMATION CONTACT: John LLC’’; and in the table in paragraph K. Harshman, Center for Veterinary (c)(2) revise the entry for ‘‘015914’’ to Medicine (HFV–104), Food and Drug read as follows: Administration, 7500 Standish Pl., Rockville, MD 20855, 301–827–0169, e§ 510.600 Names, addresses, and drug mail: john.harshman@fda.hhs.gov. labeler codes of sponsors of approved SUPPLEMENTARY INFORMATION: Superior applications. Equine Pharmaceuticals, Inc., Pleasant * * * * * Grove, UT 84062, filed ANADA 200– (c) * * * 333 that provides for the veterinary prescription use of SUPERIORBUTE (1) * * * (phenylbutazone) Powder administered to horses in feed for the relief of Drug labeler Firm name and address code inflammatory conditions associated with the musculoskeletal system. * * * * * Superior Equine Pharmaceuticals, Inc.’s Modern Veterinary TheraSUPERIORBUTE Powder is approved as peutics, LLC, 1550 a generic copy of IVX Animal Health, Madruga Ave., suite 329, Inc.’s Phenylbutazone Tablets, USP, Coral Gables, FL 33146 015914 approved under NADA 91–818. The * * * * * ANADA is approved as of April 20, 2007, and the regulations are amended (2) * * * in 21 CFR 520.1720e to reflect the approval. The basis of approval is Drug labeler discussed in the freedom of information Firm name and address code summary. In addition, Superior Equine * * * * * Pharmaceuticals, Inc., has not been 015914 Modern Veterinary Therapreviously listed in the animal drug peutics, LLC, 1550 regulations as a sponsor of an approved Madruga Ave., suite 329, application. At this time, 21 CFR Coral Gables, FL 33146 510.600(c) is being amended to add * * * * * entries for the firm. PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 E:\FR\FM\18MYR1.SGM 18MYR1

Agencies

[Federal Register Volume 72, Number 96 (Friday, May 18, 2007)]
[Rules and Regulations]
[Pages 27953-27955]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 07-2472]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-26284; Directorate Identifier 2006-CE-68-AD; 
Amendment 39-15057; AD 2007-10-16]
RIN 2120-AA64


Airworthiness Directives; British Aerospace Regional Aircraft 
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:

    The Airworthiness Limitations Section of the Aircraft 
Maintenance Manual (AMM) applicable to the British Aerospace 
Jetstream 3200 has been revised. Some lives have been amended and 
new lives introduced. Compliance with these requirements is 
necessary to maintain airworthiness.

    We are issuing this AD to require actions to correct the unsafe 
condition on these products.

DATES: This AD becomes effective June 22, 2007.

ADDRESSES: You may examine the AD docket on the Internet at https://
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 March 13, 2007 (72 
FR 11300). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    The Airworthiness Limitations Section of the Aircraft 
Maintenance Manual (AMM) applicable to the British Aerospace 
Jetstream 3200 has been revised. Some lives have been amended and 
new lives introduced. Compliance with these requirements is 
necessary to maintain airworthiness.
    From the effective date of this Airworthiness Directive (AD), 
comply with the requirements of BAE Jetstream Series 3200 Aircraft 
Maintenance Manual, Chapter 05-10-05, Airworthiness Limitations 
Description and Operation Section*, Revision 14 or later EASA 
approved revision.

    *Only the structural fatigue tasks are mandated by this AD, the 
following tasks are not addressed by this AD: All the tasks recorded 
in Tables 2, 4, 5 and 8. Together with the Table No 3--task 27-70-
000 Gust lock system.

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 20 products of U.S. registry. 
We also estimate that it will take about 1 work-hour per product to 
comply with basic requirements of this AD (inserting the document into 
the Airworthiness Limitations section of the Instructions for Continued 
Airworthiness or other FAA-approved maintenance document). The average 
labor rate is $80 per work-hour. Based on these figures, we estimate 
the cost of this AD on U.S. operators to be $1,600, or $80 per product.
    We have no way of determining the costs associated with having to 
replace certain parts at an earlier time due to reduced life limits.

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.

[[Page 27954]]

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 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 https://
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, 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:

2007-10-16 British Aerospace Regional Aircraft Jetstream: Amendment 
39-15057; Docket No. FAA-2006-26284; Directorate Identifier 2006-CE-
68-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective June 22, 
2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Jetstream Model 3201 airplanes, all 
serial numbers, certificated in any category.

Subject

    (d) Air Transport Association of America (ATA) Code 55: 
Structures.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    The Airworthiness Limitations Section of the Aircraft 
Maintenance Manual (AMM) applicable to the British Aerospace 
Jetstream 3200 has been revised. Some lives have been amended and 
new lives introduced. Compliance with these requirements is 
necessary to maintain airworthiness.
    From the effective date of this Airworthiness Directive (AD), 
comply with the requirements of BAE Jetstream Series 3200 Aircraft 
Maintenance Manual, Chapter 05-10-05, Airworthiness Limitations 
Description and Operation Section*, Revision 14 or later EASA 
approved revision. *Only the structural fatigue tasks are mandated 
by this AD, the following tasks are not addressed by this AD: All 
the tasks recorded in Tables 2, 4, 5 and 8. Together with the Table 
No 3--task 27-70-000 Gust lock system.

Actions and Compliance

    (f) Within the next 60 days after June 22, 2007 (the effective 
date of this AD) do the following, unless already done:
    (1) Incorporate the information referenced below from Aircraft 
Maintenance Manual 05-10-05 001--AIRWORTHINESS LIMITATIONS--
DESCRIPTION AND OPERATION--BAe Jetstream 32, dated January 11, 2006, 
for Recurring Mandatory Inspections and Maintenance Actions into the 
Airworthiness Limitations section of the Instructions for Continued 
Airworthiness or other FAA-approved maintenance document.
    You may use a later European Aviation Safety Agency (EASA)-
approved revision that incorporates these same life limits.

------------------------------------------------------------------------
   Table number in document       Affected areas         AD applies
------------------------------------------------------------------------
(i) Table No. 1...............  Wing, Fuselage,    Yes.
                                 Fin, Tailplane,
                                 Engine mounting,
                                 Flap system.
(ii) Table No. 2..............  Electrical Power   No.
                                 (all Items).
(iii) Table No. 3.............  Rudder pedal/      Yes.
                                 brake master
                                 cylinder
                                 attachment
                                 brackets.
(iv) Table No. 3..............  Gust lock system.  No.
(v) Table No. 4 and Table No.   Ice and rain       No.
 5.                              protection (all
                                 items).
(vi) Table No. 6 and Table No.  Landing gear (all  Yes.
 7.                              items).
(vii) Table No. 8.............  Lighting (all      No.
                                 items).
(viii) Table No. 9............  Doors (all items)  Yes.
(ix) Table No. 10.............  Fuselage (all      Yes.
                                 items).
(x) Table No. 11..............  Stabilizers (all   Yes.
                                 items).
(xi) Table No. 12.............  Wings (all items)  Yes.
------------------------------------------------------------------------

    (2) The owner/operator holding at least a private pilot 
certificate as authorized by section 43.7 of the Federal Aviation 
Regulations (14 CFR 43.7) may do the actions of this AD. Make an 
entry into the aircraft records showing compliance with this AD in 
accordance with section 43.9 of the Federal Aviation Regulations (14 
CFR 43.9).

FAA AD Differences

    Note: This AD differs from the MCAI and/or service information 
as follows:

    (1) The MCAI requires you to comply with a version of a 
maintenance manual that changes life limits. The FAA requires such 
changes through a change to the Airworthiness Limitations section of 
the Instructions for Continued Airworthiness or other FAA-approved 
maintenance document, and the FAA is mandating this through this AD.
    (2) We added information in paragraph (f) that allows the owner/
operator to insert this information into the Airworthiness 
Limitations section of the Instructions for Continued Airworthiness 
or other FAA-approved maintenance document. Without this 
information, a licensed mechanic would be required to do the action.

Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Staff, FAA, Small Airplane Directorate, 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,

[[Page 27955]]

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.

Related Information

    (h) Refer to MCAI Civil Aviation Authority AD No. G-2004-0024, 
Issue Date: September 22, 2004, EASA approved on September 16, 2004, 
under approval number 2004-9648, for related information.

    Issued in Kansas City, Missouri, on May 9, 2007.
Charles L. Smalley,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 07-2472 Filed 5-17-07; 8:45 am]
BILLING CODE 4910-13-P
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