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CFR Citation: 14 CFR Part 39

Docket ID: [Docket No. FAA-2008-0850; Directorate Identifier 2007-NM-342-AD; Amendment 39-15710; AD 2008-22-14]

RIN ID: RIN 2120-AA64

NOTICE: RULES

ACTION: Airworthiness Directives:

DOCUMENT ACTION: Final rule.

SUBJECT CATEGORY: Airworthiness Directives; Fokker Model F.28 Mark 0100 Airplanes

DATES: This AD becomes effective December 26, 2008.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of December 26, 2008.

DOCUMENT SUMMARY: We are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated 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:

* * * * *

During recent inspections it was found that some * * * bolts, that connect the horizontal stabilizer control unit actuator with the doglinks, were broken. This condition, if not corrected, could lead to [the loss of the flight control input connection to the horizontal stabilizer and consequent] partial loss of control of the aircraft.
* * * * *
We are issuing this AD to require actions to correct the unsafe condition on these products.

SUMMARY: Fokker Model F.28 Mark 0100 Airplanes,

SUPPLEMENTAL INFORMATION

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 August 7, 2008 (73 FR 45898) and proposed to supersede AD 971305, Amendment 3910051 (62 FR 34617, June 27, 1997). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states:

In January 1996, Fokker issued Service Bulletin (SB) SBF10027 069 (referencing Menasco, now Goodrich, SB 231002719) to introduce an inspection of bolt Part Number (P/N) 232331 for cracks after the examination of a failed bolt. This Service Bulletin was made mandatory by CAANL (Civil Aviation Authoritythe Netherlands) with the issuance of AD BLA 1996006 (A) [reference corresponding FAA AD 971305]. Additionally the same SB introduced a lower torque value for these bolts.

During recent inspections it was found that some of these bolts, that connect the horizontal stabilizer control unit actuator with the doglinks, were broken. This condition, if not corrected, could lead to [the loss of the flight control input connection to the horizontal stabilizer and consequent] partial loss of control of the aircraft.

Since an unsafe condition has been identified that continues to exist or develop on other aircraft of the same type design, this Airworthiness Directive supersedes CAANL AD 1996006 and requires an integrity check by a retorque in accordance with SBF10027091 and the installation of a tie wrap through the bolt, which will act as a retainer for the bolt and nut. The key function for this tie wrap is to keep the bolt in place in the event the bolt head fails. The corrective action includes replacing any failed bolt (i.e., broken or loose bolt) with a serviceable bolt. This AD also expands the applicability of AD 971305. You may obtain further information by examining the MCAI in the AD docket.

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 our FAA policies. Any such differences are highlighted in a Note within the AD.

Costs of Compliance

We estimate that this AD will affect about 9 products of U.S. registry. We also estimate that it will take about 3 workhours per product to comply with the basic requirements of this AD. The average labor rate is $80 per workhour. Based on these figures, we estimate the cost of this AD to the U.S. operators to be $2,160, or $240 per product.
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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 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 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:// www.regulations.gov; or in person at the Docket Operations office 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 Operations office (telephone (800) 6475527) 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
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39AIRWORTHINESS DIRECTIVES
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]
2. The FAA amends Sec. 39.13 by removing Amendment 3910051 (62 FR 34617, June 27, 1997) and adding the following new AD:
20082214 Fokker Services B.V.: Amendment 3915710. Docket No. FAA 20080850; Directorate Identifier 2007NM342AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective December 26, 2008.
Affected ADs
(b) This AD supersedes AD 971305, Amendment 3910051.
Applicability
(c) This AD applies to Fokker Model F.28 Mark 0100 airplanes, certificated in any category, all serial numbers.
Subject
(d) Air Transport Association (ATA) of America Code 27: Flight Controls.
Reason
(e) The mandatory continuing airworthiness information (MCAI) states:

In January 1996, Fokker issued Service Bulletin (SB) SBF10027 069 (referencing Menasco, now Goodrich, SB 231002719) to introduce an inspection of bolt Part Number (P/N) 232331 for cracks after the examination of a failed bolt. This Service Bulletin was made mandatory by CAANL (Civil Aviation Authoritythe Netherlands) with the issuance of AD BLA 1996006 (A) [reference corresponding FAA AD 971305]. Additionally the same SB introduced a lower torque value for these bolts.

During recent inspections it was found that some of these bolts, that connect the horizontal stabilizer control unit actuator with the doglinks, were broken. This condition, if not corrected, could lead to [the loss of the flight control input connection to the horizontal stabilizer and consequent] partial loss of control of the aircraft.

Since an unsafe condition has been identified that continues to exist or develop on other aircraft of the same type design, this Airworthiness Directive [European Aviation Safety Agency (EASA) Airworthiness Directive 20070287, dated November 15, 2007] supersedes CAANL AD 1996006 and requires an integrity check by a retorque in accordance with SBF10027091 and the installation of a tie wrap through the bolt, which will act as a retainer for the bolt and nut. The key function for this tiewrap is to keep the bolt in place in the event the bolt head fails.

The corrective action includes replacing any failed bolt (i.e., broken or loose bolt) with a serviceable bolt.
Actions and Compliance
(f) Unless already done, within 6 months after the effective date of this AD, do the following actions.
(1) Perform a onetime inspection (integrity check) for failure of the lower bolts of the stabilizer control unit doglinks, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF10027091, dated August 31, 2007. If a failed bolt is found, before further flight, replace the bolt with a serviceable bolt in accordance with the Accomplishment Instructions of the service bulletin.
(2) Install a tiewrap through the lower bolts of the stabilizer control unit, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF10027091, dated August 31, 2007. FAA AD Differences

Note: 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, International Branch, ANM116, Transport Airplane Directorate, 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: Tom Rodriguez, Aerospace Engineer, International Branch, ANM116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, WA 980573356; telephone (425) 2271137; fax (425) 2271149. 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 FAAapproved. Corrective actions are considered FAAapproved 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, 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 EASA Airworthiness Directive 20070287, dated November 15,
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2007; and Fokker Service Bulletin SBF10027091, dated August 31, 2007; for related information.
Material Incorporated by Reference
(i) You must use Fokker Service Bulletin SBF10027091, dated August 31, 2007, 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 Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE NieuwVennep, the Netherlands; telephone +31 (0)252627350; fax +31 (0)252627211; email
technicalservices.fokkerservices@stork.com; Internet http:// www.myfokkerfleet.com.
(3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 7416030, or go to: http://www.archives.gov/federalregister/cfr/ibr locations.html.

Issued in Renton, Washington, on October 9, 2008. Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E825755 Filed 111908; 8:45 am]
BILLING CODE 491013P

FOR FURTHER INFORMATION CONTACT Tom Rodriguez, Aerospace Engineer, International Branch, ANM116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, WA 980573356; telephone (425) 2271137; fax (425) 2271149.