## 23579 Federal Register / Vol. 75, No. 85 / Tuesday, May 4, 2010 / Rules and Regulations

left and right rear attach bolts following instruction ‘‘ 5. Rear Attach Bolt Replacement, ’’ of Gippsland Aeronautics Mandatory Service Bulletin SB–GA8–2002– 02, Issue 5, dated November 13, 2008. Reworking the mating surfaces by spotfacing is no longer acceptable. If the mating surfaces are damaged, not square, or were previously reworked by spotfacing the surface, before further flight, replace the parts as specified in Gippsland Aeronautics Mandatory Service Bulletin SB–GA8–2002–02, Issue 5, dated November 13, 2008.

(2) Within the next 10 hours TIS after May 10, 2010 (the effective date of this AD) and repetitively thereafter at intervals not to exceed 100 hours TIS or 12 months, whichever occurs first, for all aircraft:

(i) Inspect the horizontal stabilizer externally following instruction ‘‘ 2. External Inspection (Lower flange, Stabilizer rear spar), ’’ of Gippsland Aeronautics Mandatory Service Bulletin SB–GA8–2002–02, Issue 5, dated November 13, 2008; and

(ii) Inspect the horizontal stabilizer internally following instruction ‘‘ 4. Internal Inspection, ’’ of Gippsland Aeronautics Mandatory Service Bulletin SB–GA8–2002– 02, Issue 5, dated November 13, 2008.

(3) If during the inspection required by paragraph (g)(2) of this AD any excessive local deflection or movement of the lower skin surrounding the lower pivot attachment, cracking, or working (loose) rivet is found, before further flight, obtain an FAA-approved repair scheme from the manufacturer and incorporate this repair scheme. Due to FAA policy, the repair scheme for crack damage must include an immediate repair of the crack, not a repetitive inspection. Continued operational flight with un-repaired crack damage is not permitted.

FAA AD Differences

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

(1) ‘‘ Requirement: 1. Daily Inspection (Stabilizer attach bolt) ’’ of the service information requires a daily inspection of the stabilizer attach bolt. The daily inspection is not a requirement of this AD. Instead of the daily inspection, we require you to perform, within 10 hours TIS, ‘‘ Requirement 3. Rear Pivot Attachment Inspection ’’ and

‘‘Requirement 5. Rear Attachment Bolt Replacement’’ of the service information. Compliance with requirement 3. and 5. is a terminating action for the daily inspection, and we are requiring these within 10 hours TIS after the effective date of this AD.

(2) ‘‘ Requirement: 2. External Inspection (Lower flange, Stabilizer rear spar) ’’ of the service information does not specify any action if excessive local deflection or movement of lower skin, cracking, or working (loose) rivet is found. We requireobtaining and incorporating an FAAapproved repair scheme from the manufacturer before further flight.

(3) The MCAI does not state if further flight with known cracks is allowed. FAA policy is to not allow further flight with known cracks in critical structure. We require that if any cracks are found when accomplishing the inspection required in paragraphs (f)(2) and (g)(2) of this AD, you must repair the cracks before further flight. (4) The service information does not state that parts with spotfaced nut and bolt mating surfaces require replacement. However, the service information no longer allows reworking of the mating surfaces by spotfacing. We require that if any nut and bolt surfaces were previously reworked by spotfacing, you must replace the parts.

(5) The service information has not been revised to include Model GA8–TC320 airplanes; however, the procedures still apply to this model, and actions must be done following the service information.

Other FAA AD Provisions

(h) 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: Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4059; 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 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 (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

(i) Refer to MCAI Civil Aviation Safety Authority AD No. AD/GA8/5, Amdt 3, dated April 9, 2010; and Gippsland Aeronautics Mandatory Service Bulletin SB–GA8–2002– 02, Issue 5, dated November 13, 2008, for related information.
Material Incorporated by Reference

(j) You must use Gippsland Aeronautics Mandatory Service Bulletin SB–GA8–2002– 02, Issue 5, dated November 13, 2008, to do the actions required by this AD, unless the AD specifies otherwise.

(1) On March 2, 2009 (74 FR 8159; February 24, 2009), the Director of the Federal Register previously approved the incorporation by reference of Gippsland Aeronautics Mandatory Service Bulletin SB– GA8–2002–02, Issue 5, dated November 13,
2008.

(2) For service information identified in this AD, contact Gippsland Aeronautics, Attn: Technical Services, P.O. Box 881, Morwell Victoria 3840, Australia; telephone: + 61 03 5172 1200; fax: +61 03 5172 1201; Internet: http://www.gippsaero.com. (3) 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.

(4) 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 April 20, 2010. Steven W. Thompson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010–10220 Filed 5–3–10; 8:45 am]

**BILLING CODE 4910–13–P**



### DEPARTMENT OF TRANSPORTATION

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. 2000–NM–418–AD; Amendment 39–12964; AD 2002–23–20]** 

**RIN 2120–AA64**



### Airworthiness Directives; DASSAULT **AVIATION Model FALCON 900EX and MYSTERE–FALCON 900 Airplanes** 

**AGENCY** 

### : Federal Aviation Administration, DOT.

**ACTION** 

### : Final rule; correction.

**SUMMARY** 

### : This document corrects a typographical error that appeared in airworthiness directive (AD) 2002–23– 20 that was published in the Federal Register on November 29, 2002 (67 FR 71098). The typographical error resulted in an incorrect part number. This AD is applicable to Model FALCON 900EX and MYSTERE–FALCON 900 airplanes. This AD requires repetitive operational tests of the flap asymmetry detection system to verify proper functioning, and repair if necessary; repetitive replacement of the inboard flap jackscrews with new or reconditioned jackscrews; and repetitive measurement of the screw/nut play of the jackscrews on the inboard and outboard flaps to detect discrepancies, and corrective action if necessary. This AD also requires revision of the Airplane Flight Manual.

**DATES** 

### : This correction is effective May 4, 2010. The effective date of AD 2002– 23–20 remains January 3, 2003.

**FOR FURTHER INFORMATION CONTACT** 

### : Tom Rodriguez, Aerospace Engineer,


## 23580 Federal Register / Vol. 75, No. 85 / Tuesday, May 4, 2010 / Rules and Regulations

International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057–3356; telephone (425) 227–1137; fax (425) 227–1149.

**SUPPLEMENTARY INFORMATION** 

### : AD 2002– 23–20, amendment 39–12964, applicable to Model FALCON 900EX and MYSTERE–FALCON 900 airplanes, was published in the Federal Register on November 29, 2002 (67 FR 71098). That AD requires repetitive operational tests of the flap asymmetry detection system to verify proper functioning, and repair if necessary; repetitive replacement of the inboard flap jackscrews with new or reconditioned jackscrews; and repetitive measurement of the screw/nut play of the jackscrews on the inboard and outboard flaps to detect discrepancies, and corrective action if necessary. That AD also requires revision of the Airplane Flight Manual.

As published, paragraph (e)(1) of the AD specifies in error jackscrew part number 5818–1 Amdt A. P/N 5818–1 Amdt A. does not exist. The correct part number is 5318–1 Amdt A.

Since no other part of the regulatory information has been changed, the final rule is not being republished in the Federal Register.

The effective date of this AD remains January 3, 2003.

**§ 39.13 [Corrected]**

■ 

### On page 71101, in the first column, paragraph (e)(1) of AD 2002–23–20 is corrected to read as follows:

* * * * *

(1) The jackscrew has been reconditioned and reidentified as P/N 5318–1 Amdt A, in accordance with Dassault Service Bulletin AVIAC 5318– 27–01, dated September 16, 1999.

* * * * *

Issued in Renton, Washington, on April 22,

2010. Jeffrey E. Duven, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010–9943 Filed 5–3–10; 8:45 am]

**BILLING CODE 4910–13–P** 

### DEPARTMENT OF TRANSPORTATION

**Federal Aviation Administration**

**14 CFR Part 71**

**[Docket No. FAA–2009–1155; Airspace Docket No. 09–ACE–14]** 



### Amendment of Class E Airspace; **Mapleton, IA**

**AGENCY** 

### : Federal Aviation Administration (FAA), DOT.

**ACTION** 

### : Final rule.

**SUMMARY** 

### : This action amends Class E airspace for Mapleton, IA, adding additional controlled airspace to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAPs) at James G. Whiting Memorial Field Airport, Mapleton, IA. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.

**DATES** 

### : Effective date 0901 UTC, July 29, 2010. The Director of the Federal Register approves this incorporation by reference action under 1 CFR part 51, subject to the annual revision of FAA Order 7400.9 and publication of conforming amendments.

**FOR FURTHER INFORMATION CONTACT** 

### : Scott Enander, Central Service Center, Operations Support Group, Federal Aviation Administration, Southwest Region, 2601 Meacham Blvd., Fort Worth, TX 76137; telephone (817) 321–
7716.

**SUPPLEMENTARY INFORMATION** 

### : History

On February 10, 2010, the FAA published in the Federal Register a notice of proposed rulemaking to amend Class E airspace for Mapleton, IA, reconfiguring controlled airspace at James G. Whiting Memorial Field Airport (75 FR 6595) Docket No. FAA– 2009–1155. Interested parties were invited to participate in this rulemaking effort by submitting written comments on the proposal to the FAA. No comments were received. Class E airspace designations are published in paragraph 6005 of FAA Order 7400.9T signed August 27, 2009, and effective September 15, 2009, which is incorporated by reference in 14 CFR 71.1. The Class E airspace designations listed in this document will be published subsequently in the Order.

The Rule

This action amends Title 14 Code of Federal Regulations (14 CFR) part 71 by amending Class E airspace for the Mapleton, IA area, adding additional controlled airspace extending upward from 700 feet above the surface to accommodate SIAPs at James G. Whiting Memorial Field Airport. This action is necessary for the safety and management of IFR operations at the airport.

The FAA has determined that this regulation only involves an established body of technical regulations for which frequent and routine amendments are necessary to keep them operationally current. Therefore, this regulation: (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) does not warrant preparation of a regulatory evaluation as the anticipated impact is so minimal. Since this is a routine matter that will only affect air traffic procedures and air navigation, it is certified that this rule, when promulgated, will not have a significant economic impact on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

The FAA’s authority to issue rules regarding aviation safety is found in Title 49 of the U.S. Code. Subtitle 1, section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the agency’s authority. This rulemaking is promulgated under the authority described in subtitle VII, part A, subpart I, section 40103. Under that section, the FAA is charged with prescribing regulations to assign the use of airspace necessary to ensure the safety of aircraft and the efficient use of airspace. This regulation is within the scope of that authority as it amends controlled airspace at James G. Whiting Memorial Field Airport, Mapleton, IA. List of Subjects in 14 CFR Part 71

Airspace, Incorporation by reference, Navigation (air). Adoption of the Amendment

■ 

### In consideration of the foregoing, the Federal Aviation Administration amends 14 CFR part 71 as follows:

**PART 71—DESIGNATION OF CLASS A, B, C, D, AND E AIRSPACE AREAS; AIR**  **TRAFFIC SERVICE ROUTES; AND REPORTING POINTS** 

■ 

### 1. The authority citation for 14 CFR part 71 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40103, 40113, 40120; E.O. 10854, 24 FR 9565, 3 CFR, 1959– 1963 Comp., p. 389.