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

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 require 

obtaining 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, 

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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. 

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