Federal Register / Vol. 69, No. 206 / Tuesday, October 26, 2004 / Rules and Regulations 62399

Actions Compliance Procedures 

(2) Replace any cracked or corroded inboard 

aileron hinge bracket.

(i) If replacement is with a bracket made from 

magnesium, do the 100-hour TIS interval repetitive inspections as required in paragraph 

(e)(1) of this AD.

(ii) If replacement is with an FAA-approved 

bracket that is made from aluminum, then no 

further inspections are necessary. These can 

be Cessna parts or non-Cessna parts.

Prior to further flight after any inspection 

where any cracked or corroded bracket is 

found. You may terminate the repetitive inspections required by this AD when all 

brackets are replaced with FAA-approved 

brackets that are made with aluminum, as 

specified in the service information.

Use the procedures included with the FAA-approved replacement and the FAA-approved 

maintenance manual. This could include 

Cessna parts, supplemental type certificate 

(STC) parts, or parts manufacturer approval 

(PMA) parts, etc. 

(3) As terminating action for the repetitive inspections, you may replace all inboard aileron hinge brackets with FAA-approved brackets that are made from aluminum (as specified in paragraph (e)(2)(ii) of this AD) regardless if any corrosion or crack is found.You may do this replacement at any time, but 

you must replace any corroded or cracked 

bracket prior to further flight after the applicable inspection where any corrosion or 

crack is found.

Use the procedures included with the approved replacement and the FAA-approved 

maintenance manual. This could include 

Cessna parts, STC parts, or PMA parts, 

etc. 

May I Request an Alternative Method of 

Compliance? 

(f) You may request a different method of 

compliance or a different compliance time 

for this AD by following the procedures in 14 

CFR 39.19. Unless FAA authorizes otherwise, 

send your request to your principal 

inspector. The principal inspector may add 

comments and will send your request to the 

Manager, Wichita Aircraft Certification 

Office, FAA. For information on any already 

approved alternative methods of compliance, 

contact Gary D. Park, Aerospace Engineer, 

FAA, Wichita Aircraft Certification Office, 

1801 Airport Road, Room 100, Mid-Continent 

Airport, Wichita, Kansas 67209; telephone: 

(316) 946–4123; facsimile: (316) 946–4107. 

Does This AD Incorporate Any Material by 

Reference? 

(g) You must do the inspections required 

by this AD following the instructions in 

Cessna Single Engine Service Bulletin 

SEB04–1, dated April 26, 2004. The Director 

of the Federal Register approved the 

incorporation by reference of this service 

bulletin in accordance with 5 U.S.C. 552(a) 

and 1 CFR part 51. To get a copy of this 

service information, contact Cessna Aircraft 

Company, Product Support P.O. Box 7706, 

Wichita, Kansas 67277; telephone: (316) 517–

5800; facsimile: (316) 942–9006. To review 

copies of this service information, go to the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, go 

to: http://www.archives.gov/federal_register/

code_of_federal_regulations/

ibr_locations.html or call (202) 741–6030. To 

view the AD docket, go to the Docket 

Management Facility; U.S. Department of 

Transportation, 400 Seventh Street, SW., 

Nassif Building, Room PL–401, Washington, 

DC 20590–001 or on the Internet at http://

dms.dot.gov. The docket number is FAA–

2004–18033.

Issued in Kansas City, Missouri, on 

October 13, 2004. 

William J. Timberlake, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service.

[FR Doc. 04–23729 Filed 10–25–04; 8:45 am] 

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39

[Docket No. 2003–NM–90–AD; Amendment 

39–13804; AD 2004–19–10] 

RIN 2120–AA64

Airworthiness Directives; Boeing 

Model 737–100, –200, –200C, –300, 

–400, and –500 Series Airplanes

AGENCY: Federal Aviation 

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This document corrects a 

typographical error that appeared in 

airworthiness directive (AD) 2004–19–

10 that was published in the Federal 

Register on September 27, 2004 (69 FR 

57632). The typographical error resulted 

in the omission of the AD number in 

one location of the document. This AD 

is applicable to certain Boeing Model 

737–100, –200, –200C, –300, –400, and 

–500 series airplanes. This AD requires 

repetitive inspections for corrosion and 

cracking of the pivot hinge pins of the 

horizontal stabilizer, certain follow-on 

inspections, and replacement of the 

hinge pins with new or serviceable pins 

if necessary.

DATES: Effective November 1, 2004.

FOR FURTHER INFORMATION CONTACT:

Nancy Marsh, Aerospace Engineer, 

Airframe Branch, ANM–120S, FAA, 

Seattle Aircraft Certification Office, 

1601 Lind Avenue, SW., Renton, 

Washington 98055–4056; telephone 

(425) 917–6440; fax (425) 917–6590.

SUPPLEMENTARY INFORMATION:

Airworthiness Directive (AD) 2004–19–

10, amendment 39–13804, applicable to 

certain Boeing Model 737–100, –200, 

–200C, –300, –400, and –500 series 

airplanes, was published in the Federal 

Register on September 27, 2004 (69 FR 

57632). That AD requires repetitive 

inspections for corrosion and cracking 

of the pivot hinge pins of the horizontal 

stabilizer, certain follow-on inspections, 

and replacement of the hinge pins with 

new or serviceable pins if necessary. 

As published, the AD number is 

missing in the Product Identification 

line in the regulatory text of the AD. The 

correct AD number is 2004–19–10. The 

AD number is referenced correctly 

throughout the remainder of the AD. 

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 

November 1, 2004.

§ 39.13 [Corrected]

■ On page 57634, in the third column, 

the Product Identification line of AD 

2004–19–10 is corrected to read as 

follows:

* * * * *

2004–19–10 Boeing: Amendment 39–13804. 

Docket 2003–NM–90–AD.

* * * * *

Issued in Renton, Washington, on October 

18, 2004. 

Kalene C. Yanamura, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service.

[FR Doc. 04–23928 Filed 10–25–04; 8:45 am] 

BILLING CODE 4910–13–P