Federal Register / Vol. 70, No. 189 / Friday, September 30, 2005 / Rules and Regulations 57125 

SUMMARY: The FAA is correcting a 

typographical error in an existing 

airworthiness directive (AD) that was 

published in the Federal Register on 

September 15, 2005 (70 FR 54474). The 

error resulted in an inadvertent 

reference to a nonexistent paragraph. 

This AD applies to certain Boeing 

Model 747–100, 747–100B, 747–100B 

SUD, 747–200B, 747–200C, 747–200F, 

747–300, 747SR, and 747SP series 

airplanes. This AD requires repetitive 

detailed and ultrasonic inspections of 

the thrust links of the rear engine 

mounts for any crack or fracture and 

corrective actions if necessary. 

DATES: Effective September 30, 2005. 

ADDRESSES: The AD docket contains the 

proposed AD, comments, and any final 

disposition. You may examine the AD 

docket on the Internet at http:// 

dms.dot.gov, or in person at the Docket 

Management Facility office between 9 

a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. The 

Docket Management Facility office 

(telephone (800) 647–5227) is located on 

the plaza level of the Nassif Building at 

the U.S. Department of Transportation, 

400 Seventh Street SW., room PL–401, 

Washington, DC. This docket number is 

FAA–2005–22413; the directorate 

identifier for this docket is 2005–NM–

167–AD. 

FOR FURTHER INFORMATION CONTACT: Ivan 

Li, Aerospace Engineer, Airframe 

Branch, ANM–120S, FAA, Seattle 

Aircraft Certification Office, 1601 Lind 

Avenue, SW., Renton, Washington 

98055–4056; telephone (425) 917–6437; 

fax (425) 917–6590. 

SUPPLEMENTARY INFORMATION: On 

September 6, 2005, the FAA issued AD 

2005–19–06, amendment 39–14271 (70 

FR 54474, September 15, 2005), for 

certain Boeing Model 747–100, 747–

100B, 747–100B SUD, 747–200B, 747–

200C, 747–200F, 747–300, 747SR, and 

747SP series airplanes; equipped with 

Pratt & Whitney JT9D–3 and –7 series 

engines, except JT9D–70 engines. The 

AD requires repetitive detailed and 

ultrasonic inspections of the thrust links 

of the rear engine mounts for any crack 

or fracture and corrective actions if 

necessary. 

As published, the requirements of 

paragraph (h)(1) of the AD inadvertently 

reference doing the repetitive 

replacements ‘‘* * * at the applicable 

compliance time specified in paragraph 

(h)(1)(i) or (h)(2)(ii) of this AD.’’

However, there is no paragraph (h)(2)(ii) 

in the AD. We have removed reference 

to paragraph (h)(2)(ii) and replaced it 

with the correct reference to paragraph 

(h)(1)(ii). 

No other part of the regulatory 

information has been changed; 

therefore, the final rule is not 

republished in the Federal Register. 

The effective date of this AD remains 

September 30, 2005. 

§ 39.13 [Corrected] 

■ In the Federal Register of September 

15, 2005, on page 54476, in the third 

column, paragraph (h)(1) of AD 2005–

19–06 is corrected to read as follows: 

* * * * * 

(1) Replace the cracked thrust link 

with a new or overhauled thrust link in 

accordance with Part 2 of the service 

bulletin; except as provided by 

paragraph (i) of this AD. Repeat the 

replacement at the applicable 

compliance time specified in paragraph 

(h)(1)(i) or (h)(1)(ii) of this AD. 

* * * * * 

Issued in Renton, Washington, on 

September 26, 2005. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 05–19564 Filed 9–29–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–22405; Directorate 

Identifier 2002–NM–243–AD; Amendment 

39–14269; AD 2005–19–04] 

RIN 2120–AA64 

Airworthiness Directives; Airbus Model 

A340–200 and –300 Series Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting a 

typographical error in an existing 

airworthiness directive (AD) that was 

published in the Federal Register on 

September 14, 2005 (70 FR 54251). The 

error resulted in in an incorrect Docket 

No. This AD applies to certain Airbus 

Model A340–200 and –300 series 

airplanes. This AD requires revising the 

airplane flight manual to incorporate 

new procedures for the flightcrew to 

follow to correct miscalculation of the 

takeoff and accelerating or stopping 

distance of the airplane during a ferry 

flight under certain conditions. 

DATES: Effective September 29, 2005. 

ADDRESSES: The AD docket contains the 

proposed AD, comments, and any final 

disposition. You may examine the AD 

docket on the Internet at http:// 

dms.dot.gov, or in person at the Docket 

Management Facility office between 9 

a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. The 

Docket Management Facility office 

(telephone (800) 647–5227) is located on 

the plaza level of the Nassif Building at 

the U.S. Department of Transportation, 

400 Seventh Street SW., room PL–401, 

Washington, DC. This docket number is 

FAA–2005–22405; the directorate 

identifier for this docket is 2002–NM–

243–AD. 

FOR FURTHER INFORMATION CONTACT: Dan 

Rodina, Aerospace Engineer, 

International Branch, ANM–116, FAA, 

Transport Airplane Directorate, 1601 

Lind Avenue, SW., Renton, Washington 

98055–4056; telephone (425) 227–2125; 

fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: On 

September 6, 2005, the FAA issued AD 

2005–19–04, amendment 39–14269 (70 

FR 54251, September 14, 2005), for 

certain Airbus Model A340–200 and 

–300 series airplanes. The AD requires 

revising the airplane flight manual to 

incorporate new procedures for the 

flightcrew to follow to correct 

miscalculation of the takeoff and 

accelerating or stopping distance of the 

airplane during a ferry flight under 

certain conditions. 

As published, that AD specifies an 

incorrect Docket No. (i.e., FAA–2005–

20405) throughout preamble and the 

regulatory text of the AD. The correct 

Docket No. is FAA–2005–22405. 

No other part of the regulatory 

information has been changed; 

therefore, the final rule is not 

republished in the Federal Register. 

The effective date of this AD remains 

September 29, 2005. 

§ 39.13 [Corrected] 

■ In the Federal Register of September 

14, 2005, on page 54253, in the first 

column, paragraph 2. of PART 39—

AIRWORTHINESS DIRECTIVES of AD 

2005–19–04 is corrected to read as 

follows: 

* * * * * 

2005–19–04 Airbus: Amendment 39–14269. 

Docket No. FAA–2005–22405; 

Directorate Identifier 2002–NM–243–AD. 

* * * * * 

Issued in Renton, Washington, on 

September 26, 2005. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 05–19556 Filed 9–29–05; 8:45 am] 

BILLING CODE 4910–13–P