75236 Federal Register / Vol. 69, No. 241 / Thursday, December 16, 2004 / Rules and Regulations 

(2) The incorporation by reference of the service information listed in Table 6 of this AD was approved previously by the Director of 

the Federal Register as of December 11, 1996 (61 FR 57311, November 6, 1996).

TABLE 6.—MATERIAL PREVIOUSLY INCORPORATED BY REFERENCE

Shorts service bulletin Revision level Date 

SD3 SHERPA–32–2 ............................................................................................................................ Original .................... September 22, 1995. 

SD360–32–34 ...................................................................................................................................... Original .................... September 22, 1995. 

Issued in Renton, Washington, on 

December 1, 2004. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service.

[FR Doc. 04–27331 Filed 12–15–04; 8:45 am] 

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39

[Docket No. 2003–CE–40–AD; Amendment 

39–13795; AD 2004–19–01] 

RIN 2120–AA64

Airworthiness Directives; Cessna 

Aircraft Company 120, 140, 140A, 150, 

F150, 170, 172, F172, FR172, P172D, 

175, 177, 180, 182, 185, A185E, 190, 

195, 206, P206, U206, TP206, TU206, 

207, T207, 210, T210, 336, 337, and 

T337 Series Airplanes

AGENCY: Federal Aviation 

Administration (FAA), DOT.

ACTION: Final rule; correction.

SUMMARY: This document makes a 

correction to Airworthiness Directive 

(AD) 2004–19–01, which was published 

in the Federal Register on September 

17, 2004 (69 FR 55943), and applies to 

certain Cessna Aircraft Company 

(Cessna) 120, 140, 140A, 150, F150, 170, 

172, F172, FR172, P172D, 175, 177, 180, 

182, 185, A185E, 190, 195, 205, 205A, 

206, P206, P206E, TP206A, TU206, 

TU206E, U206, U206E, 207, T207, 210, 

T210, 336, 337, and T337 series 

airplanes. We incorrectly referenced a 

serial number for the affected Model 

T337B airplanes in the applicability 

section as 37–0570. The correct serial 

number is 337–0570. This action 

corrects the applicability section of AD 

2004–19–01, Amendment 39–13795.

DATES: The effective date of this AD 

remains November 1, 2004.

FOR FURTHER INFORMATION CONTACT: Gary 

D. Park, Aerospace Engineer, FAA, 

Wichita Aircraft Certification Office, 

1801 Airport Road, Room 100, MidContinent Airport, Wichita, Kansas 

67209; telephone: (316) 946–4123; 

facsimile: (316) 946–4107.

SUPPLEMENTARY INFORMATION: 

Discussion 

On September 8, 2004, FAA issued 

AD 2004–19–01, Amendment 39–13795 

(69 FR 55943, September 17, 2004) (as 

corrected in the publication of October 

7, 2004 (69 FR 60081), which applies to 

certain Cessna 120, 140, 140A, 150, 

F150, 170, 172, F172, FR172, P172D, 

175, 177, 180, 182, 185, A185E, 190, 

195, 205, 205A, 206, P206, P206E, 

TP206A, TU206, TU206E, U206, U206E, 

207, T207, 210, T210, 336, 337, and 

T337 series airplanes. This AD 

supersedes AD 86–26–04 with a new 

AD that requires you to inspect and, if 

necessary, modify the pilot/co-pilot 

upper shoulder harness adjusters that 

have certain Cessna accessory kits 

incorporated. 

Need for the Correction 

The FAA incorrectly referenced a 

serial number for Model T337B 

airplanes in the applicability section of 

AD 2004–19–01. The correct serial 

number range for the affected Model 

T337B airplanes is 337–0001, 337–0470, 

337–0526 through 337–0568, and 337–

0570 through 337–0755. This correction 

is needed to prevent confusion in the 

field regarding the FAA’s intent of the 

AD applicability. 

Correction of Publication 

Accordingly, the publication of 

September 17, 2004 (69 FR 55943), of 

AD 2004–19–01; Amendment 39–13795; 

which was the subject of FR Doc. 04–

20774 (as corrected in the publication of 

October 7, 2004 (69 FR 60081), which 

was the subject of FR Doc. 04–21814), 

is corrected as follows:

§ 39.13 [Corrected]

■ On page 55946, in § 39.13 [Amended], 

2., replace paragraph (c)(129) with the 

following text:

‘‘(129) T337B 337–0001, 337–0470, 337–

0526 through 337–0568, and 337–0570 

through 337–0755’’.

Action is taken herein to correct this 

reference in AD 2004–19–01 and to add 

this AD correction to § 39.13 of the 

Federal Aviation Regulations (14 CFR 

39.13). 

The effective date remains November 

1, 2004.

Issued in Kansas City, Missouri, on 

December 7, 2004. 

Sandra J. Campbell, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service.

[FR Doc. 04–27513 Filed 12–15–04; 8:45 am] 

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39

[Docket No. FAA–2004–18744; Directorate 

Identifier 2004–CE–24–AD; Amendment 39–

13910; AD 2004–25–22] 

RIN 2120–AA64

Airworthiness Directives; Great Lakes 

Aircraft Company, LLC, Models 2T–

1A–1 and 2T–1A–2 Airplanes

AGENCY: Federal Aviation 

Administration (FAA), DOT.

ACTION: Final rule.

SUMMARY: The FAA supersedes 

Airworthiness Directive (AD) 79–20–08, 

which applies to all Great Lakes Aircraft 

Company, LLC, (Great Lakes) Models 

2T–1A–1 and 2T–1A–2 airplanes with a 

Lycoming IO–360–B1F6 or AIO–360–

B1G6 engine installed. AD 79–20–08 

currently requires you to inspect the 

engine induction system and the 

alternate air door for any signs of 

damage and repairing or replacing any 

damaged components. AD 79–20–08 

also requires you to inspect the 

induction system for the presence of a 

drain fitting. If the drain fitting is 

blocked, restricted, or does not exist, AD 

79–20–08 requires you to clear the 

fitting or drill a hole in the elbow at the 

fitting location. This AD is the result of 

the FAA inadvertently omitting 

Lycoming engine AEIO–360–B1G6 from 

the applicability section of AD 79–20–

08. Consequently, this AD retains the 

actions required in AD 79–20–08 and 

adds Lycoming engine AEIO–360–B1G6 

to the applicability section. We are 

issuing this AD to prevent the aircraft 

induction system from becoming 

blocked or restricted, which could result