Federal Register / Vol. 69, No. 194 / Thursday, October 7, 2004 / Rules and Regulations 60081

(b) The adjustments displayed in 

paragraph (a) of this section apply to 

acts occurring beginning on November 

1, 2004.

[FR Doc. 04–22537 Filed 10–6–04; 8:45 am] 

BILLING CODE 7535–01–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) 2004–19–04, 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 the 

AD number as AD 2004–19–04. The 

correct AD number is 2004–19–01. This 

action corrects the regulatory text.

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 2004–19–04, Amendment 39–13795 

(69 FR 55943, September 17, 2004), 

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 the 

AD number as 2004–19–04. The correct 

AD number is AD 2004–19–01. This 

correction is needed to ensure that the 

correct AD number is entered in the 

logbook and to eliminate 

misunderstanding in the field.

Correction of Publication

■ Accordingly, the publication of 

September 17, 2004 (69 FR 55943), of 

Amendment 39–13795; AD 2004–19–04, 

which was the subject of FR Doc. 04–

20774, is corrected as follows:

§ 39.13 [Corrected]

■ On page 55945, in section 39.13 

[Amended], replace 2004–19–04 with 

2004–19–01. 

Action is taken herein to correct this 

reference in AD 2004–19–04 and to add 

this AD correction to section 39.13 of 

the Federal Aviation Regulations (14 

CFR 39.13). 

The effective date remains November 

1, 2004.

Issued in Kansas City, Missouri, on 

September 23, 2004. 

David R. Showers, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service.

[FR Doc. 04–21814 Filed 10–6–04; 8:45 am] 

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. 97–NM–235–AD; Amendment 

39–12861; AD 2002–16–22] 

RIN 2120–AA64 

Airworthiness Directives; Boeing 

Model 727 Series Airplanes Modified in 

Accordance With Supplemental Type 

Certificate SA1444SO, SA1509SO, 

SA1543SO, or SA1896SO

AGENCY: Federal Aviation 

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This document corrects an 

error that appeared in airworthiness 

directive (AD) 2002–16–22 (final rule, 

correction) that was published in the 

Federal Register on August 16, 2004 (69 

FR 50299). The error resulted in an 

incorrect reference to certain 

supplemental type certificates. This AD 

is applicable to certain Boeing Model 

727 series airplanes that have been 

converted from a passenger- to a cargocarrying (‘‘freighter’’) configuration. 

This AD requires, among other actions, 

installation of a fail-safe hinge, 

redesigned main deck cargo door 

warning and power control systems, and 

9g crash barrier.

DATES: Effective September 19, 2002.

FOR FURTHER INFORMATION CONTACT: M. 

Hassan Amani, Aerospace Engineer, 

Airframe Branch, ACE–117A, FAA, 

Atlanta Aircraft Certification Office, 

One Crown Center, 1895 Phoenix 

Boulevard, suite 450, Atlanta, Georgia 

30349; telephone (770) 703–6080; fax 

(770) 703–6097.

SUPPLEMENTARY INFORMATION:

Airworthiness Directive (AD) 2002–16–

22, amendment 39–12861, applicable to 

certain Boeing Model 727 series 

airplanes that have been converted from 

a passenger- to a cargo-carrying 

(‘‘freighter’’) configuration, was 

published in the Federal Register on 

August 15, 2002 (67 FR 53434). That AD 

requires, among other actions, 

installation of a fail-safe hinge, 

redesigned main deck cargo door 

warning and power control systems, and 

9g crash barrier. 

On August 16, 2004, we issued a final 

rule, correction (69 FR 50299, August 

16, 2004), to AD 2002–16–22. The final 

rule, correction corrects an error that 

resulted in an incorrect reference to a 

supplemental type certificate. As 

published, the title of final rule, 

correction states ‘‘Boeing Model 727 

Series Airplanes Modified with 

Supplemental Type Certificate 

SA1767S0 or SA1768SO.’’ However, the 

correct applicable supplemental type 

certificates (STC) are SA1444SO, 

SA1509SO, SA1543SO, or SA1896SO, 

as specified in AD 2002–16–22. 

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 

September 19, 2002.

§ 39.13 [Corrected]

■ On page 50299, in the second column, 

the title of AD 2002–16–22 is corrected 

to read as follows:

* * * * *

Airworthiness Directives; Boeing 

Model 727 Series Airplanes Modified in 

Accordance with Supplemental Type 

Certificate SA1444SO, SA1509SO, 

SA1543SO, or SA1896SO.

* * * * *