### 19313 Federal Register / Vol. 69, No. 71 / Tuesday, April 13, 2004 / Rules and Regulations Issued in Renton, Washington, on March 31, 2004. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04 – 8355 Filed 4 – 12 – 04; 8:45 am] **BILLING CODE 4910 –**  **13 –**  **P DEPARTMENT OF TRANSPORTATION**  **Federal Aviation Administration 14 CFR Part 39**  **[Docket No. 2002 –**  **NM –**  **174 –** **AD; Amendment 39**  **– 13483; AD 2004**  **– 04**  **– 03**  **RIN 2120 –** **AA64 Airworthiness Directives; Boeing**  **Model 737 –**  **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 – 04 – 03 that was published in the Federal Register on February 18, 2004 (69 FR 7565). The typographical error resulted in a reference to an incorrect effective date in the compliance time specified in Table 1 of the AD for Group 1 airplanes. This AD is applicable to certain Boeing Model 737 series airplanes. This AD requires a one-time general visual inspection of the seat locks and seat tracks of the flightcrew seats to ensure that the seats lock in position and to verify that lock nuts and bolts of adequate length are installed on the rear track lock bracket, and corrective action, if necessary. **DATES :**  Effective March 24, 2004. **FOR FURTHER INFORMATION CONTACT :**  Shannon Lennon, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM– 150S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington; telephone (425) 917 – 6436; fax (425) 917 – 6590. **SUPPLEMENTARY INFORMATION :**  Airworthiness Directive (AD) 2004 – 04 – 03, amendment 39 – 13483, applicable to certain Boeing Model 737 series airplanes, was published in the Federal Register on February 18, 2004 (69 FR 7565). That AD requires a one-time general visual inspection of the seat locks and seat tracks of the flightcrew seats to ensure that the seats lock in position and to verify that lock nuts and bolts of adequate length are installed on the rear track lock bracket, and corrective action, if necessary.

As published, that final rule incorrectly specifies ‘‘ September 26, 2001 ’’ as the effective date for AD 2000 – 10 – 21 in the compliance time specified for Group 1 airplanes in Table 1 of that final rule. The correct effective date of AD 2000 – 10 – 21 is ‘‘June 12, 2000. ’’ It was the FAA ’ s intent that operators use June 12, 2000, to determine the compliance time for Group 1 airplanes as specified in Table 1 of that final rule, as evidenced by the explanatory parenthetical reference ‘‘ (the effective date of AD 2000 – 10 – 21, amendment 39 – 11745). ’’

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 March 24, 2004. **§ 39.13 [Corrected]** 

On page 7566, the second column of Table 1 of AD 2004 – 04 – 03 is corrected to read as follows: * * * * * 

### T ABLE 

### 1. — C OMPLIANCE 

### T IME

### /S ERVICE 

### B ULLETIN Airplanes —Compliance time —Service bulletin —For Group 1 airplanes listed in Boeing Alert Service Bulletin 737 –25A1363, Revision 1, dated March 28, 2002. Within 90 days after June 12, 2000 (the effective date of AD 2000 – 10 – 21, amendment 39 – 11745). Boeing Alert Service Bulletin 737 – 25A1363, dated November 5, 1998.For Group 2 airplanes listed in Boeing Alert Service Bulletin 737 –25A1363, Revision 1, dated March 28, 2002. Within 90 days after the effective date of this AD. Boeing Alert Service Bulletin 737 – 25A1363, Revision 1, dated March 28, 2002. * * * * *

Issued in Renton, Washington, on April 1, 2004. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04 – 8296 Filed 4 – 12 – 04; 8:45 am] **BILLING CODE 4910 –**  **13 –**  **P DEPARTMENT OF TRANSPORTATION**  **Federal Aviation Administration 14 CFR Part 39**  **[Docket No. 2004 –**  **NM –**  **03 –** **AD; Amendment 39**  **– 13514; AD 2004**  **– 05**  **– 19]**  **RIN 2120 –** **AA64 Airworthiness Directives; Boeing**  **Model 737 –**  **600, –** **700, –** **700C, –**  **800, and**

**– 900 Series Airplanes**  **AGENCY :**  Federal Aviation Administration, DOT. **ACTION :**  Final rule; correction. **SUMMARY :**  This document corrects an error that appeared in airworthiness directive (AD) 2004 – 05 – 19 that was published in the Federal Register on March 9, 2004 (69 FR 10921). The error resulted in the omission of the phrase ‘‘ whichever occurs first ’’ in a certain grace period for the initial compliance time. This AD is applicable to all Boeing Model 737 – 600, – 700, – 700C, – 800, and

– 900 series airplanes. This AD requires an inspection of the rear spar attach pins and front spar attach bolts that attach the horizontal stabilizers to the horizontal stabilizer center section for damage; and follow-on or corrective actions, as applicable. **DATES :**  Effective March 24, 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 – 05 – 19, amendment 39 – 13514, applicable to all Boeing Model 737 – 600, – 700, – 700C,

– 800, and – 900 series airplanes, was VerDate mar<24>2004 15:13 Apr 12, 2004 Jkt 203001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\13APR1.SGM 13APR1