Official Marks, Devices and Certificates, 12277 [06-55508]

Download as PDF 12277 Rules and Regulations Federal Register Vol. 71, No. 47 Friday, March 10, 2006 This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. Prices of new books are listed in the first FEDERAL REGISTER issue of each week. DEPARTMENT OF AGRICULTURE Food Safety and Inspection Service 9 CFR Part 312 Official Marks, Devices and Certificates CFR Correction In Title 9 of the Code of Federal Regulations, part 200 to end, revised as of January 1, 2006, the illustration on page 144 contained in § 312.8(a), should be interchanged with the illustration on page 145 contained in § 312.10. [FR Doc. 06–55508 Filed 3–9–06; 8:45 am] BILLING CODE 1505–01–D DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2006–24110; Directorate Identifier 2006–NM–020–AD; Amendment 39–14508; AD 2006–05–11] RIN 2120–AA64 Airworthiness Directives; Bombardier Model CL–600–2B19 (Regional Jet Series 100 & 440) Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; request for comments. rwilkins on PROD1PC63 with RULES AGENCY: SUMMARY: The FAA is superseding an existing airworthiness directive (AD) that applies to certain Bombardier Model CL–600–2B19 (Regional Jet Series 100 & 440) airplanes. The existing AD currently requires revising the airworthiness limitations section of the Instructions for Continued Airworthiness of the aircraft maintenance manual (AMM) by incorporating procedures for repetitive VerDate Aug<31>2005 19:15 Mar 09, 2006 Jkt 208001 functional tests of the pilot input lever of the pitch feel simulator (PFS) units. This AD requires new repetitive functional tests of the pilot input lever of the PFS unit, and corrective actions if necessary. After initiating the new tests, this AD also requires removal of the existing procedures for the repetitive functional tests from the AMM. This AD results from a report that the shear pin located in the input lever of two PFS units failed due to fatigue. We are issuing this AD to prevent undetected failure of the shear pin of both PFS units simultaneously, which could result in loss of pitch feel forces and consequent reduced control of the airplane. DATES: This AD becomes effective March 27, 2006. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of March 27, 2006. On February 13, 2004 (69 FR 4234, January 29, 2004), the Director of the Federal Register approved the incorporation by reference of Bombardier Temporary Revision 2B– 1784, dated October 24, 2003, to the CL– 600–2B19 Canadair Regional Jet Maintenance Requirements Manual, Part 2, Appendix B, ‘‘Airworthiness Limitations.’’ We must receive any comments on this AD by May 9, 2006. ADDRESSES: Use one of the following addresses to submit comments on this AD. • DOT Docket Web site: Go to http:// dms.dot.gov and follow the instructions for sending your comments electronically. • Government-wide rulemaking Web site: Go to http://www.regulations.gov and follow the instructions for sending your comments electronically. • Mail: Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., Nassif Building, Room PL–401, Washington, DC 20590. • Fax: (202) 493–2251. • Hand Delivery: Room PL–401 on the plaza level of the Nassif Building, 400 Seventh Street SW., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Contact Bombardier, Inc., Canadair, Aerospace Group, P.O. Box 6087, Station Centre-ville, Montreal, Quebec H3C 3G9, Canada, for service information identified in this AD. You may examine the contents of the AD docket on the Internet at http:// PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 dms.dot.gov, or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., Room PL–401, on the plaza level of the Nassif Building, Washington, DC. This docket number is FAA–2006– 24110; the directorate identifier for this docket is 2006–NM–020–AD. FOR FURTHER INFORMATION CONTACT: Dan Parrillo, Aerospace Engineer, Systems and Flight Test Branch, ANE–172, New York Aircraft Certification Office, FAA, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone (516) 228–7305; fax (516) 794–5531. SUPPLEMENTARY INFORMATION: Discussion On January 20, 2004, the FAA issued AD 2004–02–07, amendment 39–13442 (69 FR 4234, January 29, 2004). That AD applies to certain Bombardier Model CL–600–2B19 (Regional Jet Series 100 & 440) airplanes. That AD requires revising the airworthiness limitations section of the Instructions for Continued Airworthiness of the aircraft maintenance manual (AMM) by incorporating procedures for repetitive functional tests of the pilot input lever of the pitch feel simulator (PFS) units. That AD also requires an initial functional test of the pilot input lever of the PFS units, and corrective action if necessary. That AD resulted from a report that the shear pin located in the input lever of two PFS units failed due to fatigue. The actions specified in that AD are intended to prevent undetected failure of the shear pin of both PFS units simultaneously, which could result in loss of pitch feel forces and consequent reduced control of the airplane. Actions Since AD Was Issued Since we issued that AD, Transport Canada Civil Aviation (TCCA), which is the airworthiness authority for Canada, has informed us of a delay in developing a terminating modification. TCCA advises that Bombardier is encountering difficulties in developing a new, improved replacement input lever for the PFS units. The resulting delay is increasing the service time on the existing levers (and resulting risk exposure) to a level that is higher than TCCA anticipated when they issued Canadian Airworthiness Directive CF– 2003–26, dated November 14, 2003. The delay also results in more airplanes being delivered with the existing lever E:\FR\FM\10MRR1.SGM 10MRR1

Agencies

[Federal Register Volume 71, Number 47 (Friday, March 10, 2006)]
[Rules and Regulations]
[Page 12277]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-55508]



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Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
week.

========================================================================


Federal Register / Vol. 71, No. 47 / Friday, March 10, 2006 / Rules 
and Regulations

[[Page 12277]]



DEPARTMENT OF AGRICULTURE

Food Safety and Inspection Service

9 CFR Part 312


Official Marks, Devices and Certificates

CFR Correction

    In Title 9 of the Code of Federal Regulations, part 200 to end, 
revised as of January 1, 2006, the illustration on page 144 contained 
in Sec.  312.8(a), should be interchanged with the illustration on page 
145 contained in Sec.  312.10.

[FR Doc. 06-55508 Filed 3-9-06; 8:45 am]
BILLING CODE 1505-01-D