Official Marks, Devices and Certificates, 12277 [06-55508]
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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 https://
dms.dot.gov and follow the instructions
for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://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 https://
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]
========================================================================
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
