[Federal Register: February 18, 2004 (Volume 69, Number 32)]
[Rules and Regulations]
[Page 7555-7556]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr18fe04-6]
[[Page 7555]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002-NM-225-AD; Amendment 39-13479; AD 2004-03-35]
RIN 2120-AA64
Airworthiness Directives; Raytheon Model Beech 400A and 400T
Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to certain Raytheon Model Beech 400A and 400T series
airplanes, that requires an inspection to determine the part number of
the A194 roll trim printed circuit board (PCB), and replacement of
certain PCBs with improved parts. This action is necessary to prevent
intermittent sticking of the relays on the PCB in either the open or
closed position, which could result in an out-of-trim condition that
could require using considerable control wheel force to keep the wings
level, and consequent reduced controllability of the airplane. This
action is intended to address the identified unsafe condition.
DATES: Effective March 24, 2004.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of March 24, 2004.
ADDRESSES: The service information referenced in this AD may be
obtained from Raytheon Aircraft Company, Department 62, P.O. Box 85,
Wichita, Kansas 67201-0085. This information may be examined at the
Federal Aviation Administration (FAA), Transport Airplane Directorate,
Rules Docket, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA,
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100,
Mid-Continent Airport, Wichita, Kansas; or at the Office of the Federal
Register, 800 North Capitol Street, NW., Suite 700, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Philip Petty, Aerospace Engineer,
Systems and Propulsion Branch, ACE-116W, FAA, Wichita Aircraft
Certification Office, 1801 Airport Road, Room 100, Mid-Continent
Airport, Wichita, Kansas 67209; telephone (316) 946-4139; fax (316)
946-4407.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to include an airworthiness
directive (AD) that is applicable to certain Raytheon Model Beech 400A
and 400T series airplanes was published in the Federal Register on
November 4, 2003 (68 FR 62415). That action proposed to require an
inspection to determine the part number of the A194 roll trim printed
circuit board (PCB), and replacement of certain PCBs with improved
parts.
Comments
We provided the public the opportunity to participate in the
development of this AD. No comments have been submitted on the proposed
AD or on the determination of the cost to the public.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD as proposed.
Cost Impact
There are approximately 467 airplanes of the affected design in the
worldwide fleet. The FAA estimates that 430 airplanes of U.S. registry
will be affected by this AD, that it will take approximately 1 work
hour per airplane to accomplish the required actions, and that the
average labor rate is $65 per work hour. Based on these figures, the
cost impact of the AD on U.S. operators is estimated to be $27,950, or
$65 per airplane.
The cost impact figure discussed above is based on assumptions that
no operator has yet accomplished any of the requirements of this AD
action, and that no operator would accomplish those actions in the
future if this AD were not adopted. The cost impact figures discussed
in AD rulemaking actions represent only the time necessary to perform
the specific actions actually required by the AD. These figures
typically do not include incidental costs, such as the time required to
gain access and close up, planning time, or time necessitated by other
administrative actions.
Regulatory Impact
The regulations adopted herein will not have a substantial direct
effect on the States, on the relationship between the national
Government and the States, or on the distribution of power and
responsibilities among the various levels of government. Therefore, it
is determined that this final rule does not have federalism
implications under Executive Order 13132.
For the reasons discussed above, I certify that this action (1) is
not a ``significant regulatory action'' under Executive Order 12866;
(2) is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and (3) will not have a
significant economic impact, positive or negative, on a substantial
number of small entities under the criteria of the Regulatory
Flexibility Act. A final evaluation has been prepared for this action
and it is contained in the Rules Docket. A copy of it may be obtained
from the Rules Docket at the location provided under the caption
ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. Section 39.13 is amended by adding the following new airworthiness
directive:
2004-03-35 Raytheon Aircraft Company (Formerly Beech): Amendment 39-
13479. Docket 2002-NM-225-AD.
Applicability: Model Beech 400A series airplanes having serial
numbers RK-45, and RK-49 through RK-322 inclusive; and Model 400T
series airplanes having serial numbers TT-1 through TT-180
inclusive, and TX-1 through TX-12 inclusive; certificated in any
category.
Compliance: Required as indicated, unless accomplished
previously.
To prevent intermittent sticking of the relays on the roll trim
printed circuit board (PCB) in either the open or closed position,
which could result in an out-of-trim condition that could require
using considerable control wheel force to keep the wings level, and
consequent reduced controllability of the airplane, accomplish the
following:
Inspection and Replacement, if Necessary
(a) Within 200 flight hours or 6 months after the effective date
of this AD, whichever occurs first, perform an inspection to
determine the part number of the A194 roll trim PCB, in accordance
with Raytheon Service Bulletin SB 27-3464, dated December 2001.
(1) If the A194 roll trim PCB has a part number of 128-364122-7
or higher (i.e., 128-364122-9, -11, etc.): No further action is
required by this paragraph.
[[Page 7556]]
(2) If the A194 roll trim PCB does not have a part number of
128-364122-7 or higher: Before further flight, replace the A194 roll
trim PCB with a PCB having a part number of 128-364122-7 or higher,
in accordance with the service bulletin.
Parts Installation
(b) As of the effective date of this AD, no person may install
on any airplane an A194 roll trim PCB having part number 128-364122-
1 or 128-364122-5.
Alternative Methods of Compliance
(c) In accordance with 14 CFR 39.19, the Manager, Wichita
Aircraft Certification Office, FAA, is authorized to approve
alternative methods of compliance for this AD.
Incorporation by Reference
(d) The actions must be done in accordance with Raytheon Service
Bulletin SB 27-3464, dated December 2001. This incorporation by
reference was approved by the Director of the Federal Register in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be
obtained from Raytheon Aircraft Company, Department 62, P.O. Box 85,
Wichita, Kansas 67201-0085. Copies may be inspected at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington; or at the FAA, Wichita Aircraft Certification Office,
1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas;
or at the Office of the Federal Register, 800 North Capitol Street,
NW., Suite 700, Washington, DC.
Effective Date
(e) This amendment becomes effective on March 24, 2004.
Issued in Renton, Washington, on February 5, 2004.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 04-3203 Filed 2-17-04; 8:45 am]
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