AD Amdt-39-14493
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | AvCraft | 328-100 | Airworthiness Directives; AvCraft Dornier Model 328-100 Airplanes |
Unsafe Condition
Certain airplane flight manual (AFM) revisions are not necessary after modifying the flap actuators of the flight controls. This AD aims to prevent an uncommanded retraction of the flaps during takeoff, which could result in an aborted takeoff and consequent potential for runway overrun.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the AFM as specified in paragraphs (g)(1) and (g)(2) of this AD. Concurrently, remove the AFM revisions required by paragraph (f) of this AD from the AFM. For specific serial number ranges, modify the flap actuators of the flight controls.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 3 days after January 8, 2001, for AFM revisions. Within 5 months after January 8, 2001, for flap actuator modifications (for specific serial numbers).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
AvCraft Dornier Model 328-100 airplanes, certificated in any category. Serial numbers 3005 through 3099, 3101 through 3108, and 3110 through 3119 are specifically mentioned for flap actuator modifications.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is revising an existing airworthiness directive (AD) that applies to all AvCraft Dornier Model 328-100 airplanes. That AD currently requires revising the airplane flight manual (AFM) to provide the flightcrew with additional information regarding procedures to ensure complete pressurization of the hydraulic lines for the flaps. The existing AD also requires, for certain airplanes, modifying of the flap actuators of the flight controls. We issued that AD to prevent an uncommanded retraction of the flaps during takeoff, which could result in an aborted takeoff and consequent potential for runway overrun. This new AD allows the removal of the AFM revisions after modifying the flap actuators of the flight controls. This AD results from the determination that the AFM revisions are not necessary after modifying the flap actuators of the flight controls. We are issuing this AD to prevent an uncommanded retraction of the flaps during takeoff, which could result in an aborted takeoff and consequent potential for runway overrun.
Document Text
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[Federal Register Volume 71, Number 36 (Thursday, February 23, 2006)]
[Rules and Regulations]
[Pages 9255-9257]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 06-1596]
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Rules and Regulations
Federal Register
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This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
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Federal Register / Vol. 71, No. 36 / Thursday, February 23, 2006 /
Rules and Regulations
[[Page 9255]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22813; Directorate Identifier 2002-NM-117-AD;
Amendment 39-14493; AD 2000-24-03 R1]
RIN 2120-AA64
Airworthiness Directives; AvCraft Dornier Model 328-100 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is revising an existing airworthiness directive (AD)
that applies to all AvCraft Dornier Model 328-100 airplanes. That AD
currently requires revising the airplane flight manual (AFM) to provide
the flightcrew with additional information regarding procedures to
ensure complete pressurization of the hydraulic lines for the flaps.
The existing AD also requires, for certain airplanes, modifying of the
flap actuators of the flight controls. We issued that AD to prevent an
uncommanded retraction of the flaps during takeoff, which could result
in an aborted takeoff and consequent potential for runway overrun. This
new AD allows the removal of the AFM revisions after modifying the flap
actuators of the flight controls. This AD results from the
determination that the AFM revisions are not necessary after modifying
the flap actuators of the flight controls. We are issuing this AD to
prevent an uncommanded retraction of the flaps during takeoff, which
could result in an aborted takeoff and consequent potential for runway
overrun.
DATES: The effective date of this AD is January 8, 2001.
On January 8, 2001 (65 FR 75601, December 4, 2000), the Director of
the Federal Register approved the incorporation by reference of Dornier
328 All Operators Telefax AOT-328-27-016, Revision 1, dated October 28,
1998; and Dornier 328 Service Bulletin SB-328-27-293, dated November
10, 1999.
On November 12, 1998 (63 FR 57244, October 27, 1998), the Director
of the Federal Register approved the incorporation by reference of
Dornier 328 All Operators Telefax AOT-328-27-016, dated July 31, 1998.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a> or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street SW., Nassif Building,
room PL-401, Washington, DC.
Contact AvCraft Aerospace GmbH, P.O. Box 1103, D-82230 Wessling,
Germany, for service information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Rosanne Ryburn, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2139; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a>
or in person at the Docket Management Facility office between 9 a.m.
and 5 p.m., Monday through Friday, except Federal holidays. The Docket
Management Facility office (telephone (800) 647-5227) is located on the
plaza level of the Nassif Building at the street address stated in the
ADDRESSES section.
Discussion
The FAA proposed to amend part 39 of the Federal Aviation
Regulations (14 CFR part 39) with an airworthiness directive (AD) to
revise AD 2000-24-03, amendment 39-12010 (65 FR 75601, December 4,
2000). The existing AD applies to all Dornier Model 328-100 series
airplanes. The proposed AD was published in the Federal Register on
November 1, 2005 (70 FR 65864) to continue to require revising the
airplane flight manual (AFM) to provide the flightcrew with additional
information regarding procedures to ensure complete pressurization of
the hydraulic lines for the flaps, and for certain airplanes, modifying
the flap actuators of the flight controls. The proposed AD also
proposed to allow the removal of the AFM revisions after modifying the
flap actuators of the flight controls.
Comments
We provided the public the opportunity to participate in the
development of this AD. We received no comments on the NPRM 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.
Costs of Compliance
We estimate that 52 airplanes of U.S. registry will be affected by
this AD.
The AFM revision that is currently required by AD 2000-24-03, and
retained in this AD, takes approximately 1 work hour per airplane to
accomplish, at an average labor rate of $65 per work hour. Based on
these figures, the cost impact of the currently required AFM revision
on U.S. operators is approximately $3,380, or $65 per airplane.
The modification that is currently required by AD 2000-24-03, and
retained in this AD, takes approximately 4 work hours per airplane to
accomplish, at an average labor rate of $65 per work hour. Required
parts will be provided by the manufacturer at no cost to the operators.
Based on these figures, the cost impact of the currently required
modification on U.S. operators is estimated to be $260 per airplane.
The removal of the AFM revisions that is specified in this AD, if
done, takes approximately 1 work hour per airplane to accomplish, at an
average labor rate of $65 per work hour. Based on these figures, the
cost impact of the removal of AFM revisions on U.S. operators is
approximately $65 per airplane.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
[[Page 9256]]
We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD 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.
For the reasons discussed above, I certify that this AD:
(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.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 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. The Federal Aviation Administration (FAA) amends Sec. 39.13 by
removing amendment 39-12010 (65 FR 75601, December 4, 2000), and adding
the following new airworthiness directive (AD):
2000-24-03 R1 AvCraft Aerospace GmbH (Formerly Fairchild Dornier
GmbH): Amendment 39-14493. Docket No. FAA-2005-22813; Directorate
Identifier 2002-NM-117-AD.
Effective Date
(a) The effective date of this AD is January 8, 2001.
Affected ADs
(b) This AD revises AD 2000-24-03.
Applicability
(c) This AD applies to all AvCraft Dornier Model 328-100
airplanes, certificated in any category.
Unsafe Condition
(d) This AD results from the determination that certain airplane
flight manual (AFM) revisions are not necessary after modifying the
flap actuators of the flight controls. We are issuing this AD to
prevent an uncommanded retraction of the flaps during takeoff, which
could result in an aborted takeoff and consequent potential for
runway overrun.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
AFM Revision
(f) Within 14 days after November 12, 1998 (the effective date
of AD 98-22-07, amendment 39-10854), accomplish the requirements of
paragraphs (f)(1) and (f)(2) of this AD.
(1) Revise the Normal Procedures section of the Dornier 328 FAA-
approved AFM to include the information specified in pages 6 and 7
of Dornier 328 All Operators Telefax (AOT) AOT-328-27-016, dated
July 31, 1998. This may be accomplished by inserting a copy of pages
6 and 7 of the AOT into the AFM.
(2) Revise the Abnormal Procedures section of the Dornier 328
FAA-approved AFM to include the information specified in page 4 of
Dornier 328 AOT-328-27-016, dated July 31, 1998. This may be
accomplished by inserting a copy of page 4 of the AOT into the AFM.
New AFM Revision
(g) For all airplanes: Within 3 days after January 8, 2001 (the
effective date of AD 2000-24-03), revise the Dornier 328 FAA-
approved AFM as specified in paragraphs (g)(1) and (g)(2) of this
AD. Concurrently with this AFM revision, remove the AFM revisions
required by paragraph (f) of this AD from the AFM.
(1) Revise the Normal Procedures section to include the
information specified in pages 4, 5, and 6 of Dornier 328 AOT-328-
27-016, Revision 1, dated October 28, 1998. This may be accomplished
by inserting a copy of pages 4, 5, and 6 of the AOT into the AFM.
(2) Revise the Abnormal Procedures section to include the
information specified in page 3 of Dornier 328 AOT-328-27-016,
Revision 1, dated October 28, 1998. This may be accomplished by
inserting a copy of page 3 of the AOT into the AFM.
Modification
(h) For airplanes with serial numbers 3005 through 3099
inclusive, 3101 through 3108 inclusive, and 3110 through 3119
inclusive: Within 5 months after January 8, 2001, modify the flap
actuators of the flight controls, in accordance with Dornier 328
Service Bulletin SB-328-27-293, dated November 10, 1999. After
accomplishing the modification, operators may remove the AFM
revisions required by paragraphs (f) and (g) of this AD from the
AFM.
Note 1: The Dornier service bulletin references Liebherr
Aerospace Service Bulletin 1048A-27-02, dated November 9, 1999, as
an additional source of service information for accomplishing the
modification of the flap actuators of the flight controls.
Alternative Methods of Compliance (AMOCs)
(i)(1) The Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA, has the authority to approve AMOCs for
this AD, if requested in accordance with the procedures found in 14
CFR 39.19.
(2) Before using any AMOC approved in accordance with 14 CFR
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
(3) AMOCs approved previously in accordance with AD 98-22-07,
amendment 39-10854, are approved as AMOCs with paragraph (f) of this
AD.
(4) AMOCs approved previously in accordance with AD 2000-24-03,
amendment 39-12010, are approved as AMOCs with this AD.
Related Information
(j) German airworthiness directive 1998-359/3, effective April
6, 2000, also addresses the subject of this AD.
Material Incorporated by Reference
(k) You must use Dornier 328 All Operators Telefax AOT-328-27-
016, dated July 31, 1998; Dornier 328 All Operators Telefax AOT-328-
27-016, Revision 1, dated October 28, 1998; and Dornier 328 Service
Bulletin SB-328-27-293, dated November 10, 1999; as applicable,
unless the AD specifies otherwise.
(1) On January 8, 2001 (65 FR 75601, December 4, 2000), the
Director of the Federal Register approved the incorporation by
reference of Dornier 328 All Operators Telefax AOT-328-27-016,
Revision 1, dated October 28, 1998; and Dornier 328 Service Bulletin
SB-328-27-293, dated November 10, 1999.
(2) On November 12, 1998 (63 FR 57244, October 27, 1998), the
Director of the Federal Register approved the incorporation by
reference of Dornier 328 All Operators Telefax AOT-328-27-016, dated
July 31, 1998.
(3) Contact AvCraft Aerospace GmbH, P.O. Box 1103, D-82230
Wessling, Germany, for a copy of this service information. You may
review copies at the Docket Management Facility, U.S. Department of
Transportation, 400 Seventh Street SW., room PL-401, Nassif
[[Page 9257]]
Building, Washington, DC; on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a>; or
at the National Archives and Records Administration (NARA). For
information on the availability of this material at the NARA, call
(202) 741-6030, or go to <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.
Issued in Renton, Washington, on February 10, 2006.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-1596 Filed 2-22-06; 8:45 am]
BILLING CODE 4910-13-P
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