[Federal Register Volume 63, Number 152 (Friday, August 7, 1998)]
[Rules and Regulations]
[Pages 42215-42217]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-21099]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-NM-213-AD; Amendment 39-10696; AD 98-16-20]
RIN 2120-AA64
Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; request for comments.
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SUMMARY: This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Saab Model SAAB 2000 series airplanes. This
action requires a one-time visual inspection of the right-and left-hand
propeller gearbox to ensure that the attachment nut that secures the
borescope plug to the gearbox is installed; and installation of an
attachment nut, if necessary. This amendment is prompted by issuance of
mandatory continuing airworthiness information by a foreign civil
airworthiness authority. The actions specified in this AD are intended
to prevent oil leakage from the propeller gearbox, which could lead to
an increase in oil temperature and result in engine shutdown.
DATES: Effective August 24, 1998. The incorporation by reference of
certain publications listed in the regulations is approved by the
Director of the Federal Register as of August 24, 1998.
Comments for inclusion in the Rules Docket must be received on or
before September 8, 1998.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Transport Airplane Directorate, ANM-114,
Attention: Rules Docket No. 98-NM-213-AD, 1601 Lind Avenue, SW.,
Renton, Washington 98055-4056.
The service information referenced in this AD may be obtained from
SaabAircraft AB, SAAB Aircraft Product Support, S-581.88, Linkoping,
Sweden. This information may be examined at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the
Office of
[[Page 42216]]
the Federal Register, 800 North Capitol Street, NW., suite 700,
Washington, DC.
FOR FURTHER INFORMATION CONTACT: Norman B. Martenson,
Manager,International Branch, ANM-116, FAA, Transport Airplane
Directorate, 1601 LindAvenue, SW., Renton, Washington 98055-4056;
telephone (425) 227-2110; fax(425) 227-1149.
SUPPLEMENTARY INFORMATION: The Luftfartsverket (LFV), which is the
airworthiness authority for Sweden, recently notified the FAA that an
unsafe condition may exist on certain Saab Model SAAB 2000 series
airplanes. The LFV advises that due to an error in Saab Service
Bulletin 2000-30-015, dated February 16, 1998, and Statement 73PPS1634,
and subsequent to the accomplishment of the actions specified in those
documents, the borescope plug on the propeller gearbox may not be
secured properly by the attachment nut and may consequently come loose.
This condition, if not corrected, could result in oil leakage from the
propeller gearbox, which could lead to an increase in oil temperature
and result in engine shutdown.
Explanation of Relevant Service Information
Saab has issued Alert Service Bulletin 2000-A72-001, dated June 12,
1998, and Revision 01, dated June 26, 1998. These alert service
bulletins describe procedures for a one-time visual inspection of the
right-and left-hand propeller gearboxes to ensure that the attachment
nut that secures the borescope plug to the gearbox is installed; and
installation of an attachment nut, if necessary. Accomplishment of the
actions specified in the alert service bulletins is intended to
adequately address the identified unsafe condition. The LFV classified
these alert service bulletins as mandatory and issued Swedish
airworthiness directive 1-129R1, dated June 26, 1998, in order to
assure the continued airworthiness of these airplanes in Sweden.
FAA's Conclusions
This airplane model is manufactured in Sweden and is type
certificated for operation in the United States under the provisions of
section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and
the applicable bilateral airworthiness agreement. Pursuant to this
bilateral airworthiness agreement, the LFV has kept the FAA informed of
the situation described above. The FAA has examined the findings of the
LFV, reviewed all available information, and determined that AD action
is necessary for products of this type design that are certificated for
operation in the United States.
Explanation of Requirements of Rule
Since an unsafe condition has been identified that is likely to
exist or develop on other airplanes of the same type design registered
in the United States, this AD is being issued to prevent oil leakage
from the propeller gearbox, which could lead to an increase in oil
temperature and result in engine shutdown. This AD requires
accomplishment of the actions specified in the alert service bulletins
described previously.
Determination of Rule's Effective Date
Since a situation exists that requires the immediate adoption of
this regulation, it is found that notice and opportunity for prior
public comment hereon are impracticable, and that good cause exists for
making this amendment effective in less than 30 days.
Comments Invited
Although this action is in the form of a final rule that involves
requirements affecting flight safety and, thus, was not preceded by
notice and an opportunity for public comment, comments are invited on
this rule. Interested persons are invited to comment on this rule by
submitting such written data, views, or arguments as they may desire.
Communications shall identify the Rules Docket number and be submitted
in triplicate to the address specified under the caption ADDRESSES. All
communications received on or before the closing date for comments will
be considered, and this rule may be amended in light of the comments
received. Factual information that supports the commenter's ideas and
suggestions is extremely helpful in evaluating the effectiveness of the
AD action and determining whether additional rulemaking action would be
needed.
Comments are specifically invited on the overall regulatory,
economic, environmental, and energy aspects of the rule that might
suggest a need to modify the rule. All comments submitted will be
available, both before and after the closing date for comments, in the
Rules Docket for examination by interested persons. A report that
summarizes each FAA-public contact concerned with the substance of this
AD will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments
submitted in response to this rule must submit a self-addressed,
stamped postcard on which the following statement is made: ``Comments
to Docket Number 98-NM-213-AD.'' The postcard will be date stamped and
returned to the commenter.
Regulatory Impact
The regulations adopted herein will not have substantial direct
effects 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, in
accordance with Executive Order 12612, it is determined that this final
rule does not have sufficient federalism implications to warrant the
preparation of aFederalism Assessment.
The FAA has determined that this regulation is an emergency
regulation that must be issued immediately to correct an unsafe
condition in aircraft, and that it is not a``significant regulatory
action'' under Executive Order 12866. It has been determined further
that this action involves an emergency regulation under DOT Regulatory
Policies and Procedures (44 FR 11034, February 26, 1979). If it is
determined that this emergency regulation otherwise would be
significant under DOT Regulatory Policies and Procedures, a final
regulatory evaluation will be prepared and placed in the Rules Docket.
A copy of it, if filed, 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
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
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]
2. Section 39.13 is amended by adding the following new
airworthiness directive:
98-16-20 Saab Aircraft AB: Amendment 39-10696. Docket 98-NM-213-AD.
Applicability: Model SAAB 2000 series airplanes, having serial
numbers -004 through -056 inclusive; on which Saab Service Bulletin
2000-30-015, dated
[[Page 42217]]
February 16, 1998, or Statement 73PPS1634 has been accomplished;
certificated in any category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
otherwise modified, altered, or repaired in the area subject to the
requirements of this AD. For airplanes that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (b) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and, if the unsafe condition has not been
eliminated, the request should include specific proposed actions to
address it.
Compliance: Required as indicated, unless accomplished
previously.
To prevent oil leakage from the propeller gearbox, which could
lead to an increase in oil temperature and result in engine
shutdown, accomplish the following:
(a) Within 3 days after the effective date of this AD, perform a
one-time visual inspection of the borescope plug in the right-and
left-hand propeller gearboxes to ensure that the attachment nut that
secures the borescope plug to the gearbox is installed, in
accordance with Saab Alert Service Bulletin 2000-A72-001, dated June
12, 1998, or Revision 01, dated June 26, 1998.
(1) If the attachment nut is installed, no further action is
required by this AD.
(2) If the attachment nut is not installed, prior to further
flight, install an attachment nut on the borescope plug, in
accordance with the alert service bulletin.
(b) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, International Branch, ANM-116, FAA,
Transport Airplane Directorate. Operators shall submit their
requests through an appropriate FAA Principal Maintenance Inspector,
who may add comments and then send it to the Manager, International
Branch, ANM-116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the International Branch, ANM-116.
(c) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be accomplished.
(d) The inspection and installation shall be done in accordance
with Saab Alert Service Bulletin 2000-A72-001, dated June 12, 1998,
or Saab Alert Service Bulletin 2000-A72-001, Revision 01, dated June
26, 1998. 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 Saab Aircraft AB,
SAAB Aircraft Product Support, S-581.88, Linkoping, Sweden. Copies
may be inspected at the FAA, Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington; or at the Office of the
Federal Register, 800 North Capitol Street, NW., suite 700,
Washington, DC.
Note 3: The subject of this AD is addressed in Swedish
airworthiness directive 1-129R1, dated June 26, 1998.
(e) This amendment becomes effective on August 24, 1998.
Issued in Renton, Washington, on July 31, 1998.
Darrell M. Pederson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 98-21099 Filed 8-6-98; 8:45 am]
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