[Federal Register Volume 63, Number 166 (Thursday, August 27, 1998)]
[Rules and Regulations]
[Pages 45681-45682]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-22825]
[[Page 45681]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-CE-51-AD; Amendment 39-10722; AD 98-18-06]
RIN 2120-AA64
Airworthiness Directives; Schempp-Hirth K.G. Model Cirrus
Sailplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment adopts a new airworthiness directive (AD) that
applies to certain Schempp-Hirth K.G. (Schemmp-Hirth) Model Cirrus
sailplanes. This AD requires modifying or replacing the connecting rod
between the airbrake bellcranks, and replacing the existing 6
millimeter (mm) bolt with an 8 mm bolt. This AD is the result of
mandatory continuing airworthiness information (MCAI) issued by the
airworthiness authority for Germany. The actions specified by this AD
are intended to prevent the threaded bolt that is welded to the
connecting rod between the airbrake bellcranks from breaking, which
could result in loss of airbrake control with a possible reduction/loss
of sailplane control.
DATES: Effective October 12, 1998.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of October 12, 1998.
ADDRESSES: Service information that applies to this AD may be obtained
from Schempp-Hirth Flugzeugbau GmbH, Kreben Strasse 25, D-73230
Kircheim unter Teck, Germany. This information may also be examined at
the Federal Aviation Administration (FAA), Central Region, Office of
the Regional Counsel, Attention: Rules Docket No. 98-CE-51-AD, Room
1558, 601 E. 12th Street, Kansas City, Missouri 64106; or at the Office
of the Federal Register, 800 North Capitol Street, NW, suite 700,
Washington, DC.
FOR FURTHER INFORMATION CONTACT: Mr. Mike Kiesov, Aerospace Engineer,
FAA, Small Airplane Directorate, 1201 Walnut, suite 900, Kansas City,
Missouri 64106; telephone: (816) 426-6934; facsimile: (816) 426-2169.
SUPPLEMENTARY INFORMATION:
Events Leading to the Issuance of This AD
A proposal to amend part 39 of the Federal Aviation Regulations (14
CFR part 39) to include an AD that would apply to certain Schempp-Hirth
K.G. (Schemmp-Hirth) Model Cirrus sailplanes was published in the
Federal Register as a notice of proposed rulemaking (NPRM) on June 18,
1998 (63 FR 33292). The NPRM proposed to require modifying or replacing
the connecting rod between the airbrake bellcranks, and replacing the
existing 6 millimeter (mm) bolt with an 8 mm bolt. Accomplishment of
the proposed action as specified in the NPRM would be in accordance
with Schempp-Hirth Technical Note No. 265-8, dated February 11, 1985.
The NPRM was the result of mandatory continuing airworthiness
information (MCAI) issued by the airworthiness authority for Germany.
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No comments were received on the
proposed rule or the FAA's determination of the cost to the public.
The FAA's Determination
After careful review of all available information related to the
subject presented above, the FAA has determined that air safety and the
public interest require the adoption of the rule as proposed except for
minor editorial corrections. The FAA has determined that these minor
corrections will not change the meaning of the AD and will not add any
additional burden upon the public than was already proposed.
Compliance Time of This AD
Although the unsafe condition identified in this AD occurs during
flight and is a direct result of sailplane operation, the FAA has no
way of determining how long the 6 mm bolt may go without breaking. For
example, the condition could exist on a sailplane with 200 hours time-
in-service (TIS), but could be developing and not actually exist on
another sailplane until 300 hours TIS. For this reason, the FAA has
determined that a compliance based on calendar time should be utilized
in this AD in order to assure that the unsafe condition is addressed on
all sailplanes in a reasonable time period.
Cost Impact
The FAA estimates that 21 sailplanes in the U.S. registry will be
affected by this AD, that it will take approximately 12 workhours per
sailplane to accomplish this action, and that the average labor rate is
approximately $60 an hour. Parts cost approximately $60 per sailplane.
Based on these figures, the total cost impact of this AD on U.S.
operators is estimated to be $16,380, or $780 per sailplane.
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 a Federalism Assessment.
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 copy of the final evaluation prepared for this
action is contained in the Rules Docket. A copy of it may be obtained
by contacting 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 a new airworthiness directive
(AD) to read as follows:
98-18-06 Schempp-Hirth K.G.: Amendment 39-10722; Docket No. 98-CE-
51-AD.
Applicability: Model Cirrus sailplanes, serial numbers 1 through
50, certificated in any category.
Note 1: This AD applies to each sailplane identified in the
preceding applicability provision, regardless of whether it has been
modified, altered, or repaired in the area subject to the
requirements of this AD. For sailplanes that have been modified,
altered, or repaired so that the performance of the
[[Page 45682]]
requirements of this AD is affected, the owner/operator must request
approval for an alternative method of compliance in accordance with
paragraph (c) 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: Within the next 4 calendar months after the
effective date of this AD, unless already accomplished.
To prevent the threaded bolt that is welded to the connecting
rod between the airbrake bellcranks from breaking, which could
result in loss of airbrake control with a possible reduction/loss of
sailplane control, accomplish the following:
(a) Modify or replace the connecting rod between the airbrake
bellcranks, and replace the existing 6 millimeter (mm) bolt with an
8 mm bolt. Accomplish these actions in accordance with Schempp-Hirth
Technical Note No. 265-8, dated February 11, 1985.
(b) 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 sailplane to a location where
the requirements of this AD can be accomplished.
(c) An alternative method of compliance or adjustment of the
compliance time that provides an equivalent level of safety may be
approved by the Manager, Small Airplane Directorate, FAA, 1201
Walnut, suite 900, Kansas City, Missouri 64106. The request shall be
forwarded through an appropriate FAA Maintenance Inspector, who may
add comments and then send it to the Manager, Small Airplane
Directorate.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Small Airplane Directorate.
(d) Questions or technical information related to Schempp-Hirth
Technical Note No. 265-8, dated February 11, 1985, should be
directed to Schempp-Hirth Flugzeugbau GmbH, Kreben Strasse 25, D-
73230 Kircheim unter Teck, Germany. This service information may be
examined at the FAA, Central Region, Office of the Regional Counsel,
Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106.
(e) The modification and replacements required by this AD shall
be done in accordance with Schempp-Hirth Technical Note No. 265-8,
dated February 11, 1985. 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
Schempp-Hirth Flugzeugbau GmbH, Kreben Strasse 25, D-73230 Kircheim
unter Teck, Germany. Copies may be inspected at the FAA, Central
Region, Office of the Regional Counsel, Room 1558, 601 E. 12th
Street, Kansas City, Missouri, 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 German AD 85-56,
dated March 4, 1985.
(f) This amendment becomes effective on October 12, 1998.
Issued in Kansas City, Missouri, on August 18, 1998.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 98-22825 Filed 8-26-98; 8:45 am]
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