[Federal Register Volume 63, Number 92 (Wednesday, May 13, 1998)]
[Rules and Regulations]
[Pages 26425-26426]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-12380]
[[Page 26425]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 97-CE-103-AD; Amendment 39-10518; AD 98-10-07]
RIN 2120-AA64
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau
Model ASK 21 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 all Alexander Schleicher Segelflugzeugbau (Alexander
Schleicher) Model ASK 21 sailplanes that have certain modifications
installed. This AD requires changing the sailplane flight manual's
weight and balance information. 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 operator from using inaccurate weight and balance
information provided in the sailplane flight manual (SFM), which could
lead to hazardous flight conditions.
DATES: Effective June 26, 1998.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of June 26, 1998.
ADDRESSES: Service information that applies to this AD may be obtained
from Alexander Schleicher, Segelflugzeugbau, 6416 Poppenhausen,
Wasserkuppe, Federal Republic of Germany; telephone: 49.6658.890 or
49.6658.8920; facsimile: 49.6658.8923 or 49.6658.8940. This information
may also be examined at the Federal Aviation Administration (FAA),
Central Region, Office of the Regional Counsel, Attention: Rules Docket
No. 97-CE-103-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. J. Mike Kiesov, Project Officer,
Sailplanes/Gliders, Small Airplane Directorate, Aircraft Certification
Service, FAA, 1201 Walnut, suite 900, Kansas City, Missouri 64106;
telephone: (816) 426-6932; 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 all Alexander
Schleicher Model ASK 21 sailplanes was published in the Federal
Register as a notice of proposed rulemaking (NPRM) on February 12, 1998
(63 FR 7083). The NPRM proposed to require changing the SFM by
replacing two pages referencing the trim weight information.
Accomplishment of the proposed installation would be in accordance with
the Action section of Alexander Schleicher Technical Note No. 13 a,
dated June 4, 1984.
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.
Cost Impact
The FAA estimates that 30 sailplanes in the U.S. registry will be
affected by this AD, that it will take approximately 1 workhour per
sailplane to accomplish this action, and that the average labor rate is
approximately $60 an hour. There are no parts required for this action.
This action may be performed by the owner/operator holding at least a
private pilot certificate as authorized by section 43.7 of the Federal
Aviation Regulations (14 CFR 43.7), and must be entered into the
aircraft records showing compliance with this AD in accordance with
section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). Based
on these figures, there is no cost impact of this AD on U.S. operators.
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:
98-10-07 Alexander Schleicher Segelflugzeugbau: Amendment 39-10518;
Docket No. 97-CE-103-AD.
Applicability: Model ASK 21 sailplanes, all serial numbers,
certificated in any category, that are equipped with the
modifications in Alexander Schleicher Technical Note (TN) 3 or TN 7.
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 requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (d) 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
[[Page 26426]]
been eliminated, the request should include specific proposed
actions to address it.
Compliance: Required within the next 3 calendar months after the
effective date of this AD, unless already accomplished.
To prevent the operator from using inaccurate weight and balance
information provided in the sailplane flight manual (SFM), which
could lead to hazardous flight conditions, accomplish the following:
(a) Replace page 2 (dated May 16, 1984) and page 13 (dated
February 16, 1984) from the Alexander Schleicher Model ASK 21 SFM
with new pages 2 and 13, both dated June 4, 1984, in accordance with
Alexander Schleicher ASK 21 Technical Note No. 13 a, dated June 4,
1984.
(b) Incorporating the SFM revisions, as required by this AD, may
be performed by the owner/operator holding at least a private pilot
certificate as authorized by section 43.7 of the Federal Aviation
Regulations (14 CFR 43.7), and must be entered into the aircraft
records showing compliance with this AD in accordance with section
43.9 of the Federal Aviation Regulations (14 CFR 43.9).
(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 sailplane to a location where
the requirements of this AD can be accomplished.
(d) 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, Aircraft
Certification Service, 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.
(e) Questions or technical information related to Alexander
Schleicher ASK 21 Technical Note No. 13 a, dated June 4, 1984,
should be directed to Alexander Schleicher, Segelflugzeugbau, 6416
Poppenhausen, Wasserkuppe, Federal Republic of Germany; telephone:
49.6658.890 or 49.6658.8920; facsimile: 49.6658.8923 or
49.6658.8940. 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.
(f) The replacement required by this AD shall be done in
accordance with Alexander Schleicher ASK 21 Technical Note No. 13 a,
dated June 4, 1984. 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 Alexander
Schleicher, Segelflugzeugbau, 6416 Poppenhausen, Wasserkuppe,
Federal Republic of 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 No. 84-
32/2 Schleicher, dated June 12, 1984.
(g) This amendment becomes effective on June 26, 998. Issued in
Kansas City, Missouri, on April 30, 1998.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 98-12380 Filed 5-12-98; 8:45 am]
BILLING CODE 4910-13-U
