AD 95-17-08

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AD Number:
95-17-08
Document Type:
AD Final Rules
Docket Number:
94-CE-32-AD
Subject Heading:
Airworthiness Directives; Stemme GMBH; Model S10 Gliders
Subject:
Rudder Control Cable System
Status:
Current
Citation:
Federal Register: August 28, 1995 (Volume 60, Number 166)
Citation Publish Date:
08/28/1995
Effective Date:
10/10/1995
Make:
Stemme GmbH & Co. KG
Model:
Stemme S10
Product Type:
Aircraft
Product Subtype:
Glider
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 95-17-08
CITATION:   [Federal Register: August 28, 1995 (Volume 60, Number 166)]

PAGE NUMBER:   [Page 44423]

DOCKET NUMBER:   94-CE-32-AD

AMENDMENT:   39-9338

AD NUMBER:   95-17-08

SUBJECT HEADING:   Airworthiness Directives; Stemme GMBH; Model S10 Gliders

ACTION:   Final rule

SUMMARY:   This amendment adopts a new airworthiness directive (AD) that applies to Stemme GmbH (Stemme) S10 gliders. This action requires modifying the rudder control cable system. Rupture of a turnbuckle eye bolt in the rudder control cable system on one of the affected gliders prompted this action. The actions specified by this AD are intended to prevent rudder control cable system failure caused by rupture of the turnbuckle eye bolt, which, if not detected and corrected, could result in loss of rudder control and eventual loss of control of the glider.

DATES:   Effective October 10, 1995. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of October 10, 1995.

ADDRESSES:   Service information that applies to this AD may be obtained from Stemme GmbH & Co. KG, Flugplatz Gebaude 47, D-15344 Staussberg, Germany. This information may also be examined at the Federal Aviation Administration (FAA), Central Region, Office of the Assistant Chief Counsel, Attention: Rules Docket 94-CE-32-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. Herman C. Belderok, Project Officer, 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:  
A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to Stemme S10 gliders was published in the Federal Register on March 30, 1995 (60 FR 16395). The proposal would require modifying the rudder control cable system in accordance with Stemme Service Bulletin (SB) A31-10-018 (pages 4- 6), dated June 3, 1994.

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.

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.

The FAA estimates that 3 gliders in the U.S. registry will be affected by this AD, that it will take approximately 4 workhours per glider to accomplish the required action, and that the average labor rate is approximately $60 an hour. Parts cost approximately $60 per glider. Based on these figures, the total cost impact of the AD on U.S. operators is estimated to be $900 ($300 per glider). This figure is based upon the assumption that no affected owner/operator of the affected gliders has accomplished the proposed modification.

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), 40101, 40113, 44701.

Section 39.13 - [AMENDED]
2. Section 39.13 is amended by adding a new airworthiness directive to read as follows:

REGULATORY TEXT:  
95-17-08 STEMME GMBH: Amendment 39-9338; Docket No. 94-CE-32-AD.

Applicability: Model S10 Gliders (serial numbers 10-03 through 10-58), certificated in any category.

NOTE 1: This AD applies to each glider 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 gliders that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must use the authority provided in paragraph (c) of this AD to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any glider from the applicability of this AD.

Compliance: Required upon the accumulation of 150 hours time-in-service (TIS) or within the next 20 hours TIS after the effective date of this AD, whichever occurs later, unless already accomplished.

To prevent rudder control cable system failure caused by rupture of the turnbuckle eye bolt, which, if not detected and corrected, could result in loss of rudder control, accomplish the following:

(a) Modify the rudder control cable system in accordance with the instructions in Stemme Service Bulletin A31-10-018 (pages 4-6), dated June 3, 1994.

(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 glider 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) The modifications required by this AD shall be done in accordance with Stemme Service Bulletin A31-10-018 (pages 4-6), dated June 3, 1994. 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 Stemme GmbH & Co. KG, Flugplatz Gebaude 47, D-15344 Staussberg, Germany. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW., 7th Floor, suite 700, Washington, DC.

(e) This amendment becomes effective on October 10, 1995.

FOOTER: