80 FR 14296 - Airworthiness Directives; Stemme AG Gliders

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 80, Issue 53 (March 19, 2015)

Page Range		14296-14297
FR Document		2015-06296

We are adopting a new airworthiness directive (AD) for Stemme AG TSA-M Models S6 and S6-RT gliders. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a bending defect of the fork head installed in the aileron, speed brake, and flap control systems. We are issuing this AD to require actions to address the unsafe condition on these products.

Federal Register, Volume 80 Issue 53 (Thursday, March 19, 2015)

[Federal Register Volume 80, Number 53 (Thursday, March 19, 2015)]
[Rules and Regulations]
[Pages 14296-14297]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2015-06296]



[[Page 14296]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-0633; Directorate Identifier 2015-CE-005-AD; 
Amendment 39-18121; AD 2015-06-03]
RIN 2120-AA64


Airworthiness Directives; Stemme AG Gliders

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for Stemme 
AG TSA-M Models S6 and S6-RT gliders. This AD results from mandatory 
continuing airworthiness information (MCAI) issued by the aviation 
authority of another country to identify and correct an unsafe 
condition on an aviation product. The MCAI describes the unsafe 
condition as a bending defect of the fork head installed in the 
aileron, speed brake, and flap control systems. We are issuing this AD 
to require actions to address the unsafe condition on these products.

DATES: This AD is effective March 24, 2015.
    We must receive comments on this AD by May 4, 2015.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: (202) 493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays.
    For information concerning this action, contact Stemme AG, 
Flugplatzstra[szlig]e F2, Nr. 6-7, D-15344 Strausberg, Germany; phone: 
+49 (0) 3341/3612 0; fax: none; email: [email protected]; internet: 
www.stemme.info.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015-
0633; or in person at the Docket Management Facility between 9 a.m. and 
5 p.m., Monday through Friday, except Federal holidays. The AD docket 
contains this AD, the regulatory evaluation, any comments received, and 
other information. The street address for the Docket Office (telephone 
(800) 647-5527) is in the ADDRESSES section. Comments will be available 
in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aerospace Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090; email: 
[email protected].

SUPPLEMENTARY INFORMATION: 

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Community, has issued AD 
No.: 2015-0034-E, dated February 27, 2015, (referred to after this as 
``the MCAI''), to correct an unsafe condition for the specified 
products. The MCAI states:

    A report was received concerning a broken fork head, installed 
in the speed brake control circuit of a TSA-M Model S6-RT powered 
sailplane. Preliminary investigation results revealed additional 
cases of bending defect of the same part, which were installed in 
the aileron and flaps control systems of the TSA-M type design. The 
same fork heads are also installed in the control systems of ASP 
Model S15-1 aeroplanes.
    This condition, if not corrected, could lead to failure of the 
flight control system, possibly resulting in loss of control of the 
aeroplane.
    For the reasons described above, this AD prohibits the operation 
of the affected aeroplanes pending the availability of a 
modification of the affected flight control systems in accordance 
with approved instructions.

    This AD is a temporary measure and further AD action may follow. 
You may examine the MCAI on the Internet at http://www.regulations.gov 
by searching for and locating Docket No. FAA-2015-0633.

FAA's Determination and Requirements of the AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with this State of Design Authority, they 
have notified us of the unsafe condition described in the MCAI and 
service information referenced above. We are issuing this AD because we 
evaluated all information provided by the State of Design Authority and 
determined the unsafe condition exists and is likely to exist or 
develop on other products of the same type design.

FAA's Determination of the Effective Date

    An unsafe condition exists that requires the immediate adoption of 
this AD. The FAA has found that the risk to the flying public justifies 
waiving notice and comment prior to adoption of this rule because a 
bending defect of the fork head could lead to failure of the flight 
control system, possibly resulting in loss of control. Therefore, we 
determined that notice and opportunity for public comment before 
issuing this AD are impracticable and that good cause exists for making 
this amendment effective in fewer than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight 
safety, and we did not precede it by notice and opportunity for public 
comment. We invite you to send any written relevant data, views, or 
arguments about this AD. Send your comments to an address listed under 
the ADDRESSES section. Include ``Docket No. FAA-2015-0633; Directorate 
Identifier 2015-CE-005-AD'' at the beginning of your comments. We 
specifically invite comments on the overall regulatory, economic, 
environmental, and energy aspects of this AD. We will consider all 
comments received by the closing date and may amend this AD because of 
those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this AD.

Costs of Compliance

    We estimate that this AD will affect 6 products of U.S. registry.
    At the time of issuance of this AD, no design solution is available 
to restore the airworthiness of the respective type designs to a level 
corresponding to their approved type design specifications. Therefore, 
the FAA cannot determine the cost of returning the affected gliders to 
service.

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 14297]]

    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 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 the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) 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.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

    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 FAA amends Sec.  39.13 by adding the following new AD:

2015-06-03 Stemme AG: Amendment 39-18121; Docket No. FAA-2015-0633; 
Directorate Identifier 2015-CE-005-AD.

(a) Effective Date

    This airworthiness directive (AD) becomes effective March 24, 
2015.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Stemme AG TSA-M Models S6 and S6-RT gliders, 
all serial numbers, certificated in any category.

(d) Subject

    Air Transport Association of America (ATA) Code 27: Flight 
Controls.

(e) Reason

    This AD was prompted by mandatory continuing airworthiness 
information (MCAI) originated by an aviation authority of another 
country to identify and correct an unsafe condition on an aviation 
product. The MCAI describes the unsafe condition as a bending defect 
of the fork head installed in the aileron, speed brake, and flap 
control systems. We are issuing this AD to detect and correct the 
bending defect of the fork head that could result in failure of the 
flight control system, possibly resulting in loss of control.

(f) Actions and Compliance

    Unless already done, before further flight, after March 24, 2015 
(the effective date of this AD), modify the affected flight control 
systems, or take other actions, following a method approved 
specifically for this AD by the FAA, Small Airplane Directorate. 
Contact Stemme AG to obtain FAA-approved repair instructions 
approved specifically for compliance with this AD and incorporate 
those instructions. You can find contact information for Stemme AG 
in paragraph (i)(2) of this AD.
    Note 1 to paragraph (f) of this AD: At the time of issuance of 
this AD, no design solution is available to restore the 
airworthiness of the respective type designs to a level 
corresponding to their approved type design specifications.

(g) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Office, FAA, has the authority to approve AMOCs for this 
AD, if requested using the procedures found in 14 CFR 39.19. Send 
information to ATTN: Jim Rutherford, Aerospace Engineer, FAA, Small 
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4165; fax: (816) 329-4090; email: 
[email protected]. Before using any approved AMOC on any 
airplane to which the AMOC applies, notify your appropriate 
principal inspector (PI) in the FAA Flight Standards District Office 
(FSDO), or lacking a PI, your local FSDO.
    (2) Airworthy Product: For any requirement in this AD to obtain 
corrective actions from a manufacturer or other source, use these 
actions if they are FAA-approved. Corrective actions are considered 
FAA-approved if they are approved by the State of Design Authority 
(or their delegated agent). You are required to assure the product 
is airworthy before it is returned to service.

(h) Special Flight Permit

    Special flight permits are prohibited.

(i) Related Information

    (1) Refer to MCAI European Aviation Safety Agency (EASA) AD No.: 
2015-0034-E, dated February 27, 2015, for related information. You 
may examine the MCAI on the Internet at http://www.regulations.gov 
by searching for and locating Docket No. FAA-2015-0633.
    (2) For information concerning this action, contact Stemme AG, 
Flugplatzstra[szlig]e F2, Nr. 6-7, D-15344 Strausberg, Germany; 
phone: +49 (0) 3341/3612 0; fax: none; email: [email protected]; 
internet: www.stemme.info.

    Issued in Kansas City, Missouri, on March 12, 2015.
Robert Busto,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-06296 Filed 3-18-15; 8:45 am]
 BILLING CODE 4910-13-P

14296 Federal Register / Vol. 80, No. 53 / Thursday, March 19, 2015 / Rules and Regulations

DEPARTMENT OF TRANSPORTATION Management Facility between 9 a.m. unsafe condition exists and is likely to
and 5 p.m., Monday through Friday, exist or develop on other products of the
Federal Aviation Administration except Federal holidays. The AD docket same type design.
contains this AD, the regulatory
14 CFR Part 39 FAA’s Determination of the Effective
evaluation, any comments received, and
Date
[Docket No. FAA–2015–0633; Directorate other information. The street address for
Identifier 2015–CE–005–AD; Amendment the Docket Office (telephone (800) 647– An unsafe condition exists that
39–18121; AD 2015–06–03] 5527) is in the ADDRESSES section. requires the immediate adoption of this
Comments will be available in the AD AD. The FAA has found that the risk to
RIN 2120–AA64 the flying public justifies waiving notice
docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Jim and comment prior to adoption of this
Airworthiness Directives; Stemme AG rule because a bending defect of the fork
Gliders Rutherford, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, head could lead to failure of the flight
AGENCY: Federal Aviation Room 301, Kansas City, Missouri 64106; control system, possibly resulting in
Administration (FAA), DOT. telephone: (816) 329–4165; fax: (816) loss of control. Therefore, we
ACTION: Final rule; request for 329–4090; email: jim.rutherford@ determined that notice and opportunity
comments. faa.gov. for public comment before issuing this
AD are impracticable and that good
SUMMARY: We are adopting a new SUPPLEMENTARY INFORMATION: cause exists for making this amendment
airworthiness directive (AD) for Stemme Discussion effective in fewer than 30 days.
AG TSA–M Models S6 and S6–RT Comments Invited
gliders. This AD results from mandatory The European Aviation Safety Agency
continuing airworthiness information (EASA), which is the Technical Agent This AD is a final rule that involves
(MCAI) issued by the aviation authority for the Member States of the European requirements affecting flight safety, and
of another country to identify and Community, has issued AD No.: 2015– we did not precede it by notice and
correct an unsafe condition on an 0034–E, dated February 27, 2015, opportunity for public comment. We
aviation product. The MCAI describes (referred to after this as ‘‘the MCAI’’), to invite you to send any written relevant
the unsafe condition as a bending defect correct an unsafe condition for the data, views, or arguments about this AD.
of the fork head installed in the aileron, specified products. The MCAI states: Send your comments to an address
speed brake, and flap control systems. A report was received concerning a broken listed under the ADDRESSES section.
We are issuing this AD to require fork head, installed in the speed brake Include ‘‘Docket No. FAA–2015–0633;
actions to address the unsafe condition control circuit of a TSA–M Model S6–RT Directorate Identifier 2015–CE–005–
on these products. powered sailplane. Preliminary investigation AD’’ at the beginning of your comments.
results revealed additional cases of bending We specifically invite comments on the
DATES: This AD is effective March 24, defect of the same part, which were installed
2015. overall regulatory, economic,
in the aileron and flaps control systems of the
We must receive comments on this TSA–M type design. The same fork heads are
environmental, and energy aspects of
AD by May 4, 2015. also installed in the control systems of ASP this AD. We will consider all comments
Model S15–1 aeroplanes. received by the closing date and may
ADDRESSES: You may send comments by amend this AD because of those
This condition, if not corrected, could lead
any of the following methods: to failure of the flight control system, comments.
• Federal eRulemaking Portal: Go to possibly resulting in loss of control of the We will post all comments we
http://www.regulations.gov. Follow the aeroplane. receive, without change, to http://
instructions for submitting comments. For the reasons described above, this AD www.regulations.gov, including any
• Fax: (202) 493–2251. prohibits the operation of the affected personal information you provide. We
• Mail: U.S. Department of aeroplanes pending the availability of a will also post a report summarizing each
Transportation, Docket Operations, M– modification of the affected flight control
systems in accordance with approved
substantive verbal contact we receive
30, West Building Ground Floor, Room about this AD.
W12–140, 1200 New Jersey Avenue SE., instructions.
Washington, DC 20590. This AD is a temporary measure and Costs of Compliance
• Hand Delivery: U.S. Department of further AD action may follow. You may We estimate that this AD will affect 6
Transportation, Docket Operations, M– examine the MCAI on the Internet at products of U.S. registry.
30, West Building Ground Floor, Room http://www.regulations.gov by searching At the time of issuance of this AD, no
W12–140, 1200 New Jersey Avenue SE., for and locating Docket No. FAA–2015– design solution is available to restore
Washington, DC 20590, between 9 a.m. 0633. the airworthiness of the respective type
and 5 p.m., Monday through Friday, designs to a level corresponding to their
FAA’s Determination and Requirements
except Federal holidays. approved type design specifications.
of the AD
For information concerning this Therefore, the FAA cannot determine
action, contact Stemme AG, This product has been approved by the cost of returning the affected gliders
Flugplatzstra+e F2, Nr. 6–7, D–15344 the aviation authority of another to service.
Strausberg, Germany; phone: +49 (0) country, and is approved for operation
3341/3612 0; fax: none; email: info@ in the United States. Pursuant to our Authority for This Rulemaking
stemme.de; internet: www.stemme.info. bilateral agreement with this State of Title 49 of the United States Code
Rmajette on DSK2VPTVN1PROD with RULES

Design Authority, they have notified us specifies the FAA’s authority to issue
Examining the AD Docket of the unsafe condition described in the rules on aviation safety. Subtitle I,
You may examine the AD docket on MCAI and service information section 106, describes the authority of
the Internet at http:// referenced above. We are issuing this the FAA Administrator. ‘‘Subtitle VII:
www.regulations.gov by searching for AD because we evaluated all Aviation Programs,’’ describes in more
and locating Docket No. FAA–2015– information provided by the State of detail the scope of the Agency’s
0633; or in person at the Docket Design Authority and determined the authority.

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Federal Register / Vol. 80, No. 53 / Thursday, March 19, 2015 / Rules and Regulations 14297

We are issuing this rulemaking under (b) Affected ADs (i) Related Information
the authority described in ‘‘Subtitle VII, None. (1) Refer to MCAI European Aviation
Part A, Subpart III, Section 44701: Safety Agency (EASA) AD No.: 2015–0034–
(c) Applicability E, dated February 27, 2015, for related
General requirements.’’ Under that
section, Congress charges the FAA with This AD applies to Stemme AG TSA–M information. You may examine the MCAI on
Models S6 and S6–RT gliders, all serial the Internet at http://www.regulations.gov by
promoting safe flight of civil aircraft in numbers, certificated in any category. searching for and locating Docket No. FAA–
air commerce by prescribing regulations 2015–0633.
for practices, methods, and procedures (d) Subject
(2) For information concerning this action,
the Administrator finds necessary for Air Transport Association of America contact Stemme AG, Flugplatzstra+e F2, Nr.
safety in air commerce. This regulation (ATA) Code 27: Flight Controls. 6–7, D–15344 Strausberg, Germany; phone:
is within the scope of that authority (e) Reason +49 (0) 3341/3612 0; fax: none; email: info@
because it addresses an unsafe condition stemme.de; internet: www.stemme.info.
This AD was prompted by mandatory
that is likely to exist or develop on continuing airworthiness information (MCAI) Issued in Kansas City, Missouri, on March
products identified in this rulemaking originated by an aviation authority of another 12, 2015.
action. country to identify and correct an unsafe Robert Busto,
condition on an aviation product. The MCAI Acting Manager, Small Airplane Directorate,
Regulatory Findings describes the unsafe condition as a bending Aircraft Certification Service.
We determined that this AD will not defect of the fork head installed in the
[FR Doc. 2015–06296 Filed 3–18–15; 8:45 am]
have federalism implications under aileron, speed brake, and flap control
Executive Order 13132. This AD will systems. We are issuing this AD to detect and BILLING CODE 4910–13–P

not have a substantial direct effect on correct the bending defect of the fork head
that could result in failure of the flight
the States, on the relationship between control system, possibly resulting in loss of DEPARTMENT OF TRANSPORTATION
the national government and the States, control.
or on the distribution of power and Federal Aviation Administration
responsibilities among the various (f) Actions and Compliance
levels of government. Unless already done, before further flight, 14 CFR Part 39
For the reasons discussed above, I after March 24, 2015 (the effective date of
certify that this AD: this AD), modify the affected flight control [Docket No. FAA–2014–0579; Directorate
(1) Is not a ‘‘significant regulatory systems, or take other actions, following a Identifier 2014–SW–020–AD; Amendment
method approved specifically for this AD by 39–18115; AD 2015–05–05]
action’’ under Executive Order 12866,
the FAA, Small Airplane Directorate. Contact
(2) Is not a ‘‘significant rule’’ under Stemme AG to obtain FAA-approved repair RIN 2120–AA64
the DOT Regulatory Policies and instructions approved specifically for
Procedures (44 FR 11034, February 26, compliance with this AD and incorporate Airworthiness Directives; Agusta
1979), those instructions. You can find contact S.p.A. Helicopters
(3) Will not affect intrastate aviation information for Stemme AG in paragraph
AGENCY: Federal Aviation
in Alaska, and (i)(2) of this AD.
(4) Will not have a significant Note 1 to paragraph (f) of this AD: At the Administration (FAA), DOT.
economic impact, positive or negative, time of issuance of this AD, no design ACTION: Final rule.
on a substantial number of small entities solution is available to restore the
airworthiness of the respective type designs SUMMARY: We are superseding
under the criteria of the Regulatory Airworthiness Directive (AD) 2014–04–
to a level corresponding to their approved
Flexibility Act. type design specifications. 14 for Agusta S.p.A. (Agusta) Model
List of Subjects in 14 CFR Part 39 (g) Other FAA AD Provisions
A109S, AW109SP, A119, and AW119
Air transportation, Aircraft, Aviation MKII helicopters. AD 2014–04–14
The following provisions also apply to this
safety, Incorporation by reference, required removing certain rod end
AD:
Safety. (1) Alternative Methods of Compliance assemblies from service because of
(AMOCs): The Manager, Standards Office, reports of fractures. This new AD retains
Adoption of the Amendment FAA, has the authority to approve AMOCs the requirements of AD 2014–04–14 but
Accordingly, under the authority for this AD, if requested using the procedures expands the scope of applicable rod end
delegated to me by the Administrator, found in 14 CFR 39.19. Send information to assemblies. This AD was prompted by
ATTN: Jim Rutherford, Aerospace Engineer, reports of additional fractured rod end
the FAA amends 14 CFR part 39 as
FAA, Small Airplane Directorate, 901 Locust, assemblies. We are issuing this AD to
follows: Room 301, Kansas City, Missouri 64106; prevent failure of a rod end assembly,
telephone: (816) 329–4165; fax: (816) 329–
PART 39—AIRWORTHINESS 4090; email: jim.rutherford@faa.gov. Before which could result in damage to the
DIRECTIVES using any approved AMOC on any airplane main rotor assembly and loss of control
to which the AMOC applies, notify your of the helicopter.
■ 1. The authority citation for part 39 appropriate principal inspector (PI) in the DATES: This AD is effective April 23,
continues to read as follows: FAA Flight Standards District Office (FSDO), 2015.
Authority: 49 U.S.C. 106(g), 40113, 44701. or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement ADDRESSES: For service information
§ 39.13 [Amended] in this AD to obtain corrective actions from identified in this AD, contact
a manufacturer or other source, use these AgustaWestland, Product Support
■ 2. The FAA amends § 39.13 by adding
actions if they are FAA-approved. Corrective Engineering, Via del Gregge, 100, 21015
the following new AD:
Rmajette on DSK2VPTVN1PROD with RULES

actions are considered FAA-approved if they Lonate Pozzolo (VA) Italy, ATTN:
2015–06–03 Stemme AG: Amendment 39– are approved by the State of Design Authority Maurizio D’Angelo; telephone 39–0331–
18121; Docket No. FAA–2015–0633; (or their delegated agent). You are required 664757; fax 39–0331–664680; or at
Directorate Identifier 2015–CE–005–AD. to assure the product is airworthy before it
is returned to service. http://www.agustawestland.com/
(a) Effective Date technical-bulletins. You may view this
This airworthiness directive (AD) becomes (h) Special Flight Permit referenced service information at the
effective March 24, 2015. Special flight permits are prohibited. FAA, Office of the Regional Counsel,

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Document Created: 2018-02-21 09:42:02
Document Modified: 2018-02-21 09:42:02

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Rules and Regulations
Action		Final rule; request for comments.
Dates		This AD is effective March 24, 2015.
Contact		Jim Rutherford, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090; email: [email protected]
FR Citation		80 FR 14296
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

80 FR 14296 - Airworthiness Directives; Stemme AG Gliders

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 80, Issue 53 (March 19, 2015)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration