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[Federal Register Volume 80, Number 198 (Wednesday, October 14, 2015)]
[Rules and Regulations]
[Pages 61722-61725]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-25710]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-3224; Directorate Identifier 2015-CE-026-AD; 
Amendment 39-18290; AD 2015-20-11]
RIN 2120-AA64

Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH 
Sailplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for 
Schempp-Hirth Flugzeugbau GmbH Models Duo Discus and Duo Discus T 
powered sailplanes. This AD results from mandatory continuing 
airworthiness information (MCAI) issued 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 excessive 
load on the air brake system. We are issuing this AD to require actions 
to address the unsafe condition on these products.

DATES: This AD is effective November 18, 2015.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in the AD as of November 18, 
2015.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015-
3224; or in person at Document Management Facility, U.S. Department of 
Transportation, Docket Operations, M-30, West Building Ground Floor, 
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
    For service information identified in this AD, contact Schempp-
Hirth Flugzeugbau GmbH, Krebenstrasse 25, 73230 Kirchheim/Teck, 
Germany; telephone: +49 7021 7298-0; fax: +49 7021 7298-199; email: 
/hirth.com">hirth.com">info@schempp-hirth.com; Internet: http://

[[Page 61723]]

www.schempp-hirth.com. You may view this referenced service information 
at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, 
Missouri 64106. For information on the availability of this material at 
the FAA, call (816) 329-4148. It is also available on the Internet at 
http://www.regulations.gov by searching for Docket No. FAA-2015-3224.

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: 
jim.rutherford@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to add an AD that would apply to Schempp-Hirth Flugzeugbau GmbH 
Models Duo Discus and Duo Discus T powered sailplanes. The NPRM was 
published in the Federal Register on August 4, 2015 (80 FR 46206). The 
NPRM proposed to correct an unsafe condition for the specified products 
and was based on mandatory continuing airworthiness information (MCAI) 
originated by an aviation authority of another country. The MCAI 
states:

    Operational experience shows that application of an excessive 
load on the air brake system may induce damage to the drive funnels 
in the fuselage and to the air brake bellcrank at the root rips of 
the wing.
    This condition, if not detected and corrected, could lead to an 
uncontrolled actuation of the air brakes (symmetric and asymmetric), 
possibly resulting in reduced control of the (powered) sailplane.
    To address this potential unsafe condition, Schempp-Hirth 
Flugzeugbau GmbH issued Technical Note (TN) 380-2, 396-17, 868-22 
and 890-14 (published as a single document) to provide inspection 
instructions.
    Consequently EASA issued AD 2015-0139 to require to repetitive 
inspections of the air brake bellcrank, the air brake drive funnels 
and the airbrake control system, and replacement of damaged parts.
    Since that AD was issued, it was found that the drawing number 
of the reinforced air brake drive funnel was incorrectly stated in 
the original issue of the Schempp-Hirth TN. The wrongly referred 
drawing S14FB703 refers to an existing part, different from air 
brake drive funnel and cannot be installed as a replacement part for 
air brake drive funnel. Consequently, Schempp-Hirth Flugzeugbau GmbH 
issued Revision 1 of TN 380-2, 396-17, 868-22 and 890-14, hearafter 
referenced to as `the revised TN' in this AD.
    For the reasons described above, this AD is revised to require 
using the revised TN.

The MCAI can be found in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2015-3224-0002.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM (80 FR 46206, August 4, 
2015) or on the determination of the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting the AD as proposed except for 
minor editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM (80 FR 46206, August 4, 2015) for correcting the unsafe condition; 
and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM (80 FR 46206, August 4, 2015).

Related Service Information Under 1 CFR Part 51

    We reviewed Schempp-Hirth Flugzeugbau GmbH Technical Note No. 380-
2/396-17/868-22/890-14, Revision 1, issued July 13, 2015 (published as 
a single document), and Working instruction for Technical Note No. 380-
2/396-17/868-22/890-14, Ausgabe (English translation: issue) 1, Datum 
(English translation: dated) May 11, 2015. The service information 
describes procedures for inspecting and replacing the airbrake bell 
crank and the airbrake drive funnels and inspecting the airbrake 
control system for proper clearance and making necessary adjustments. 
This service information is reasonably available because the interested 
parties have access to it through their normal course of business or by 
the means identified in the ADDRESSES section of the AD.

Costs of Compliance

    We estimate that this AD will affect 31 products of U.S. registry. 
We also estimate that it will take about 2 work-hours per product to 
comply with the basic inspection requirements of this AD. The average 
labor rate is $85 per work-hour.
    Based on these figures, we estimate the cost of this portion of the 
AD on U.S. operators to be $5,270, or $170 per product.
    We estimate that it will take about 4 work-hours per product to 
comply with the airbrake bell crank replacement requirement of this AD. 
The average labor rate is $85 per work-hour. Required parts will cost 
about $500 per product.
    Based on these figures, we estimate the cost of this portion of the 
AD on U.S. operators to be $26,040, or $840 per product.
    We estimate that it will take about 4 work-hours per product to 
comply with the airbrake drive funnel replacement requirement of this 
AD. The average labor rate is $85 per work-hour. Required parts will 
cost about $500 per product.
    Based on these figures, we estimate the cost of this portion of the 
AD on U.S. operators to be $26,040, or $840 per product.
    In addition, we estimate that any necessary follow-on actions to 
make any necessary adjustments to the airbrake control system will take 
about 2 work-hours for a cost of $170 per product. We have no way of 
determining the number of products that may need these actions.

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.
    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 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

[[Page 61724]]

    (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.

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-
3224; 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 the NPRM, 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.

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:

2015-20-11 Schempp-Hirth Flugzeugbau GmbH: Amendment 39-18290; 
Docket No. FAA-2015-3224; Directorate Identifier 2015-CE-026-AD.

(a) Effective Date

    This airworthiness directive (AD) becomes effective November 18, 
2015.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Schempp-Hirth Flugzeugbau GmbH Model Duo 
Discus powered sailplanes, serial numbers 1 through 639, and Model 
Duo Discus T powered sailplanes, serial numbers 1 through 110 and 
112 through 247, 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 excessive load 
on the air brake system. We are issuing this AD to prevent 
uncontrolled actuation of the air brakes (symmetric or asymmetric), 
which could result in reduced control.

(f) Actions and Compliance

    Unless already done, do the actions in paragraph (f)(1) through 
(f)(5) of this AD.
    (1) Within 40 days after November 17, 2015 (the effective date 
of this AD) and repetitively thereafter at intervals not to exceed 
100 hours time-in-service until the terminating replacement action 
required in paragraphs (f)(2) and (f)(3) of this AD (as applicable) 
is done, inspect the airbrake bell crank, the airbrake drive 
funnels, and the airbrake control system.
    (i) Inspect the airbrake bell crank and the airbrake drive 
funnels for cracks and damage following Action 1 in Schempp-Hirth 
Flugzeugbau GmbH Technical Note No. 380-2/396-17/868-22/890-14, 
Revision 1, issued July 13, 2015 (published as a single document).
    (ii) Inspect the airbrake control system for proper clearance 
following Paragraph 2.d. of Schempp-Hirth Flugzeugbau GmbH Working 
instruction for Technical Note No. 380-2/396-17/868-22/890-14, 
Ausgabe (English translation: issue) 1, Datum (English translation: 
dated) May 11, 2015.
    (2) If cracks or damage is found on the airbrake bell cranks or 
the airbrake drive funnels during any inspection required in 
paragraph (f)(1) of this AD, before further flight, replace each 
cracked or damaged part with a reinforced part. Installing a 
reinforced part terminates the repetitive inspections required in 
paragraph (f)(1) of this AD for that part.
    (i) For replacement of the airbrake bell cranks, follow Picture 
2: Reinforced version of airbrake bell crank according to HS 11-
50.016, Revision a or later, in Schempp-Hirth Flugzeugbau GmbH 
Working instruction for Technical Note No. 380-2/396-17/868-22/890-
14, Ausgabe (English translation: issue) 1, Datum (English 
translation: dated) May 11, 2015.
    (ii) For replacement of the airbrake drive funnels, follow 
Picture 5: Airbrake drive funnel in fuselage ``Reinforcement of 
airbrake drive funnel according to drawing S14RB703, Revision a, in 
Schempp-Hirth Flugzeugbau GmbH Working instruction for Technical 
Note No. 380-2/396-17/868-22/890-14, Ausgabe (English translation: 
issue) 1, Datum (English translation: dated) May 11, 2015.
    (3) If no cracks or damage were found on the airbrake bell 
cranks or the airbrake drive funnels during any inspection required 
in paragraph (f)(1) of this AD, within 12 months after November 17, 
2015 (the effective date of this AD), replace each of the airbrake 
bell cranks and airbrake drive funnels with a reinforced part. These 
replacements terminate the repetitive inspections required in 
paragraph (f)(1) of this AD.
    (i) For replacement of the airbrake bell cranks, follow Picture 
2: Reinforced version of airbrake bell crank according to HS 11-
50.016, Revision a or later, in Schempp-Hirth Flugzeugbau GmbH 
Working instruction for Technical Note No. 380-2/396-17/868-22/890-
14, Ausgabe (English translation: issue) 1, Datum (English 
translation: dated) May 11, 2015.
    (ii) For replacement of the airbrake drive funnels, follow 
Picture 5: Airbrake drive funnel in fuselage, ``Reinforcement of 
airbrake drive funnel according to drawing S14RB703, Revision a,'' 
in Schempp-Hirth Flugzeugbau GmbH Working instruction for Technical 
Note No. 380-2/396-17/868-22/890-14, Ausgabe (English translation: 
issue) 1, Datum (English translation: dated) May 11, 2015.
    (4) If the airbrake control system is found to not have proper 
clearance during the inspection required in paragraph (f)(1) of this 
AD, before further flight, make all necessary corrective adjustments 
following Paragraph 2.d. of Schempp-Hirth Flugzeugbau GmbH Working 
instruction for Technical Note No. 380-2/396-17/868-22/890-14, 
Ausgabe (English translation: issue) 1, Datum (English translation: 
dated) May 11, 2015.
    (5) As of November 17, 2015 (the effective date of this AD), 
only install an airbrake bell crank or an airbrake drive funnel that 
corresponds to Picture 2: Reinforced version of airbrake bell crank 
according to HS 11-50.016, Revision a or later, and Picture 5: 
Airbrake drive funnel in fuselage, ``Reinforcement of airbrake drive 
funnel according to drawing S14RB703, Revision a,'' in Schempp-Hirth 
Flugzeugbau GmbH Working instruction for Technical Note No. 380-2/
396-17/868-22/890-14, Ausgabe (English translation: issue) 1, Datum 
(English translation: dated) May 11, 2015, as applicable.

(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: 
jim.rutherford@faa.gov. Before using any approved AMOC on any 
sailplane 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) Related Information

    Refer to MCAI European Aviation Safety Agency (EASA) AD No. 
2015-0139R1, dated July 15, 2015, for related information. You may 
examine the MCAI on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2015-3224-0002.

[[Page 61725]]

(i) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (i) Schempp-Hirth Flugzeugbau GmbH Technical Note No. 380-2/396-
17/868-22/890-14, Revision 1, issued July 13, 2015 (published as a 
single document).
    (ii) Schempp-Hirth Flugzeugbau GmbH Working instruction for 
Technical Note No. 380-2/396-17/868-22/890-14, Ausgabe (English 
translation: issue) 1, Datum (English translation: dated) May 11, 
2015.
    (3) For Schempp-Hirth Flugzeugbau GmbH service information 
identified in this AD, contact Schempp-Hirth Flugzeugbau GmbH, 
Krebenstrasse 25, 73230 Kirchheim/Teck, Germany; telephone: +49 7021 
7298-0; fax: +49 7021 7298-199; email: /hirth.com">hirth.com">info@schempp-hirth.com; 
Internet: http://www.schempp-hirth.com.
    (4) You may view this service information at the FAA, Small 
Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For 
information on the availability of this material at the FAA, call 
(816) 329-4148. In addition, you can access this service information 
on the Internet at http://www.regulations.gov by searching for and 
locating Docket No. FAA-2015-3224.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Kansas City, Missouri, on October 1, 2015.
Melvin Johnson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.

[FR Doc. 2015-25710 Filed 10-13-15; 8:45 am]
BILLING CODE 4910-13-P
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