[Federal Register Volume 80, Number 216 (Monday, November 9, 2015)]
[Rules and Regulations]
[Pages 69113-69115]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-28339]


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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 Gliders

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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SUMMARY: The FAA is correcting an airworthiness directive (AD) that 
published in the Federal Register. That AD applies to certain Schempp-
Hirth Flugzeugbau GmbH Models Duo Discus and Duo Discus T gliders. The 
Model Duo Discus gliders were incorrectly referenced as powered 
sailplanes in the Applicability section. This document corrects that 
error and refers to both models as just gliders as in previous ADs. In 
all other respects, the original document remains the same; however we 
are publishing the entire rule in the Federal Register.

DATES: This final rule is effective 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 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 address for the Docket Office (phone: 800-647-
5527) is 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 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: Airworthiness Directive 2015-20-11, 
Amendment 39-18290 (80 FR 61722, October 14, 2015), currently requires 
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.

[[Page 69114]]

    As published, the Model Duo Discus gliders were incorrectly 
referenced as powered sailplanes in the Applicability section. This 
could cause confusion because the Model Duo Discus does not have an 
engine. This document corrects that error and refers to both models as 
just gliders as in previous ADs.
    Although no other part of the preamble or regulatory information 
has been corrected, we are publishing the entire rule in the Federal 
Register.
    The effective date of this AD remains November 18, 2015.

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 on November 
18, 2015.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Schempp-Hirth Flugzeugbau GmbH Model Duo 
Discus gliders, serial numbers 1 through 639, and Model Duo Discus T 
gliders, 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 18, 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 18, 
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 18, 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: 
[email protected]. Before using any approved AMOC on any glider 
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.

(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,

[[Page 69115]]

Krebenstrasse 25, 73230 Kirchheim/Teck, Germany; telephone: +49 7021 
7298-0; fax: +49 7021 7298-199; email: 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 November 2, 2015.
Melvin Johnson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-28339 Filed 11-6-15; 8:45 am]
 BILLING CODE 4910-13-P