AD 2022-06-04 ACTIVE

The FAA is adopting a new airworthiness directive (AD) for certain Schempp-Hirth Flugzeugbau GmbH Model Janus, Mini-Nimbus HS-7, Nimbus-2, and Standard Cirrus gliders. 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 disconnected pendulum elevator. This AD requires installing colored markings and revising the existing aircraft flight manual (FM) and service manual (SM). The FAA is issuing this AD to address the unsafe condition on these products.

Final rule.

1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2022-06-04 Schempp-Hirth Flugzeugbau GmbH: Amendment 39-21970; Docket No. FAA-2021-1170; Project Identifier MCAI-2020-01572-G. (a) Effective Date This airworthiness directive (AD) is effective May 9, 2022. (b) Affected ADs None. (c) Applicability This AD applies to Schempp-Hirth Flugzeugbau GmbH Model Janus, Mini-Nimbus HS-7, Nimbus-2, and Standard Cirrus gliders, with a serial number listed in Schempp-Hirth Flugzeugbau GmbH Technical Note No. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document), certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code 2700, Flight Control System. (e) Unsafe Condition 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 disconnected pendulum elevator. The FAA is issuing this AD to prevent an improperly locked elevator attachment. The unsafe condition, if not addressed, could result in failure of the elevator connection and loss of control of the glider. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 90 days after the effective date of this AD, do the following actions concurrently. (1) Install colored markings on the elevator in accordance with Action 1 in Schempp-Hirth Flugzeugbau GmbH Technical Note No. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document). (2) Revise the existing aircraft flight manual (FM) and service manual (SM) for your glider by replacing the pages specified in Action 2 in Schempp-Hirth Flugzeugbau GmbH Technical Note No. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document), as applicable to your glider, with the revised pages for the manual applicable to your glider dated June 2020. (3) The action required by paragraph (g)(2) of this AD may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417. (h) Alternative Methods of Compliance (AMOCs) (1) The Manager, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph (i)(1) of this AD and email to: 9-AVS-AIR-730-AMOC@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (i) Related Information (1) For more information about this AD, contact Jim Rutherford, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 901 Locust, Room 301, Kansas City, MO 64106; phone: (816) 329-4165; email: jim.rutherford@faa.gov. (2) Refer to European Union Aviation Safety Agency (EASA) AD 2020-0260, dated November 26, 2020, for more information. You may examine the EASA AD in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-1170. (j) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference 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. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document). Note 1 to paragraph (j)(2)(i): This service information contains German to English translation. EASA used the English translation in referencing the document from Schempp-Hirth Flugzeugbau GmbH. For enforceability purposes, the FAA will cite references to the service information in English as it appears on the document. (ii) [Reserved] (3) For service information identified in this AD, contact Schempp-Hirth Flugzeugbau GmbH, Krebenstrasse 25, 73230 Kirchheim/Teck, Germany; phone: +49 7021 7298-0; fax: +49 7021 7298-199; email: info@schempp-hirth.com; website: https://www.schempp-hirth.com. (4) You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. (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, email: fr.inspection@nara.gov, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued on March 10, 2022. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022-06959 Filed 4-1-22; 8:45 am]BILLING CODE 4910-13-P

Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain serial-numbered Schempp-Hirth Flugzeugbau GmbH Model Janus, Mini-Nimbus HS-7, Nimbus-2, and Standard Cirrus gliders. The NPRM published in the Federal Register on January 3, 2022 (87 FR 55). The NPRM was prompted by MCAI originated by the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union. EASA issued AD 2020-0260, dated November 26, 2020 (referred to after this as "the MCAI"), to address an unsafe condition on certain serial numbered Schempp-Hirth Flugzeugbau GmbH Model Janus, Mini-Nimbus HS 7, Nimbus-2, Standard Cirrus, Standard Cirrus B, Standard Cirrus CS 11-75L, and Nimbus-2M gliders. The MCAI states: During an aero tow of a Standard Cirrus, the pendulum elevator disconnected. The technical investigation concluded that the elevator attachment was not properly locked. Due to similarity of design, this kind of event could also occur on other Schempp-Hirth sailplanes, including Nimbus-2M powered sailplanes. This condition, if not corrected, could lead to failure of the elevator connection and loss of control of the (powered) sailplane. To address this potential unsafe condition, Schempp-Hirth published the [technical note] TN, providing instructions to install an optical indicator and to update the Aircraft Flight Manual (AFM). For the reasons described above, this [EASA] AD requires installation of an optical indicator and amendment of the AFM. You may examine the MCAI in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-1170. Discussion of Final Airworthiness Directive Comments The FAA received no comments on the NPRM or on the determination of the costs. Conclusion This product has been approved by the aviation authority of another country and is approved for operation in the United States. Pursuant to the FAA's bilateral agreement with this State of Design Authority, it has notified the FAA of the unsafe condition described in the MCAI referenced above. The FAA reviewed the relevant data and determined that air safety requires adopting this AD as proposed. Accordingly, the FAA is issuing this AD to address the unsafe condition on these products. This AD is adopted as proposed in the NPRM. Related Service Information Under 1 CFR Part 51 The FAA reviewed Schempp-Hirth Flugzeugbau GmbH Technical Note No. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document). The service information specifies procedures for installing colored markings to the top of the elevator on both sides of the locking mechanism and revising the existing aircraft FM and SM. 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. Differences Between This AD and the MCAI The MCAI applies to Schempp-Hirth Flugzeugbau GmbH Model Standard Cirrus B, Standard Cirrus CS 11-75L, and Nimbus-2M gliders, and this AD does not because these models do not have an FAA type certificate. Costs of Compliance The FAA estimates that this AD affects 87 gliders of U.S. registry. The FAA estimates the following costs to comply with this AD: Estimated Costs Action Labor cost Parts cost Cost per product Cost on U.S. operators Install markings 1 work-hour × $85 per hour = $85 $10 $95 $8,265 Revise FM and SM 1 work-hour × $85 per hour = $85 0 85 7,395 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. The FAA is 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 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) Will not affect intrastate aviation in Alaska, 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. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. 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 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2022-06-04 Schempp-Hirth Flugzeugbau GmbH: Amendment 39-21970; Docket No. FAA-2021-1170; Project Identifier MCAI-2020-01572-G. (a) Effective Date This airworthiness directive (AD) is effective May 9, 2022. (b) Affected ADs None. (c) Applicability This AD applies to Schempp-Hirth Flugzeugbau GmbH Model Janus, Mini-Nimbus HS-7, Nimbus-2, and Standard Cirrus gliders, with a serial number listed in Schempp-Hirth Flugzeugbau GmbH Technical Note No. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document), certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code 2700, Flight Control System. (e) Unsafe Condition 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 disconnected pendulum elevator. The FAA is issuing this AD to prevent an improperly locked elevator attachment. The unsafe condition, if not addressed, could result in failure of the elevator connection and loss of control of the glider. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 90 days after the effective date of this AD, do the following actions concurrently. (1) Install colored markings on the elevator in accordance with Action 1 in Schempp-Hirth Flugzeugbau GmbH Technical Note No. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document). (2) Revise the existing aircraft flight manual (FM) and service manual (SM) for your glider by replacing the pages specified in Action 2 in Schempp-Hirth Flugzeugbau GmbH Technical Note No. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document), as applicable to your glider, with the revised pages for the manual applicable to your glider dated June 2020. (3) The action required by paragraph (g)(2) of this AD may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417. (h) Alternative Methods of Compliance (AMOCs) (1) The Manager, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph (i)(1) of this AD and email to: 9-AVS-AIR-730-AMOC@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (i) Related Information (1) For more information about this AD, contact Jim Rutherford, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 901 Locust, Room 301, Kansas City, MO 64106; phone: (816) 329-4165; email: jim.rutherford@faa.gov. (2) Refer to European Union Aviation Safety Agency (EASA) AD 2020-0260, dated November 26, 2020, for more information. You may examine the EASA AD in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-1170. (j) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference 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. 278-40/286-36/295-33/328-14/798-4, Revision 1, dated November 12, 2020 (issued as one document). Note 1 to paragraph (j)(2)(i): This service information contains German to English translation. EASA used the English translation in referencing the document from Schempp-Hirth Flugzeugbau GmbH. For enforceability purposes, the FAA will cite references to the service information in English as it appears on the document. (ii) [Reserved] (3) For service information identified in this AD, contact Schempp-Hirth Flugzeugbau GmbH, Krebenstrasse 25, 73230 Kirchheim/Teck, Germany; phone: +49 7021 7298-0; fax: +49 7021 7298-199; email: info@schempp-hirth.com; website: https://www.schempp-hirth.com. (4) You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. (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, email: fr.inspection@nara.gov, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued on March 10, 2022. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.

For service information identified in this final rule, contact Schempp-Hirth Flugzeugbau GmbH, Krebenstrasse 25, 73230 Kirchheim/Teck, Germany; phone: +49 7021 7298-0; fax: +49 7021 7298-199; email: info@schempp-hirth.com; website: https://www.schempp-hirth.com. You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. It is also available at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-1170.

Jim Rutherford, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 901 Locust, Room 301, Kansas City, MO 64106; phone: (816) 329-4165; email: jim.rutherford@faa.gov.