Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter Deutschland GmbH) Helicopters, 13975-13982 [2021-05146]

Download as PDF Federal Register / Vol. 86, No. 47 / Friday, March 12, 2021 / Rules and Regulations Issued on February 17, 2021. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. availability of this material at the FAA, call 817–222–5110. [FR Doc. 2021–05142 Filed 3–11–21; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2015–4497; Project Identifier 2016–SW–011–AD; Amendment 39–21450; AD 2021–05–07] RIN 2120–AA64 Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter Deutschland GmbH) Helicopters Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: The FAA is adopting a new airworthiness directive (AD) for Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model BO–105A, BO– 105C, BO–105S, MBB–BK 117 A–1, MBB–BK 117 A–3, MBB–BK 117 A–4, MBB–BK 117 B–1, MBB–BK 117 B–2, and MBB–BK 117 C–1 helicopters. This AD was prompted by a report of a loss of electrical ground between the startergenerator and the generator voltage regulator (regulator). This AD requires inspecting the starter-generator electrical ground connection, retrofitting the starter-generator wire harness, and depending on model, revising the existing Rotorcraft Flight Manual (RFM) for your helicopter. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 16, 2021. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of April 16, 2021. ADDRESSES: For Eurocopter service information identified in this final rule, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052; telephone 972–641–0000 or 800–232– 0323; fax 972–641–3775; or at https:// www.airbus.com/helicopters/services/ technical-support.html. You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. For information on the SUMMARY: VerDate Sep<11>2014 19:32 Mar 11, 2021 Jkt 253001 Examining the AD Docket You may examine the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2015– 4497; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, any comments received, and other information. The street address for Docket Operations is 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: Ronnea L. Derby, Aerospace Engineer, Denver ACO Branch, FAA, 26805 East 68th Ave., Room 214, Denver, CO 80249; telephone 303–342–1093; email ronnea.l.derby.@faa.gov. SUPPLEMENTARY INFORMATION: Discussion The European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2015–0098, dated June 2, 2015 (EASA AD 2015–0098), and EASA AD 2015– 0220, dated November 9, 2015 (EASA AD 2015–0220) (also referred to as the Mandatory Continuing Airworthiness Information, or the MCAI), to correct an unsafe condition for all Airbus Helicopters Model MBB–BK117 A–1, MBB–BK117 A–3, MBB–BK117 A–4, MBB–BK117 B–1, MBB–BK117 B–2, and MBB–BK117 C–1 helicopters; and Airbus Helicopters Model BO105 A, BO105 C, BO105 D and BO105 S helicopters with certain part-numbered voltage regulators. The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Airbus Helicopters Model BO–105A, BO–105C, and BO– 105S helicopters; and all Airbus Helicopters Model MBB–BK 117 A–1, MBB–BK 117 A–3, MBB–BK 117 A–4, MBB–BK 117 B–1, MBB–BK 117 B–2, and MBB–BK 117 C–1 helicopters. The NPRM published in the Federal Register on July 16, 2020 (85 FR 43153). The NPRM was prompted by a report of a loss of electrical ground between the starter-generator and the regulator. The NPRM proposed to require inspecting the starter-generator electrical ground connection, retrofitting the startergenerator wire harness, and depending on model, revising the existing RFM for your helicopter. PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 13975 The FAA is issuing this AD to address the loss of electrical ground between the starter-generator and the regulator. This condition could result in an overvoltage of electrical power, damage to electronic equipment, and subsequent loss of control of the helicopter. Comments The FAA gave the public the opportunity to participate in developing this final rule. The FAA received no comments on the NPRM or on the determination of the cost to the public. Conclusion The FAA reviewed the relevant data and determined that air safety and the public interest require adopting this final rule as proposed, except for minor editorial changes. The FAA has determined that these minor changes: • Are consistent with the intent that was proposed in the NPRM for addressing the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the NPRM. Related Service Information Under 1 CFR Part 51 Eurocopter (now Airbus Helicopters) issued Alert Service Bulletin ASB– MBB–BK117–90–118, Revision 2, dated May 4, 2009, for certain Model MBB– BK117 helicopters and Alert Service Bulletin ASB BO105–90–103, Revision 4, dated June 21, 2010, for certain Model BO105 helicopters. This service information specifies a visual inspection for damage, corrosion, and cracks and measuring the resistance of the left-hand and right-hand electrical ground connections between each startergenerator and the regulator. If there is damage or suspected damage, or if the resistance is out of tolerance, this service information specifies replacing the wire terminal. This service information also specifies performing the visual inspection and resistance measurement each time the starter generator is removed or the wiring is disconnected until a retrofit ground connection is installed. These documents are distinct since they apply to different models. Eurocopter also issued Eurocopter Flight Manual BK117 A–3 Temporary Revision 9, Eurocopter Flight Manual BK117 A–4 Temporary Revision 5, Eurocopter Flight Manual BK117 B–1 Temporary Revision 6, Eurocopter Flight Manual BK 117 B–2 Temporary Revision 1, and Eurocopter Flight Manual BK 117 C–1 Temporary Revision 2, all dated September 22, 2006, to provide updated procedures in the event of a generator failure. These E:\FR\FM\12MRR1.SGM 12MRR1 13976 Federal Register / Vol. 86, No. 47 / Friday, March 12, 2021 / Rules and Regulations documents are distinct since they apply to different models. 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. Other Related Service Information Eurocopter (now Airbus Helicopters) issued Service Bulletin SB BO105–90– 104, Revision 1, dated June 21, 2010, for certain Model BO105 helicopters. This service information specifies procedures for installing a retrofit ground connection of the starter-generator. Eurocopter issued Alert Service Bulletin ASB–BO 105–80–118, Revision 1, dated November 29, 1995, and Service Bulletin SB–BO105–80–119, dated November 7, 1994, both for certain Model BO105 helicopters. This service information specifies retrofitting certain helicopters with voltage regulators that incorporate overvoltage protection by modifying the main relay box, modifying the overhead panel, and performing a functional test. Eurocopter issued Information Notice 2370–I–24, Revision 0, dated November 15, 2011, for certain Model BO105 helicopters to provide notice that a modified starter-generator may only be installed on helicopters that have also been modified. This service information states that combining modified with non-modified can cause overvoltage in the electrical system during the first ground run following engine replacement and subsequent damage to electronic equipment. This service information also recommends retrofitting all helicopters approved to only fly under visual flight rules. Differences Between This AD and the EASA ADs The EASA ADs require visually inspecting the wire terminals for damage, corrosion, and cracks. This AD requires visually inspecting for a crack, a kink, fraying, looseness, missing material, and corrosion. The EASA ADs require repeating the visual inspection and resistance measurement each time a startergenerator is removed or the wiring is disconnected from a starter-generator. This AD does not because such a compliance time would be difficult to enforce. EASA AD 2015–0220 requires additional actions for Model BO–105 helicopters with a serial number up to 0160 than for helicopters with a serial number 0161 and larger. This AD requires the same actions for all Model BO–105 helicopters regardless of serial number. VerDate Sep<11>2014 19:32 Mar 11, 2021 Jkt 253001 EASA AD 2015–0220 allows credit for complying with Eurocopter Alert Service Bulletin ASB BO105–90–103, Revision 2 or Revision 3, whereas this AD does not. Costs of Compliance The FAA estimates that this AD affects 40 Model BO–105 helicopters and 44 Model MBB–BK 117 helicopters of U.S. Registry. The FAA estimates that operators may incur the following costs in order to comply with this AD using an estimated labor cost of $85 per workhour. Performing a visual inspection and resistance measurement of the electrical ground connection takes about 2 workhours for an estimated cost of $170 per helicopter and $14,280 for the U.S. fleet per inspection and measurement. Performing the retrofit of the wiring harness takes about 10 work-hours. Required parts for a Model BO–105 helicopter cost $2,509 for an estimated replacement cost of $3,359 per helicopter and $134,360 for the U.S. fleet. Required parts for a Model MBB– BK 117 helicopter cost $1,730 for an estimated replacement cost of $2,580 per helicopter and $113,520 for the U.S. fleet. Revising the existing RFM for Model MBB–BK 117 helicopters takes about 0.5 work-hour, for an estimated cost of $43 per helicopter and $1,892 for the U.S. fleet. 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 PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 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) 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. 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 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: ■ 2021–05–07 Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter Deutschland GmbH): Amendment 39– 21450; Docket No. FAA–2015–4497; Project Identifier 2016–SW–011–AD. (a) Effective Date This airworthiness directive (AD) is effective April 16, 2021. (b) Affected ADs None. (c) Applicability This AD applies to the following Airbus Helicopters Deutschland GmbH (Type Certificate previously held by Eurocopter Deutschland GmbH) helicopters, certificated in any category: (1) Model BO–105A, BO–105C, and BO– 105S helicopters with a voltage regulator part number (P/N) 51565–000, 51565–000R, or 51509–002R installed; and (2) Model MBB–BK 117 A–1, MBB–BK 117 A–3, MBB–BK 117 A–4, MBB–BK 117 B–1, MBB–BK 117 B–2, and MBB–BK 117 C–1 helicopters. (d) Subject Joint Aircraft Service Component (JASC) Code: 2497, Electrical Power System Wiring. (e) Unsafe Condition This AD was prompted by a report of a loss of electrical ground between the starter- E:\FR\FM\12MRR1.SGM 12MRR1 Federal Register / Vol. 86, No. 47 / Friday, March 12, 2021 / Rules and Regulations generator and the generator voltage regulator (regulator). The FAA is issuing this AD to address loss of electrical ground between the starter-generator and the regulator. This condition could result in an overvoltage of electrical power, damage to electronic equipment, and subsequent loss of control of the helicopter. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions (1) Within 50 hours time-in-service (TIS): (i) Visually inspect the wire terminal of wire P55F16N/P56F16N for Model BO–105A, BO–105C, and BO–105S helicopters and wire 1PA53B20/2PA53B20 for Model MBB–BK 117 A–1, MBB–BK 117 A–3, MBB–BK 117 A–4, MBB–BK 117 B–1, MBB–BK 117 B–2, and MBB–BK 117 C–1 helicopters on Terminal E of each starter-generator for a crack, a kink, fraying, looseness, missing material, and corrosion. If there is a crack, a kink, fraying, looseness, missing material, or any corrosion, before further flight, replace the wire terminal. VerDate Sep<11>2014 19:32 Mar 11, 2021 Jkt 253001 (ii) Measure the resistance between each starter-generator and its regulator in accordance with the Accomplishment Instructions, paragraph 2.A.2.3. of Eurocopter Alert Service Bulletin ASB BO105–90–103, Revision 4, dated June 21, 2010, or paragraphs 2.A.2.3. and 2.A.2.5. of Eurocopter Alert Service Bulletin ASB– MBB–BK117–90–118, Revision 2, dated May 4, 2009, as applicable to your model helicopter. If the resistance is more than 500 milliohms, before further flight, replace the wire terminal. (2) Within 150 hours TIS: (i) Install a wire harness from each generator voltage regulator as follows. (A) For Model BO–105A, BO–105C, and BO–105S helicopters: Wire harness P/N 105– 90081. (B) For Model MBB–BK 117 A–1, MBB–BK 117 A–3, MBB–BK 117 A–4, MBB–BK 117 B– 1, and MBB–BK 117 B–2 helicopters: Wire harness P/N 117–901941. (C) For Model MBB–BK 117 C–1 helicopters: Wire harness P/N 117–901961. (ii) For Model MBB–BK 117 A–3, MBB–BK 117 A–4, MBB–BK 117 B–1, MBB–BK 117 B– 2, and MBB–BK 117 C–1 helicopters, revise PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 13977 the existing Rotorcraft Flight Manual (RFM) for your helicopter to include the information in Section 3 Emergency and Malfunction Procedures of the following temporary revisions, as applicable to your helicopter: Eurocopter Flight Manual BK117 A–3 Temporary Revision 9, Eurocopter Flight Manual BK117 A–4 Temporary Revision 5, Eurocopter Flight Manual BK117 B–1 Temporary Revision 6, Eurocopter Flight Manual BK 117 B–2 Temporary Revision 1, or Eurocopter Flight Manual BK 117 C–1 Temporary Revision 2, all dated September 22, 2006. Using a later RFM revision with information identical to that contained in the temporary revision specified for your helicopter is acceptable for compliance with the requirement of this paragraph. (iii) For Model MBB–BK 117 A–1 helicopters, revise Section 3 Emergency and Malfunction Procedures of the existing RFM for your helicopter to include the information in Figures 1 through 3 to paragraph (g)(2)(iii) of this AD. BILLING CODE 4910–13–P E:\FR\FM\12MRR1.SGM 12MRR1 VerDate Sep<11>2014 Federal Register / Vol. 86, No. 47 / Friday, March 12, 2021 / Rules and Regulations 19:32 Mar 11, 2021 Jkt 253001 PO 00000 Frm 00008 Fmt 4700 Sfmt 4725 E:\FR\FM\12MRR1.SGM 12MRR1 ER12MR21.007</GPH> 13978 VerDate Sep<11>2014 19:32 Mar 11, 2021 Jkt 253001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4725 E:\FR\FM\12MRR1.SGM 12MRR1 13979 ER12MR21.008</GPH> Federal Register / Vol. 86, No. 47 / Friday, March 12, 2021 / Rules and Regulations VerDate Sep<11>2014 Federal Register / Vol. 86, No. 47 / Friday, March 12, 2021 / Rules and Regulations 19:32 Mar 11, 2021 Jkt 253001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4725 E:\FR\FM\12MRR1.SGM 12MRR1 ER12MR21.009</GPH> 13980 Federal Register / Vol. 86, No. 47 / Friday, March 12, 2021 / Rules and Regulations 13981 VerDate Sep<11>2014 19:32 Mar 11, 2021 Jkt 253001 PO 00000 Frm 00011 Fmt 4700 Sfmt 4700 E:\FR\FM\12MRR1.SGM 12MRR1 ER12MR21.010</GPH> BILLING CODE 4910–13–C 13982 Federal Register / Vol. 86, No. 47 / Friday, March 12, 2021 / Rules and Regulations (h) Alternative Methods of Compliance (AMOCs) (1) The Manager, Strategic Policy Rotorcraft Section, 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 certification office, send it to the attention of the person identified in paragraph (i)(1) of this AD. Information may be emailed to: 9-DenverAircraft-Cert@faa.gov or ronnea.l.derby.@ 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 Ronnea L. Derby, Aerospace Engineer, Denver ACO Branch, FAA, 26805 East 68th Ave., Room 214, Denver, CO 80249; telephone 303–342–1093; email ronnea.l.derby.@faa.gov. (2) The subject of this AD is addressed in European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA) AD 2015–0098, dated June 2, 2015, and EASA AD 2015–0220, dated November 9, 2015. You may view the EASA ADs on the internet at https://www.regulations.gov in Docket No. FAA–2015–4497. (3) The following documents, which are not incorporated by reference, contain additional information about the subject of this AD: Eurocopter Alert Service Bulletin ASB–BO 105–80–118, Revision 1, dated November 29, 1995; Eurocopter Information Notice 2370–I–24, Revision 0, dated November 15, 2011; Eurocopter Service Bulletin SB–BO105–80–119, dated November 7, 1994; and Eurocopter Service Bulletin SB BO105–90–104, Revision 1, dated June 21, 2010. (4) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (j)(3) and (4) of this AD. (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 this AD specifies otherwise. (i) Eurocopter Alert Service Bulletin ASB– MBB–BK117–90–118, Revision 2, dated May 4, 2009. (ii) Eurocopter Alert Service Bulletin ASB BO105–90–103, Revision 4, dated June 21, 2010. (iii) Eurocopter Flight Manual BK117 A–3 Temporary Revision 9, dated September 22, 2006. (iv) Eurocopter Flight Manual BK117 A–4 Temporary Revision 5, dated September 22, 2006. 19:32 Mar 11, 2021 Jkt 253001 Issued on February 19, 2021. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2021–05146 Filed 3–11–21; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2020–1131; Project Identifier MCAI–2020–00613–R; Amendment 39–21445; AD 2021–05–02] RIN 2120–AA64 Airworthiness Directives; Airbus Helicopters Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: (j) Material Incorporated by Reference VerDate Sep<11>2014 (v) Eurocopter Flight Manual BK117 B–1 Temporary Revision 6, dated September 22, 2006. (vi) Eurocopter Flight Manual BK 117 B– 2 Temporary Revision 1, dated September 22, 2006. (vii) Eurocopter Flight Manual BK 117 C– 1 Temporary Revision 2, dated September 22, 2006. (3) For Eurocopter service information identified in this AD, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052; telephone 972–641–0000 or 800–232–0323; fax 972–641–3775; or at https://www.airbus.com/helicopters/services/ technical-support.html. (4) You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. 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 fedreg.legal@nara.gov, or go to: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, and AS350D helicopters; Model AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters; and Model EC130B4 and EC130T2 helicopters. This AD was prompted by a report of failed main rotor hub-to-mast attachment screws. This AD requires determining whether the helicopter has been operated in a severe environment since the last inspection of the main rotor hub-to-mast attachment screws, an SUMMARY: PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 inspection of the main rotor hub-to-mast attachment screws if the helicopter has been operated in a severe environment, and replacement of the main rotor hubto-mast attachment screws if necessary, as specified in a European Aviation Safety Agency (now European Union Aviation Safety Agency) (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 16, 2021. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 16, 2021. ADDRESSES: For material incorporated by reference (IBR) in this AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: ADs@ easa.europa.eu; internet: www.easa.europa.eu. You may find this material on the EASA website at https:// ad.easa.europa.eu. You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call 817–222–5110. It is also available in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2020–1131. Examining the AD Docket You may examine the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2020– 1131; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, any comments received, and other information. The address for Docket Operations is 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: Hal Jensen, Aerospace Engineer, Operational Safety Branch, FAA, 470 L’Enfant Plaza SW, Washington, DC 20024; phone: 202–267–9167; email: hal.jensen@ faa.gov. SUPPLEMENTARY INFORMATION: Discussion The EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2017–0032, dated February 17, 2017; corrected February 20, 2017 (EASA AD 2017–0032) (also referred to as the E:\FR\FM\12MRR1.SGM 12MRR1

Agencies

[Federal Register Volume 86, Number 47 (Friday, March 12, 2021)]
[Rules and Regulations]
[Pages 13975-13982]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-05146]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-4497; Project Identifier 2016-SW-011-AD; Amendment 
39-21450; AD 2021-05-07]
RIN 2120-AA64


Airworthiness Directives; Airbus Helicopters Deutschland GmbH 
(Type Certificate Previously Held by Eurocopter Deutschland GmbH) 
Helicopters

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

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model BO-105A, 
BO-105C, BO-105S, MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-
BK 117 B-1, MBB-BK 117 B-2, and MBB-BK 117 C-1 helicopters. This AD was 
prompted by a report of a loss of electrical ground between the 
starter-generator and the generator voltage regulator (regulator). This 
AD requires inspecting the starter-generator electrical ground 
connection, retrofitting the starter-generator wire harness, and 
depending on model, revising the existing Rotorcraft Flight Manual 
(RFM) for your helicopter. The FAA is issuing this AD to address the 
unsafe condition on these products.

DATES: This AD is effective April 16, 2021.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of April 16, 
2021.

ADDRESSES: For Eurocopter service information identified in this final 
rule, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 
75052; telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or at 
https://www.airbus.com/helicopters/services/technical-support.html. You 
may view this service information at the FAA, Office of the Regional 
Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort 
Worth, TX 76177. For information on the availability of this material 
at the FAA, call 817-222-5110.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2015-
4497; or in person at Docket Operations between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays. The AD docket contains 
this final rule, any comments received, and other information. The 
street address for Docket Operations is 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: Ronnea L. Derby, Aerospace Engineer, 
Denver ACO Branch, FAA, 26805 East 68th Ave., Room 214, Denver, CO 
80249; telephone 303-342-1093; email [email protected]

SUPPLEMENTARY INFORMATION: 

Discussion

    The European Aviation Safety Agency (now European Union Aviation 
Safety Agency) (EASA), which is the Technical Agent for the Member 
States of the European Union, has issued EASA AD 2015-0098, dated June 
2, 2015 (EASA AD 2015-0098), and EASA AD 2015-0220, dated November 9, 
2015 (EASA AD 2015-0220) (also referred to as the Mandatory Continuing 
Airworthiness Information, or the MCAI), to correct an unsafe condition 
for all Airbus Helicopters Model MBB-BK117 A-1, MBB-BK117 A-3, MBB-
BK117 A-4, MBB-BK117 B-1, MBB-BK117 B-2, and MBB-BK117 C-1 helicopters; 
and Airbus Helicopters Model BO105 A, BO105 C, BO105 D and BO105 S 
helicopters with certain part-numbered voltage regulators.
    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 by adding an AD that would apply to certain Airbus 
Helicopters Model BO-105A, BO-105C, and BO-105S helicopters; and all 
Airbus Helicopters Model MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-
4, MBB-BK 117 B-1, MBB-BK 117 B-2, and MBB-BK 117 C-1 helicopters. The 
NPRM published in the Federal Register on July 16, 2020 (85 FR 43153). 
The NPRM was prompted by a report of a loss of electrical ground 
between the starter-generator and the regulator. The NPRM proposed to 
require inspecting the starter-generator electrical ground connection, 
retrofitting the starter-generator wire harness, and depending on 
model, revising the existing RFM for your helicopter.
    The FAA is issuing this AD to address the loss of electrical ground 
between the starter-generator and the regulator. This condition could 
result in an overvoltage of electrical power, damage to electronic 
equipment, and subsequent loss of control of the helicopter.

Comments

    The FAA gave the public the opportunity to participate in 
developing this final rule. The FAA received no comments on the NPRM or 
on the determination of the cost to the public.

Conclusion

    The FAA reviewed the relevant data and determined that air safety 
and the public interest require adopting this final rule as proposed, 
except for minor editorial changes. The FAA has determined that these 
minor changes:
     Are consistent with the intent that was proposed in the 
NPRM for addressing the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    Eurocopter (now Airbus Helicopters) issued Alert Service Bulletin 
ASB-MBB-BK117-90-118, Revision 2, dated May 4, 2009, for certain Model 
MBB-BK117 helicopters and Alert Service Bulletin ASB BO105-90-103, 
Revision 4, dated June 21, 2010, for certain Model BO105 helicopters. 
This service information specifies a visual inspection for damage, 
corrosion, and cracks and measuring the resistance of the left-hand and 
right-hand electrical ground connections between each starter-generator 
and the regulator. If there is damage or suspected damage, or if the 
resistance is out of tolerance, this service information specifies 
replacing the wire terminal. This service information also specifies 
performing the visual inspection and resistance measurement each time 
the starter generator is removed or the wiring is disconnected until a 
retrofit ground connection is installed. These documents are distinct 
since they apply to different models.
    Eurocopter also issued Eurocopter Flight Manual BK117 A-3 Temporary 
Revision 9, Eurocopter Flight Manual BK117 A-4 Temporary Revision 5, 
Eurocopter Flight Manual BK117 B-1 Temporary Revision 6, Eurocopter 
Flight Manual BK 117 B-2 Temporary Revision 1, and Eurocopter Flight 
Manual BK 117 C-1 Temporary Revision 2, all dated September 22, 2006, 
to provide updated procedures in the event of a generator failure. 
These

[[Page 13976]]

documents are distinct since they apply to different models.
    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.

Other Related Service Information

    Eurocopter (now Airbus Helicopters) issued Service Bulletin SB 
BO105-90-104, Revision 1, dated June 21, 2010, for certain Model BO105 
helicopters. This service information specifies procedures for 
installing a retrofit ground connection of the starter-generator.
    Eurocopter issued Alert Service Bulletin ASB-BO 105-80-118, 
Revision 1, dated November 29, 1995, and Service Bulletin SB-BO105-80-
119, dated November 7, 1994, both for certain Model BO105 helicopters. 
This service information specifies retrofitting certain helicopters 
with voltage regulators that incorporate overvoltage protection by 
modifying the main relay box, modifying the overhead panel, and 
performing a functional test.
    Eurocopter issued Information Notice 2370-I-24, Revision 0, dated 
November 15, 2011, for certain Model BO105 helicopters to provide 
notice that a modified starter-generator may only be installed on 
helicopters that have also been modified. This service information 
states that combining modified with non-modified can cause overvoltage 
in the electrical system during the first ground run following engine 
replacement and subsequent damage to electronic equipment. This service 
information also recommends retrofitting all helicopters approved to 
only fly under visual flight rules.

Differences Between This AD and the EASA ADs

    The EASA ADs require visually inspecting the wire terminals for 
damage, corrosion, and cracks. This AD requires visually inspecting for 
a crack, a kink, fraying, looseness, missing material, and corrosion.
    The EASA ADs require repeating the visual inspection and resistance 
measurement each time a starter-generator is removed or the wiring is 
disconnected from a starter-generator. This AD does not because such a 
compliance time would be difficult to enforce.
    EASA AD 2015-0220 requires additional actions for Model BO-105 
helicopters with a serial number up to 0160 than for helicopters with a 
serial number 0161 and larger. This AD requires the same actions for 
all Model BO-105 helicopters regardless of serial number.
    EASA AD 2015-0220 allows credit for complying with Eurocopter Alert 
Service Bulletin ASB BO105-90-103, Revision 2 or Revision 3, whereas 
this AD does not.

Costs of Compliance

    The FAA estimates that this AD affects 40 Model BO-105 helicopters 
and 44 Model MBB-BK 117 helicopters of U.S. Registry. The FAA estimates 
that operators may incur the following costs in order to comply with 
this AD using an estimated labor cost of $85 per work-hour.
    Performing a visual inspection and resistance measurement of the 
electrical ground connection takes about 2 work-hours for an estimated 
cost of $170 per helicopter and $14,280 for the U.S. fleet per 
inspection and measurement.
    Performing the retrofit of the wiring harness takes about 10 work-
hours. Required parts for a Model BO-105 helicopter cost $2,509 for an 
estimated replacement cost of $3,359 per helicopter and $134,360 for 
the U.S. fleet. Required parts for a Model MBB-BK 117 helicopter cost 
$1,730 for an estimated replacement cost of $2,580 per helicopter and 
$113,520 for the U.S. fleet. Revising the existing RFM for Model MBB-BK 
117 helicopters takes about 0.5 work-hour, for an estimated cost of $43 
per helicopter and $1,892 for the U.S. fleet.

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 that 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.

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 airworthiness 
directive:

2021-05-07 Airbus Helicopters Deutschland GmbH (Type Certificate 
Previously Held by Eurocopter Deutschland GmbH): Amendment 39-21450; 
Docket No. FAA-2015-4497; Project Identifier 2016-SW-011-AD.

(a) Effective Date

    This airworthiness directive (AD) is effective April 16, 2021.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the following Airbus Helicopters Deutschland 
GmbH (Type Certificate previously held by Eurocopter Deutschland 
GmbH) helicopters, certificated in any category:
    (1) Model BO-105A, BO-105C, and BO-105S helicopters with a 
voltage regulator part number (P/N) 51565-000, 51565-000R, or 51509-
002R installed; and
    (2) Model MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 
117 B-1, MBB-BK 117 B-2, and MBB-BK 117 C-1 helicopters.

(d) Subject

    Joint Aircraft Service Component (JASC) Code: 2497, Electrical 
Power System Wiring.

(e) Unsafe Condition

    This AD was prompted by a report of a loss of electrical ground 
between the starter-

[[Page 13977]]

generator and the generator voltage regulator (regulator). The FAA 
is issuing this AD to address loss of electrical ground between the 
starter-generator and the regulator. This condition could result in 
an overvoltage of electrical power, damage to electronic equipment, 
and subsequent loss of control of the helicopter.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Required Actions

    (1) Within 50 hours time-in-service (TIS):
    (i) Visually inspect the wire terminal of wire P55F16N/P56F16N 
for Model BO-105A, BO-105C, and BO-105S helicopters and wire 
1PA53B20/2PA53B20 for Model MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 
117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2, and MBB-BK 117 C-1 
helicopters on Terminal E of each starter-generator for a crack, a 
kink, fraying, looseness, missing material, and corrosion. If there 
is a crack, a kink, fraying, looseness, missing material, or any 
corrosion, before further flight, replace the wire terminal.
    (ii) Measure the resistance between each starter-generator and 
its regulator in accordance with the Accomplishment Instructions, 
paragraph 2.A.2.3. of Eurocopter Alert Service Bulletin ASB BO105-
90-103, Revision 4, dated June 21, 2010, or paragraphs 2.A.2.3. and 
2.A.2.5. of Eurocopter Alert Service Bulletin ASB-MBB-BK117-90-118, 
Revision 2, dated May 4, 2009, as applicable to your model 
helicopter. If the resistance is more than 500 milliohms, before 
further flight, replace the wire terminal.
    (2) Within 150 hours TIS:
    (i) Install a wire harness from each generator voltage regulator 
as follows.
    (A) For Model BO-105A, BO-105C, and BO-105S helicopters: Wire 
harness P/N 105-90081.
    (B) For Model MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-4, 
MBB-BK 117 B-1, and MBB-BK 117 B-2 helicopters: Wire harness P/N 
117-901941.
    (C) For Model MBB-BK 117 C-1 helicopters: Wire harness P/N 117-
901961.
    (ii) For Model MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 B-1, 
MBB-BK 117 B-2, and MBB-BK 117 C-1 helicopters, revise the existing 
Rotorcraft Flight Manual (RFM) for your helicopter to include the 
information in Section 3 Emergency and Malfunction Procedures of the 
following temporary revisions, as applicable to your helicopter: 
Eurocopter Flight Manual BK117 A-3 Temporary Revision 9, Eurocopter 
Flight Manual BK117 A-4 Temporary Revision 5, Eurocopter Flight 
Manual BK117 B-1 Temporary Revision 6, Eurocopter Flight Manual BK 
117 B-2 Temporary Revision 1, or Eurocopter Flight Manual BK 117 C-1 
Temporary Revision 2, all dated September 22, 2006. Using a later 
RFM revision with information identical to that contained in the 
temporary revision specified for your helicopter is acceptable for 
compliance with the requirement of this paragraph.
    (iii) For Model MBB-BK 117 A-1 helicopters, revise Section 3 
Emergency and Malfunction Procedures of the existing RFM for your 
helicopter to include the information in Figures 1 through 3 to 
paragraph (g)(2)(iii) of this AD.
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(h) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Strategic Policy Rotorcraft Section, 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 certification office, send it to the 
attention of the person identified in paragraph (i)(1) of this AD. 
Information may be emailed to: [email protected] or 
[email protected]
    (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 Ronnea L. Derby, 
Aerospace Engineer, Denver ACO Branch, FAA, 26805 East 68th Ave., 
Room 214, Denver, CO 80249; telephone 303-342-1093; email 
[email protected]
    (2) The subject of this AD is addressed in European Aviation 
Safety Agency (now European Union Aviation Safety Agency) (EASA) AD 
2015-0098, dated June 2, 2015, and EASA AD 2015-0220, dated November 
9, 2015. You may view the EASA ADs on the internet at https://www.regulations.gov in Docket No. FAA-2015-4497.
    (3) The following documents, which are not incorporated by 
reference, contain additional information about the subject of this 
AD: Eurocopter Alert Service Bulletin ASB-BO 105-80-118, Revision 1, 
dated November 29, 1995; Eurocopter Information Notice 2370-I-24, 
Revision 0, dated November 15, 2011; Eurocopter Service Bulletin SB-
BO105-80-119, dated November 7, 1994; and Eurocopter Service 
Bulletin SB BO105-90-104, Revision 1, dated June 21, 2010.
    (4) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (j)(3) and (4) of this AD.

(j) 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 this AD specifies otherwise.
    (i) Eurocopter Alert Service Bulletin ASB-MBB-BK117-90-118, 
Revision 2, dated May 4, 2009.
    (ii) Eurocopter Alert Service Bulletin ASB BO105-90-103, 
Revision 4, dated June 21, 2010.
    (iii) Eurocopter Flight Manual BK117 A-3 Temporary Revision 9, 
dated September 22, 2006.
    (iv) Eurocopter Flight Manual BK117 A-4 Temporary Revision 5, 
dated September 22, 2006.
    (v) Eurocopter Flight Manual BK117 B-1 Temporary Revision 6, 
dated September 22, 2006.
    (vi) Eurocopter Flight Manual BK 117 B-2 Temporary Revision 1, 
dated September 22, 2006.
    (vii) Eurocopter Flight Manual BK 117 C-1 Temporary Revision 2, 
dated September 22, 2006.
    (3) For Eurocopter service information identified in this AD, 
contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 
75052; telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or 
at https://www.airbus.com/helicopters/services/technical-support.html.
    (4) You may view this service information at the FAA, Office of 
the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 
6N-321, Fort Worth, TX 76177. 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 [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on February 19, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2021-05146 Filed 3-11-21; 8:45 am]
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