AD 2021-05-07

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.

Final rule.

Adoption of the Amendment \n\n\n\tAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n0 1. The authority citation for part 39 continues to read as follows: \n\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\n\n\nSec. 39.13 (Amended) \n\n0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive: \n\n2021-05-07 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. \n\n(a) Effective Date \n\n\n\tThis airworthiness directive (AD) is effective April 16, 2021. \n\n(b) Affected ADs \n\n\n\tNone. \n\n(c) Applicability \n\n\n\tThis AD applies to the following Airbus Helicopters Deutschland GmbH (Type Certificate previously held by Eurocopter Deutschland GmbH) helicopters, certificated in any category: \n\t(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 \n\t(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. \n\n(d) Subject \n\n\n\tJoint Aircraft Service Component (JASC) Code: 2497, Electrical Power System Wiring. \n\n(e) Unsafe Condition \n\n\n\tThis AD was prompted by a report of a loss of electrical ground between the starter- \n\n((Page 13977)) \n\ngenerator 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. \n\n(f) Compliance \n\n\n\tComply with this AD within the compliance times specified, unless already done. \n\n(g) Required Actions \n\n\n\t(1) Within 50 hours time-in-service (TIS): \n\t(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. \n\t(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. \n\t(2) Within 150 hours TIS: \n\t(i) Install a wire harness from each generator voltage regulator as follows. \n\t(A) For Model BO-105A, BO-105C, and BO-105S helicopters: Wire harness P/N 105-90081. \n\t(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. \n\t(C) For Model MBB-BK 117 C-1 helicopters: Wire harness P/N 117- 901961. \n\t(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. \n\t(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 \n\n((Page 13978)) \n\n(GRAPHIC) (TIFF OMITTED) TR12MR21.007 \n\n\n\n((Page 13979)) \n\n\n\n(GRAPHIC) (TIFF OMITTED) TR12MR21.008 \n\n\n\n((Page 13980)) \n\n\n\n(GRAPHIC) (TIFF OMITTED) TR12MR21.009 \n\n\n\n((Page 13981)) \n\n\n\n(GRAPHIC) (TIFF OMITTED) TR12MR21.010 \n\nBILLING CODE 4910-13-C \n\n((Page 13982)) \n\n(h) Alternative Methods of Compliance (AMOCs) \n\n\n\t(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-Denver-Aircraft-Cert@faa.gov or ronnea.l.derby.@faa.gov. \n\t(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. \n\n(i) Related Information \n\n\n\t(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. \n\t(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. \n\t(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. \n\t(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. \n\n(j) Material Incorporated by Reference \n\n\n\t(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. \n\t(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. \n\t(i) Eurocopter Alert Service Bulletin ASB-MBB-BK117-90-118, Revision 2, dated May 4, 2009. \n\t(ii) Eurocopter Alert Service Bulletin ASB BO105-90-103, Revision 4, dated June 21, 2010. \n\t(iii) Eurocopter Flight Manual BK117 A-3 Temporary Revision 9, dated September 22, 2006. \n\t(iv) Eurocopter Flight Manual BK117 A-4 Temporary Revision 5, dated September 22, 2006. \n\t(v) Eurocopter Flight Manual BK117 B-1 Temporary Revision 6, dated September 22, 2006. \n\t(vi) Eurocopter Flight Manual BK 117 B-2 Temporary Revision 1, dated September 22, 2006. \n\t(vii) Eurocopter Flight Manual BK 117 C-1 Temporary Revision 2, dated September 22, 2006. \n\t(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. \n\t(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. \n\t(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/ibr-locations.html. \n\n\n\tIssued 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

Discussion \n\n\n\tThe 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. \n\tThe 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 117A- 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. \n\tThe 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. \n\nComments \n\n\n\tThe 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. \n\nConclusion \n\n\n\tThe 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: \n\tAre consistent with the intent that was proposed in the NPRM for addressing the unsafe condition; and \n\tDo not add any additional burden upon the public than was already proposed in the NPRM. \n\nRelated Service Information Under 1 CFR Part 51 \n\n\n\tEurocopter (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 resistanceis 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. \n\tEurocopter 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 \n\n((Page 13976)) \n\ndocuments are distinct since they apply to different models. \n\tThis service information is reasonably available because the interested parties have access to it through their normalcourse of business or by the means identified in the ADDRESSES section. \n\nOther Related Service Information \n\n\n\tEurocopter (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. \n\tEurocopter 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. \n\tEurocopter 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 onlybe 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. \n\nDifferences Between This AD and the EASA ADs \n\n\n\tThe 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. \n\tThe 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. \n\tEASA AD 2015-0220 requires additional actions for Model BO-105 helicopterswith 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. \n\tEASA 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. \n\nCosts of Compliance \n\n\n\tThe 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. \n\tPerforming 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. \n\tPerforming 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. \n\nAuthority for This Rulemaking \n\n\n\tTitle 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. \n\tThe 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 regulationsfor 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. \n\nRegulatory Findings \n\n\n\tThis 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. \n\tFor the reasons discussed above, I certify that this AD: \n\t(1) Is not a ''significant regulatory action'' under Executive Order 12866, \n\t(2) Will not affect intrastate aviation in Alaska, and \n\t(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. \n\nList of Subjects in 14 CFR Part 39 \n\n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.