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2020-04-14 |
HONDA AIRCRAFT COMPANY LLC: Amendment 39-21031; Docket No. FAA-2020-0195; Product Identifier 2019-CE-052-AD. |
(a) EFFECTIVE DATE This AD is effective April 6, 2020. (b) AFFECTED ADS None. (c) APPLICABILITY This AD applies to Honda Aircraft Company LLC Model HA-420 airplanes, serial numbers (S/Ns) 42000011 through 42000184, certificated in any category. (d) SUBJECT Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 32, Landing Gear. (e) UNSAFE CONDITION This AD was prompted by reports of damage to the wheel speed trans- ducer wiring harness due to excessive slack in the wiring harness assembly that allows contact with the main landing gear tire and the determination that the airplane flight manuals (AFMs) and quick reference handbooks (QRHs) contain incorrect procedures for antiskid braking system failures. The FAA is issuing this AD to prevent un -annunciated loss of normal brakes and reduced directional control during landing deceleration and ground operations, which could lead to a runway excursion. (f) COMPLIANCE Comply with this AD within the compliance time specified, unless al- ready done. (g) REVISE THE AIRPLANE FLIGHT MANUALS AND QUICK REFERENCE HANDBOOKS Before further flight after April 6, 2020 (the effective date of this AD), revise your AFM and your QRH as specified below. (1) For airplanes with S/Ns 42000012 through 42000125 without SB-420-55- 001: Remove the Abnormal Procedure pages for ANTI-SKID Fail and re- place with Pages 3A178 through 3A-180 from Section 3A—Abnormal Pro- cedures in Honda Aircraft Company Airplane Flight Manual, Model HA-420 Part No.: HJ1-29000-003-001, Revision D, dated December 12, 2019. (2) For airplanes with S/Ns 42000012 through 42000125 without SB-420-55- 001: Remove the Abnormal Procedure pages for ANTI-SKID FAIL and re- place with Page A126 and Page A-127 from Model HA-420, HJ1-29000-007- 001, Volume 1 of 2, Quick Reference Handbook, Normal Procedures, Revision D, dated December 12, 2019. (3) For airplanes with S/Ns 42000011, 42000012 through 42000125 with SB- 420-55-001, and 42000126 through 42000184: Remove the Abnormal Pro- cedure pages for ANTI-SKID FAIL and replace with Pages 3A-178 through 3A-180 from Section 3A—Abnormal Procedures in Honda Aircraft Company Airplane Flight Manual, Model HA-420, Part No.: HJ1-29001-003-001, Revision B1, dated December 12, 2019. (4) For airplanes with S/Ns 42000011, 42000012 through 42000125 with SB- 420-55-001, and 42000126 through 42000184: Remove the Abnormal Pro- cedure pages for ANTI-SKID FAIL and replace with Page A-124 and Page A-125 from Model HA-420, HJ1-29001-007-001, Quick Reference Handbook, Revision B, dated December 12, 2019. (h) CORRECTIVE ACTIONS FOR THE WHEEL SPEED TRANSDUCER WIRING HARNESS Within 90 days after April 6, 2020 (the effective date of this AD), do the actions specified in steps 1 through 7 of the Accomplishment Instructions in Honda Aircraft Company Service Bulletin Alert SB-420- 32-008, Revision B, dated November 16, 2019. (i) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS) (1) The Manager, Atlanta ACO 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 certification office, send it to the attention of the person identified in paragraph (j) of this AD. (2) Before using any approved AMOC, notify your appropriate principal in- spector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (3) For service information that contains steps that are labeled as Required for Compliance (RC), the provisions of paragraphs (i)(3)(i) and (ii) of this AD apply. (i) The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with this AD. An AMOC is required for any deviations to RC steps, including substeps and identified figures. (ii) Steps not labeled as RC may be deviated from using accepted methods in accordance with the operator’s maintenance or inspection program without obtaining approval of an AMOC, provided the RC steps, includ- ing substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition. (j) RELATED INFORMATION For more information about this AD, contact Samuel Kovitch, Aerospace Engineer, Atlanta ACO Branch, FAA, 1701 Columbia Avenue, College Park, Georgia 30337; phone: (404) 474-5570; fax: (404) 474-5605; email: samuel.kovitch@faa.gov. (k) 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) Pages 3A-178 through 3A-180 from Section 3A—Abnormal Procedures in Honda Aircraft Company Airplane Flight Manual, HondaJet, Effectivity: 42000012 through 42000125, Model HA-420, Part No.: HJ1-29000-003-001, Revision D, dated December 12, 2019. (ii) Page A-126 and Page A-127 from HondaJet, Model HA-420, HJ1-29000-007- 001, Volume 1 of 2, Effectivity 42000012 through 42000125, Quick Reference Handbook, Normal Procedures, Revision D, dated December 12, 2019. (iii) Pages 3A-178 through 3A-180 from Section 3A—Abnormal Procedures in Honda Aircraft Company Airplane Flight Manual, HondaJet ELITE, Effectivity: 42000011, 42000126 and after, HondaJet APMG, Effectivity: 42000012 through 42000125 with SB-420-55-001, Model HA- 420, Part No.: HJ1-29001-003-001, Revision B1, dated December 12, 2019. (iv) Page A-124 and Page A-125 from HondaJet, Model HA-420, HJ1-29001-007- 001, HondaJet ELITE, Effectivity: 42000011, 42000126 and after, Honda Jet APMG, Effectivity: 42000012 through 42000125 with SB-420-55-001, Quick Reference Handbook, Revision B, dated December 12, 2019. (v) Honda Aircraft Company Service Bulletin Alert SB-420-32-008, Revision B, dated November 16, 2019. (3) For service information identified in this AD, contact Honda Aircraft Company LLC, 6430 Ballinger Road, Greensboro, North Carolina 27410; telephone (336) 662-0246; Internet: https://www.hondajet.com. (4) You may view this service information at the FAA, Policy and Innova- tion Division, 901 Locust, Kansas City, Missouri 64106. For informa- tion on the availability of this material at the FAA, call (816) 329- 4148. (5) You may view the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For infor- mation 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. Issued in Kansas City, Missouri, on March 16, 2020. Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service. FOR FURTHER INFORMATION CONTACT: Samuel Kovitch, Aerospace Engineer, Atlanta ACO Branch, FAA, 1701 Columbia Avenue, College Park, Georgia 30337 phone: (404) 474-5570; fax: (404) 474-5605; email: samuel.kovitch@faa.gov.
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DEPARTMENT OF TRANSPORTATION
The FAA estimates the following costs
to do any necessary
* Note: Since all operators are required
to install wiring hardware and reroute the WST wiring harness, there is |