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2024-07-03: Horizontal Stabilizer Structure

FAA order 2024-07-03 is an airworthiness directive in force since April 24, 2024. The FAA's subject line: Horizontal Stabilizer Structure. It names Diamond Aircraft DA 62: about 173 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Diamond Aircraft Industries Inc
Models
DA 62
On this site
Diamond Aircraft DA 62 173 registered

Dates and paperwork

In force since
April 24, 2024
Published
April 9, 2024 (signed March 27, 2024)
Docket
FAA-2024-0991
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain Diamond Aircraft Industries Inc. Model DA 62 airplanes. This AD was prompted by a report that certain revisions of the airplane maintenance manual (AMM) specified incorrect torque values for the horizontal stabilizer attachment bolts. This AD requires reviewing the airplane maintenance records to determine the torque values for the horizontal stabilizer attachment bolts and torquing the horizontal stabilizer attachment bolts to the correct torque value if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,816 characters)
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: 2024-07-03 Diamond Aircraft Industries Inc.: Amendment 39-22724; Docket No. FAA-2024-0991; Project Identifier MCAI-2024-00051-A. (a) Effective Date This airworthiness directive (AD) is effective April 24, 2024. (b) Affected ADs None. (c) Applicability This AD applies to Diamond Aircraft Industries Inc. Model DA 62 airplanes, serial numbers 62.C001 through 62.C044 inclusive and 62.008 through 62.203 inclusive, certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code 5510, Horizontal Stabilizer Structure. (e) Unsafe Condition This AD was prompted by a report that certain revisions of the airplane maintenance manual specified incorrect torque values for the horizontal stabilizer attachment bolts. The FAA is issuing this AD to address incorrect torque values for the horizontal stabilizer attachment bolts. The unsafe condition, if not addressed, could result in premature wearing of the horizontal stabilizer attachment bolts, loss of structural integrity of the horizontal stabilizer, subsequent separation of the horizontal stabilizer from the fuselage, and loss of control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 30 days or 30 hours time-in-service after the effective date of this AD, whichever occurs later, review the airplane maintenance records to determine if the horizontal stabilizer attachment bolts were last torqued to 45 newton meter (Nm) and if the torque value is not 45 Nm, or if the value cannot be determined, before further flight, torque the bolts to 45 Nm, in accordance with steps 3 through 6 of the Instructions, Section III, in Diamond Aircraft Industries Work Instruction WI-MSB-62-052, Revision 0, dated September 18, 2023, attached to Diamond Aircraft Industries Mandatory Service Bulletin MSB 62-052, Revision 0, dated September 18, 2023 (issued as one document). (h) Alternative Methods of Compliance (AMOCs) 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)(2) of this AD or email to: 9-AVS-AIR-730-AMOC@faa.gov . If mailing information, also submit information by email. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (i) Additional Information (1) Refer to Transport Canada AD CF-2024-02, dated January 12, 2024, for related information. This Transport Canada AD may be found in the AD docket at regulations.gov under Docket No. FAA-2024-0991. (2) For more information about this AD, contact Isabel Saltzman, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (781) 238-7649; email: isabel.l.saltzman@faa.gov . (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) Diamond Aircraft Industries Work Instruction WI-MSB-62-052, Revision 0, dated September 18, 2023, attached to Diamond Aircraft Industries Mandatory Service Bulletin MSB 62-052, Revision 0, dated September 18, 2023 (issued as one document). (ii) [Reserved] (3) For service information contact Diamond Aircraft Industries Inc., 1560 Crumlin Road, London, N5V 1S2, Canada; phone: (519) 457-4041; email: support-canada@diamondaircraft.com ; website: diamondaircraft.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 material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email fr.inspection@nara.gov . Issued on March 27, 2024. Victor Wicklund, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2024-07441 Filed 4-4-24; 11:15 am]BILLING CODE 4910-13-P

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2024-07-03.json · aircraft systems.