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2022-06-08: Flight Control System

FAA order 2022-06-08 is an airworthiness directive in force since May 9, 2022. The FAA's subject line: Flight Control System. It names Diamond Aircraft DA 42 Twin Star: about 264 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Diamond Aircraft Industries GmbH
Models
DA 42, DA 42 M-NG, DA 42 NG
On this site
Diamond Aircraft DA 42 Twin Star 264 registered

Dates and paperwork

In force since
May 9, 2022
Published
April 4, 2022 (signed March 10, 2022)
Docket
FAA-2021-1077
Replaces
2017-18-10
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is superseding Airworthiness Directive (AD) 2017-18- 10, which applied to certain Diamond Aircraft Industries GmbH (DAI) Model DA 42, DA 42 M-NG, and DA 42 NG airplanes. AD 2017-18-10 required modifying the flap control system, repetitively inspecting the flap bell crank, and replacing the flap bell crank as necessary. Since the FAA issued AD 2017-18-10, the European Union Aviation Safety Agency (EASA) superseded its mandatory continuing airworthiness information (MCAI) to correct an unsafe condition on these products. This AD retains the actions required by AD 2017-18-10, expands the applicability, and prohibits the installation of certain flap bell cranks. 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 (7,010 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: a. Removing Airworthiness Directive 2017-18-10, Amendment 39-19019 (82 FR 42029, September 6, 2017); and b. Adding the following new airworthiness directive: 2022-06-08 Diamond Aircraft Industries GmbH: Amendment 39-21974; Docket No. FAA-2021-1077; Project Identifier MCAI-2021-00607-A. (a) Effective Date This airworthiness directive (AD) is effective May 9, 2022. (b) Affected ADs This AD replaces AD 2017-18-10, Amendment 39-19019 (82 FR 42029, September 6, 2017). (c) Applicability This AD applies to Diamond Aircraft Industries GmbH Model DA 42, DA 42 M-NG, and DA 42 NG airplanes, all serial numbers, certificated in any category, with a flap bell crank part number (P/N) D60-2757-11-00, up to and including revision "f" installed. (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 cracks and deformation on certain flap bell cranks. The FAA is issuing this AD to prevent failure of the flap bell crank. The unsafe condition, if not addressed, could result in reduced control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Actions (1) Comply with paragraph (g)(2) or (3) of this AD at whichever compliance time in paragraph (g)(1)(i) or (ii) of this AD occurs later. (i) Before the flap bell crank accumulates 600 hours time-in-service (TIS); or (ii) Within 100 hours TIS after the effective date of this AD or within 6 months after the effective date of this AD, whichever occurs first. (2) For airplanes with a flap bell crank revision "e" or "f": Inspect the flap bell crank P/N D60-2757-11-00 for cracks and deformation and modify the flap control system by installing two spacers, P/N DS BU2-10-06-0065-C, by following section III Instructions in Diamond Aircraft Industries GmbH Work Instruction WI-MSB 42-126 and WI-MSB 42NG-066, Revision 1, dated November 14, 2019 (issued as one document) attached to Diamond Aircraft Mandatory Service Bulletin MSB 42-126/1 and MSB 42NG-066/1, dated November 14, 2019 (issued as one document). (i) If there is a crack or any deformation, you must replace the flap bell crank with P/N D60-2757-11-00_01, as required by step 6 of the Instructions, before further flight. (ii) If there are no cracks and no deformation, repeat the inspection (not the modification) at intervals not to exceed 200 hours TIS until the flap bell crank is replaced with flap bell crank P/N D60-2757-11-00_01. (3) For airplanes with a flap bell crank up to revision "d": Replace the flap bell crank with P/N D60-2757-11-00_01 in accordance with section III Instructions in Diamond Aircraft Industries GmbH Work Instruction WI-MSB 42-126 and WI-MSB 42NG-066, Revision 1, dated November 14, 2019 (issued as one document) attached to Diamond Aircraft Mandatory Service Bulletin MSB 42-126/1 and MSB 42NG-066/1, dated November 14, 2019 (issued as one document). (h) Prohibited Installation As of the effective date of this AD, do not install on any airplane a flap bell crank P/N D60-2757-11-00 with a revision up to and including revision "d." (i) Credit for Previous Actions This paragraph provides credit for the actions required by paragraphs (g)(2) and (3) of this AD, if done before the effective date of this AD using Diamond Aircraft Industries GmbH Work Instruction WI-MSB 42-126 and WI-MSB 42NG-066, dated March 27, 2017 (issued as one document) attached to Diamond Aircraft Mandatory Service Bulletin MSB 42-126 and MSB 42NG-066, dated March 27, 2017 (issued as one document). (j) 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 certification office, send it to the attention of the person identified in paragraph (k)(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. (k) Related Information (1) For more information about this AD, contact Penelope Trease, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 26805 E 68th Avenue, Denver, CO 80249; phone: (303) 342-1094; email: penelope.trease@faa.gov. (2) Refer to European Union Aviation Safety Agency (EASA) AD 2020-0008, dated January 20, 2020, for more information. You may examine the EASA AD at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-1077. (3) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (l)(3) and (4) of this AD. (l) 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 Mandatory Service Bulletin MSB 42-126/1 and MSB 42NG-066/1, dated November 14, 2019 (issued as one document) published with Diamond Aircraft Industries GmbH Work Instruction WI-MSB 42-126 and WI-MSB 42NG-066, Revision 1, dated November 14, 2019 (issued as one document) attached. (ii) [Reserved] (3) For service information identified in this AD, contact Diamond Aircraft Industries GmbH, N.A. Otto-Straße 5, A-2700 Wiener Neustadt, Austria; phone: +43 2622 26700; email: office@diamond-air.at; website: https://www.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 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. Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022-06961 Filed 4-1-22; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2009-02-11CE-09-12 · Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 Installations
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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/2022-06-08.json · aircraft systems.