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2020-23-09: Doors

FAA order 2020-23-09 is an airworthiness directive in force since December 24, 2020. The FAA's subject line: Doors. It names Airbus Helicopters EC 130 now H130: about 311 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: rotorcraft systems.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus Helicopters
Models
EC130B4
On this site
Airbus Helicopters EC 130 now H130 311 registered

Dates and paperwork

In force since
December 24, 2020
Published
November 19, 2020 (signed November 4, 2020)
Docket
FAA-2020-0685
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 all Airbus Helicopters Model EC130B4 helicopters. This AD was prompted by reports of inflight detachment of the left-hand (LH) side cabin sliding doors and cases of impact damage on the main rotor blades, which were caused by degradation of the sliding door locking mechanism. This AD requires repetitive checks (measurements) of the load that operates the sliding door opening mechanism, repetitive inspections of the markings of the attachment screws for proper alignment, modifying the attachment system of the sliding door, and corrective actions if necessary, as specified in a 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.

The order itself the regulatory text, as published

Show the full text (4,687 characters)
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\n2020-23-09 Airbus Helicopters: Amendment 39-21325; Docket No. FAA- 2020-0685; Project Identifier MCAI-2020-00396-R. \n\n(a) Effective Date \n\n\n\tThis airworthiness directive (AD) is effective December 24, 2020. \n\n(b) Affected ADs \n\n\n\tNone. \n\n(c) Applicability \n\n\n\tThis AD applies to all Airbus Helicopters Model EC130B4 helicopters, certificated in any category. \n\n(d) Subject \n\n\n\tAir Transport Association (ATA) of America Code 52, Doors. \n\n(e) Reason \n\n\n\tThis AD was prompted by reports of inflight detachment of the left-hand (LH) side cabin sliding doors and cases of impact damage on the main rotor blades, which were caused by degradation of the sliding door locking mechanism. The FAA is issuing this AD to address degradation of the locking mechanism, which could lead to further events of inflight detachment of a LH side cabin sliding door, and possibly result in damage to the helicopter and injury to persons on the ground. \n\n(f) Compliance \n\n\n\tComply with this AD within the compliance times specified, unless already done. \n\n(g) Requirements \n\n\n\tExcept as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2020-0069, dated March 24, 2020 (EASA AD 2020-0069). \n\n(h) Exceptions to EASA AD 2020-0069 \n\n\n\t(1) Where EASA AD 2020-0069 refers to its effective date, this AD requires using the effective date of this AD. \n\t(2) Where EASA AD 2020-0069 refers to January 24, 2019 (the effective date of EASA AD 2020-0069), this AD requires using the effective date of this AD. \n\t(3) The ''Remarks'' section of EASA AD 2020-0069 does not apply to this AD. \n\t(4) The ''Parts Installation'' allowance provided in paragraph (8) of EASA AD 2020-0069 does not apply to this AD. \n\t(5) Although the service information referenced in EASA AD 2020- 0069 specifies to discard certain parts, this AD does not include that requirement. \n\n(i) Alternative Methods of Compliance (AMOCs) \n\n\n\tThe Manager, Rotorcraft Standards Branch, FAA, may approve AMOCs for this AD. Send your proposal to: Manager, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5110; email [email protected]. \n\n(j) Related Information \n\n\n\tFor more information about this AD, contact Kristin Bradley, Aviation Safety Engineer, International Validation Branch, General Aviation & Rotorcraft Unit, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5485;email [email protected]. \n\n((Page 73617)) \n\n(k) 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) European Union Aviation Safety Agency (EASA) AD 2020-0069, dated March 24, 2020. \n\t(ii) (Reserved) \n\t(3) For EASA AD 2020-0069, contact the EASA, Konrad-Adenauer- Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email [email protected]; internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https://ad.easa.europa.eu. \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. This material may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA- 2020-0685. \n\t(5) You may view this material 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. \n\n\n\tIssued on November 4, 2020. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. (FR Doc. 2020-25469 Filed 11-18-20; 8:45 am) BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2019-07-15SW-17-23R2 · Fuel System
2018-03-02SW-17-23R1 · Fuel System
2015-08-13SW-15-20 · Air Conditioning System Wiring
2012-10-03SW-12-45 · Garmin Model 400W/500W Series GPS-WAAS Navigation System
2012-02-03SW-12-17 · Autopilot System

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 November 6, 2026. Connections as data: /graph/directive/2020-23-09.json · aircraft systems.