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FAA orders · airworthiness directive · historical

2020-09-15: Cabin Equipment/Furnishings; Ice/Rain Protection System; Fuselage Structure (General)

FAA order 2020-09-15 is an airworthiness directive in force since May 20, 2020. The FAA's subject line: Cabin Equipment/Furnishings; Ice/Rain Protection System; Fuselage Structure (General). It names Airbus Helicopters AS332: about 8 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: cabin, seats and restraints.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus Helicopters
Models
AS332C, AS332C1, AS332L, AS332L1
On this site
Airbus Helicopters AS332 8 registered

Dates and paperwork

In force since
May 20, 2020
Published
May 20, 2020 (signed May 13, 2020)
Docket
FAA-2020-0454
Replaced by
2026-05-11
Status
Historical
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 Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. This AD was prompted by a report of vibrations around the 12Hz frequency due to the specific helicopter configuration. This AD requires removing the removable parts of the dual hoist installation or removing the de-icing system. This AD also allows, for certain helicopters, revising the Rotorcraft Flight Manual (RFM) for your helicopter and installing a placard as an optional method of compliance. 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 (6,341 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 (AD): \n\n2020-09-15 Airbus Helicopters: Amendment 39-19911; Docket No. FAA- 2020-0454; Product Identifier 2019-SW-113-AD. \n\n(a) Effective Date \n\n\n\tThis AD becomes effective May 20, 2020. \n\n(b) Affected ADs \n\n\n\tNone. \n\n(c) Applicability \n\n\n\tThis AD applies to Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters, certificated in any category, equipped with a dual hoist installation and de-icing system, except those that have Airbus Helicopters modification 0722907 installed in production. \n\n(d) Subject \n\n\n\tJoint Aircraft Service Component (JASC) Code 2500, Cabin Equipment/Furnishings; 3000, Ice/Rain Protection System; 5300, Fuselage Structure (General). \n\n(e) Reason \n\n\n\tThis AD was prompted by a report of vibrations around the 12Hz frequency due to the specific helicopter configuration. The FAA is issuing this AD to address this condition, which could generate divergent aeromechanic coupling between the helicopter structure and the rotor, possibly resulting in mechanical failure of structural parts and 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\tWithin 7 days after the effective date of this AD: Remove the removable parts of the dual hoist installation or remove the de- icing system in accordance with the instructions of section 3.B of Airbus Helicopters Emergency Alert Service Bulletin AS332 01.00.91, Revision 1, dated December 4, 2019, or Section 3.B.2 of Airbus HelicoptersEmergency Alert Service Bulletin AS332 01.00.96, Revision 0, dated December 4, 2019, as applicable to your helicopter, except you are not required to contact Airbus Helicopters. \n\n(h) Optional Method of Compliance \n\n\n\tFor Airbus Helicopter Model AS332L or AS332L1 helicopters: Revising the Rotorcraft Flight Manual for your helicopter by inserting the information specified in Appendix 4A, 4B, or 4C of Airbus Helicopters Emergency Alert Service Bulletin AS332 01-00.96, Revision 0, dated December 4, 2019, as applicable to your helicopter model and configuration, and installing a locally made placard on the instrument panel, in accordance with the instructions of section 3.B.1 of Airbus Helicopters Emergency Alert Service Bulletin AS332 01-00.96, Revision 0, dated December 4, 2019, is an acceptable method for compliance with the requirements of paragraph (g) of this AD. \n\n(i) Credit for Previous Actions \n\n\n\tThis paragraph provides credit for actions required by paragraph (g) of this AD, if those actions were performed before the effective date of this AD using Airbus Helicopters Emergency Alert Service Bulletin AS332 01.00.91, Revision 0, dated July 3, 2018. \n\n(j) Special Flight Permit \n\n\n\tSpecial flight permits may be issued in accordance with 14 CFR 21.197 and 21.199 to operate the helicopter to a location where the helicopter can be modified as specified in paragraph (g) of this AD, provided the Rotorcraft Flight Manual revisions and the locally made placard specified in paragraph (h) of this AD are in place. \n\n(k) Alternative Methods of Compliance (AMOCs) \n\n\n\t(1) The Manager, Safety Management Section, Rotorcraft Standards Branch, FAA, may approve AMOCs for this AD. Send your proposal to: Manager, Safety Management Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222- 5110; email 9-ASW-FTW-AMOC-Requests@faa.gov. \n\t(2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, notify your principal inspector or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC. \n\n(l) Related Information \n\n\n\t(1) The subject of this AD is addressed in the European Union Aviation Safety Agency (EASA) AD 2018-0142R1, dated December 9, 2019. This EASA AD may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-0454. \n\t(2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (m)(3) and (4) of this AD. \n\n(m) 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) Airbus Helicopters Emergency Alert Service Bulletin AS332 01.00.91, Revision 1, dated December 4, 2019. \n\t(ii) Airbus Helicopters Emergency Alert Service Bulletin AS332 01.00.96, Revision 0, dated December 4, 2019. \n\t(3) For 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. \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\n((Page 30592)) \n\n\n\n\n\tIssued on May 13, 2020. Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service. (FR Doc. 2020-10667 Filed 5-19-20; 8:45 am) BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2008-07-01SW-08-30R2 · Inadvertent Deployment of Crash Position Indicator (CPI) Beacon
2008-06-30SW-08-30R1 · Inadvertent Deployment of Crash Position Indicator (CPI) Beacon

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 7, 2026. Connections as data: /graph/directive/2020-09-15.json · aircraft systems.