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FAA orders · airworthiness directive · current

2016-22-02: Equipment/Furnishing

FAA order 2016-22-02 is an airworthiness directive in force since December 1, 2016. The FAA's subject line: Equipment/Furnishing. It names Embraer EMB-500 Phenom 100, Embraer EMB-505 Phenom 300: about 892 aircraft on the U.S. register today across them, 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
Embraer S.A.
Models
EMB-500, EMB-505
On this site
Embraer EMB-500 Phenom 100 221 registered
Embraer EMB-505 Phenom 300 671 registered

Dates and paperwork

In force since
December 1, 2016
Published
October 27, 2016 (signed October 17, 2016)
Docket
FAA-2016-8160
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for Embraer S.A. Models EMB-500 and EMB-505 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued 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 incorrect installation of passenger seat attachment fittings. We are issuing this AD to correct the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (6,850 characters)
Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new AD: 2016-22-02 Embraer S.A.: Amendment 39-18691; Docket No. FAA-2016- 8160; Directorate Identifier 2016-CE-019-AD. (a) Effective Date This airworthiness directive (AD) becomes effective December 1, 2016. (b) Affected Ads None. (c) Applicability (1) This AD applies to Embraer S.A. Model EMB-500 airplanes, serial numbers 50000322, 50000324 through 50000328, 50000330 through 50000344, 50000346 through 50000350, and 50000353, certificated in any category; and Embraer S.A. Model EMB-505 airplanes, serial numbers 50500004 through 50500215, 50500217 through 50500245, 50500247 through 50500255, 50500257 through 50500259, 50500261 through 50500263, 50500265, and 50500267, certificated in any category. [[Page 74671]] (2) The airplanes identified in paragraph (c)(1) of this AD had passenger seats installed at manufacturer as listed in Embraer S.A. Service Bulletin (SB) No.: 500-25-0016, dated December 8, 2015; or Embraer S.A. SB No.: 505-25-0020, dated December 8, 2015. Since these are line replaceable units and the unsafe condition of this AD was originated during manufacturing, any passenger seat replaced with another one during routine maintenance is not affected by the actions of this AD. (d) Subject Air Transport Association of America (ATA) Code 25: Equipment/ Furnishing. (e) Reason 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 incorrect installation of passenger seat attachment fittings. We are issuing this proposed AD to detect and correct improperly installed seat attachment fittings, which could result in seat damage causing injury to occupants during an emergency landing condition. (f) Actions and Compliance Unless already done, do the following actions in paragraphs (f)(1) and (2) of this AD following the Accomplishment Instructions in Embraer S.A. Service Bulletin (SB) No.: 500-25-0016, dated December 8, 2015; or Embraer S.A. SB No.: 505-25-0020, dated December 8, 2015, as applicable: (1) Within the next 30 months after December 1, 2016 (the effective date of this AD), inspect each applicable passenger seat for the correct installation of attachment fittings. (2) If any discrepancy is found during the inspection required in paragraph (f)(1) of this AD, before further flight, correct the discrepancy following the applicable service information or using FAA-approved procedures. (g) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Jim Rutherford, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090; email: jim.rutherford@faa.gov. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, only use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, a federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (h) Related Information Refer to MCAI Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD No.: 2016-05-01, dated May 27, 2016, for related information. You may examine the MCAI in the AD docket on the Internet at: https://www.regulations.gov/document?D=FAA-2016-8160-0001. (i) 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) Embraer S.A. Service Bulletin (SB) No.: 500-25-0016, dated December 8, 2015. (ii) Embraer S.A. SB No.: 505-25-0020, dated December 8, 2015. (3) For Embraer S.A. service information identified in this AD, contact Embraer--S.A., Phenom Maintenance Support, Avenida Brigadeiro Faria Lima, 2170, S[atilde]o Jos[eacute] dos Campos--SP-- 12227-901, P.O. Box 36/2, Brasil; phone: +55 12 3927 1000; fax: +55 12 3927-2619; email: phenom.reliability@embraer.com.br; Internet: http://www.embraer.com.br/en-US/Pages/home.aspx. (4) You may view this service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. In addition, you can access this service information on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-8160. (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, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

Related safety bulletins advice on the same designs, not orders

2021-02-11AIR-21-04 · HYDRAULIC POWER SYSTEM
2016-09-07CE-16-23 · Navigation; Degraded Attitude and Heading Reference System (AHRS) Performance When Operating in Areas of...
2010-08-16CE-10-46 · Navigation; Embraer EMB-505 Terrain Awareness Warning System (TAWS) Instructions in Airplane Flight Manual

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/2016-22-02.json · aircraft systems.