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2024-14-08: Pneumatic System

FAA order 2024-14-08 is an airworthiness directive in force since September 25, 2024. The FAA's subject line: Pneumatic System. It names Embraer ERJ 170 E170 and E175: about 759 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: heating, ice protection and utility systems.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Embraer S.A.
Models
ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD, ERJ 170-100 SU, ERJ 170-200 LL, ERJ 170-200 LR, ERJ 170-200 STD, ERJ 170-200 SU
On this site
Embraer ERJ 170 E170 and E175 759 registered

Dates and paperwork

In force since
September 25, 2024
Published
August 21, 2024 (signed July 12, 2024)
Docket
FAA-2024-0772
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 Embraer S.A. Model ERJ 170 airplanes. This AD was prompted by a manufacturing quality escape concerning some overheat detection system (ODS) sensing elements. This AD requires inspecting the ODS sensing elements and performing applicable corrective actions, and prohibits the installation of affected parts, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) 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 (6,948 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: 2024-14-08 Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.): Amendment 39-22789; Docket No. FAA-2024-0772; Project Identifier MCAI-2023-01203-T. (a) Effective Date This airworthiness directive (AD) is effective September 25, 2024. (b) Affected ADs None. (c) Applicability This AD applies to Embraer S.A. (Type Certificate previously held by Yaborã Indústria Aeronáutica S.A.) Model ERJ 170-100 LR, -100 SE, -100 STD, and -100 SU airplanes, and Model ERJ 170-200 LL, -200 LR, -200 STD, and -200 SU airplanes, certificated in any category, as identified in Agência Nacional de Aviação Civil (ANAC) AD 2023-11-01, effective November 21, 2023 (ANAC AD 2023-11-01). (d) Subject Air Transport Association (ATA) of America Code 36, Pneumatic System. (e) Unsafe Condition This AD was prompted by a manufacturing quality escape concerning some overheat detection system (ODS) sensing elements. The FAA is issuing this AD to address defective sensing elements. The unsafe condition, if not addressed, could result in a sensing element not being able to detect a thermal bleed leak, which is a latent failure, and depending on the affected area, may start an ignition source in the fuel tank, which could damage some electronic boxes and expose the wing structure to high temperature gradients and unexpected thermal loads, which could result in reduced structural integrity of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Requirements Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, ANAC AD 2023-11-01. (h) Exceptions to ANAC AD 2023-11-01 (1) Where ANAC AD 2023-11-01 refers to its effective date, this AD requires using the effective date of this AD. (2) Where paragraphs (b)(1), (c)(1), (d)(1), (e)(1), (f)(1), and (g)(1), of ANAC AD 2023-11-01 specify to inspect ODS sensing elements at various locations, this AD requires adding "in accordance with Embraer Service Bulletin 170-36-0027, revision 04, dated September 5, 2023; or later revisions approved by ANAC." (3) Where paragraphs (b) through (h) of ANAC AD 2023-11-01 specify on-condition actions based on the results of the ODS sensing element inspections required by paragraphs (b)(1), (c)(1), (d)(1), (e)(1), (f)(1), and(g)(1) of ANAC AD 2023-11-01, this AD requires performing all applicable on-condition actions before further flight after each inspection. (4) This AD does not adopt paragraph (k) of ANAC AD 2023-11-01. (i) Parts Returned to Supplier Where the service information referenced in ANAC AD 2023-11-01 specifies to send removed sensing elements to the supplier, this AD does not include that requirement. (j) Additional AD Provisions The following provisions also apply to this AD: (1) 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 responsible Flight Standards Office, as appropriate. If sending information directly to the manager of the International Validation Branch, mail it to the address identified in paragraph (k) of this AD or email to: 9-ANM-Seattle-ACO-AMOC-Requests@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. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, International Validation Branch, FAA; or ANAC; or ANAC's authorized Designee. If approved by the ANAC Designee, the approval must include the Designee's authorized signature. (3) Required for Compliance (RC): Except as required by paragraph (j)(2) of this AD, if any service information referenced in ANAC AD 2023-11-01 contains steps in the Accomplishment Instructions or figures that are labeled as RC, the instructions in RC steps, including subparagraphs under an RC step and any figures identified in an RC step, must be done to comply with this AD; any steps including substeps under those steps, that are not identified as RC are recommended. The instructions in steps, including substeps under those steps, not identified as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the instructions identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to instructions identified as RC require approval of an AMOC. If a step or substep is labeled "RC Exempt," then the RC requirement is removed from that step or substep. (k) Additional Information For more information about this AD, contact Joshua Bragg, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: 817-222-5366; email: joshua.k.bragg@faa.gov. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this material as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Agência Nacional de Aviação Civil (ANAC) AD 2023-11-01, effective November 21, 2023. (ii) [Reserved] (3) For ANAC AD 2023-11-01, contact ANAC, Aeronautical Products Certification Branch (GGCP), Rua Dr. Orlando Feirabend Filho, 230-Centro Empresarial Aquarius-Torre B-Andares 14 a 18, Parque Residencial Aquarius, CEP 12.246-190-São José dos Campos-SP, Brazil; phone 55 (12) 3203-6600; email pac@anac.gov.br; website anac.gov.br/en/. You may find this ANAC AD on the ANAC website sistemas.anac.gov.br/certificacao/DA/DAE.asp. (4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th Street, Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (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 July 12, 2024. Suzanne Masterson, Deputy Director, Integrated Certificate Management Division, Aircraft Certification Service. [FR Doc. 2024-18634 Filed 8-20-24; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2020-06-18NM-20-12 · Powerplant System - Operating in Icing Conditions

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/2024-14-08.json · aircraft systems.