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2016-20-15: Engine fan stator module assembly

FAA order 2016-20-15 is an airworthiness directive in force since November 18, 2016. The FAA's subject line: Engine fan stator module assembly. It names the General Electric GENX-1B67/P2, General Electric GENX-1B70/P2, General Electric GENX-1B74/75/ engines: about 105 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Engine
Makes
General Electric Company
Models
GEnx-1B64/P2, GEnx-1B67/P2, GEnx-1B70/75/P2, GEnx-1B70/P2, GEnx-1B70C/P2, GEnx-1B74/75/P2
Engine series
General Electric GENX-1B67/P2 1 aircraft
General Electric GENX-1B70/P2 44 aircraft
General Electric GENX-1B74/75/ 60 aircraft

Dates and paperwork

In force since
November 18, 2016
Published
October 14, 2016 (signed September 30, 2016)
Docket
FAA-2016-5872
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 all General Electric Company (GE) GEnx-1B64/P2, -1B67/P2, -1B70/P2, -1B70C/ P2, -1B70/75/P2, and -1B74/75/P2 turbofan engines with engine assembly, part number (P/N) 2447M10G01 or P/N 2447M10G02, installed. This AD was prompted by a report of a significant fan rub event. This AD requires rework of the engine fan stator module assembly. We are issuing this AD to prevent failure of the fan blades and the load reduction device, loss of power to one or more engines, loss of thrust control, and loss of the airplane.

The order itself the regulatory text, as published

Show the full text (4,423 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 airworthiness directive (AD): 2016-20-15 General Electric Company: Amendment 39-18681; Docket No. FAA-2016-5872; Directorate Identifier 2016-NE-11-AD. (a) Effective Date This AD is effective November 18, 2016. (b) Affected ADs None. (c) Applicability This AD applies to all General Electric Company (GE) GEnx-1B64/ P2, -1B67/P2, -1B70/P2, -1B70C/P2, -1B70/75/P2, and -1B74/75/P2 turbofan engines with engine assembly, part number (P/N) 2447M10G01 or P/N 2447M10G02, installed. (d) Unsafe Condition This AD was prompted by a report of a significant fan rub event. We are issuing this AD to prevent failure of the fan blades and the load reduction device, loss of power to one or more engines, loss of thrust control, and loss of the airplane. (e) Compliance Comply with this AD within the compliance times specified, unless already done. (1) Modify the fan stator module assembly, with one of the following methods, before December 31, 2016. (i) Use paragraphs 3.B.(1) through 3.B.(6) or 3.C.(1) through 3.C.(6) of the Accomplishment Instructions of GE GEnx-1B Service Bulletin (SB) 72-0314 R00, dated April 1, 2016, to do the modification. (ii) Use paragraphs 3.B.(1) through 3.B.(6) or 3.C.(1) through 3.C.(6) of the Accomplishment Instructions of GE GEnx-1B SB 72-0309 R00, dated March 11, 2016, to do the modification. (iii) Use paragraph 3.A. of the Accomplishment Instructions of GE GEnx-1B SB 72-0317 R00, dated June 29, 2016, to do the modification. (2) Reserved. (f) Terminating Action Compliance with this AD constitutes terminating action for AD 2016-06-08, Amendment 39-18439 (81 FR 14704, March 18, 2016) (``AD 2016-06-08'') and AD 2016-08-12, Amendment 39-18488 (81 FR 23581, April 22, 2016) (``AD 2016-08-12''), provided that all of the airplanes within the operator's fleet that have engines identified in paragraph (c) of this AD are modified as specified in paragraph (e) of this AD. After fleet incorporation of this AD, do not install any engine listed in paragraph (c) of this AD unless the engine is modified as specified in paragraph (e) of this AD, or AD 2016-06-08, or AD 2016-08-12. (g) Alternative Methods of Compliance (AMOCs) The Manager, Engine Certification Office, FAA, may approve AMOCs to this AD. Use the procedures found in 14 CFR 39.19 to make your request. You may email your request to: [email protected]. (h) Related Information (1) For more information about this AD, contact Christopher McGuire, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7120; fax: 781-238-7199; email: [email protected]. (2) AD 2016-06-08 and AD 2016-08-12 pertain to the subject of this AD. (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) General Electric Company (GE) GEnx-1B Service Bulletin (SB) 72-0309 R00, dated March 11, 2016. (ii) GE GEnx-1B SB 72-0314 R00, dated April 1, 2016. (iii) GE GEnx-1B SB 72-0317 R00, dated June 29, 2016. (3) For GE service information identified in this AD, contact General Electric Company, GE Aviation, Room 285, 1 Neumann Way, Cincinnati, OH 45215; phone: 513-552-3272; email: [email protected]. (4) You may view this service information at FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA. For [[Page 70928]] information on the availability of this material at the FAA, call 781-238-7125. (5) You may view this service information 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.

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/2016-20-15.json · aircraft systems.