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2009-24-04: Fan spinner

FAA order 2009-24-04 is an airworthiness directive in force since December 28, 2009. The FAA's subject line: Fan spinner. It names the Rolls-Royce AE 3007A1, Rolls-Royce AE 3007A1/3, Rolls-Royce AE 3007A1E, Rolls-Royce AE 3007A1P, Rolls-Royce AE 3007C, Rolls-Royce AE 3007C1, Rolls-Royce AE3007 series engines: about 327 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
Rolls-Royce Corporation
Models
AE 3007A1, AE 3007A1E, AE 3007A1P, AE 3007A1/1, AE 3007A1/3, AE 3007A3, AE 3007C, AE 3007C1
Engine series
Rolls-Royce AE 3007A1 4 aircraft
Rolls-Royce AE 3007A1/3 7 aircraft
Rolls-Royce AE 3007A1E 36 aircraft
Rolls-Royce AE 3007A1P 59 aircraft
Rolls-Royce AE 3007C 16 aircraft
Rolls-Royce AE 3007C1 20 aircraft
Rolls-Royce AE3007 series 185 aircraft

Dates and paperwork

In force since
December 28, 2009
Published
November 23, 2009 (signed November 13, 2009)
Docket
FAA-2009-0246
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 Rolls-Royce Corporation (RRC) AE 3007A1/1, AE 3007A1/3, AE 3007A1, AE 3007A1E, AE 3007A1P, AE 3007A3, AE 3007C, and AE 3007C1 turbofan engines with a fan spinner part number (P/N) 23070964 or P/N 23078783, installed. This AD requires replacement of the fan spinner. This AD results from a report of a fan spinner releasing from an AE 3007A turbofan engine, during flight. We are issuing this AD to prevent the fan spinner from releasing, which could result in injury, damage to the engine, and damage to the airplane.

The order itself the regulatory text, as published

Show the full text (2,974 characters)
2009-24-04 Rolls-Royce Corporation (formerly Allison Engine Company): Amendment 39-16091. Docket No. FAA-2009-0246; Directorate Identifier 2009-NE-04-AD. Effective Date (a) This airworthiness directive (AD) becomes effective December 28, 2009. Affected ADs (b) None. Applicability (c) This AD applies to Rolls-Royce Corporation (RRC) AE 3007A1/ 1, AE 3007A1/3, AE 3007A1, AE 3007A1E, AE 3007A1P, AE 3007A3, AE 3007C, and AE 3007C1 turbofan engines with a fan spinner part number (P/N) 23070964 or P/N 23078783, installed. These engines are installed on, but not limited to, Embraer EMB-135, EMB-145, and Cessna Citation X airplanes. Unsafe Condition (d) This AD results from a report of a fan spinner releasing from an AE 3007A turbofan engine during flight. We are issuing this AD to prevent the fan spinner from releasing, which could result in injury, damage to the engine, and damage to the airplane. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done. Replacement of the Fan Spinner (f) For RRC AE 3007A1/1, AE 3007A1/3, AE 3007A1, AE 3007A1E, AE 3007A1P, and AE 3007A3 turbofan engines, remove fan spinner P/N 23070964 or P/N 23078783 at the next shop visit, but no later than 4,000 additional cycles-in-service (CIS) after the effective date of this AD, and install an approved P/N fan spinner. (g) For RRC AE 3007C and AE 3007C1 turbofan engines, remove fan spinner P/N 23070964 or P/N 23078783 at the next shop visit, but no later than 4,000 additional CIS after the effective date of this AD, and install an approved P/N fan spinner. Fan Spinner Installation Prohibition (h) After the effective date of this AD, do not install any fan spinner P/N 23070964 or P/N 23078783 on any Rolls Royce Corporation engine. Definition (i) For the purpose of this AD, a shop visit is induction of the engine into the engine maintenance shop for any cause. Alternative Methods of Compliance (j) The Manager, Chicago Aircraft Certification Office, has the authority to approve alternative methods of compliance for this AD if requested using the procedures found in 14 CFR 39.19. Related Information (k) Contact Michael Downs, Aerospace Engineer, Chicago Aircraft Certification Office, FAA, Small Airplane Directorate, 2300 East Devon Avenue, Des Plaines, IL 60018; e-mail: michael.downs@faa.gov; telephone: (847) 294-7870; fax: (847) 294-7834, for more information about this AD. (l) Rolls-Royce Corporation Service Bulletin (SB) No. AE 3007A- 72-361, dated June 26, 2008, and SB No. AE 3007C-72-285, dated June 26, 2008, pertain to the subject of this AD. Contact Rolls-Royce Corporation, P.O. Box 420, Indianapolis, IN 46206; telephone (317) 230-3774; fax (317) 230-8084; e-mail: indy.pubs.services@rolls- royce.com, for a copy of this service information. Material Incorporated by Reference (m) None.

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/2009-24-04.json · aircraft systems.