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2010-18-13: Blade

FAA order 2010-18-13 is an airworthiness directive in force since October 18, 2010. The FAA's subject line: Blade. It names the Pratt & Whitney PW4052, Pratt & Whitney PW4056, Pratt & Whitney PW4060, Pratt & Whitney PW4062, Pratt & Whitney PW4062A, Pratt & Whitney PW4090, Pratt & Whitney PW4158, Pratt & Whitney PW4168A, Pratt & Whitney PW4460, Pratt & Whitney PW4462 engines: about 145 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
Pratt & Whitney Division
Models
PW4052, PW4056, PW4060, PW4062, PW4062A, PW4074, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, PW4152, PW4156A, PW4158, PW4164, PW4168, PW4168A, PW4460, PW4462
Engine series
Pratt & Whitney PW4052 1 aircraft
Pratt & Whitney PW4056 25 aircraft
Pratt & Whitney PW4060 14 aircraft
Pratt & Whitney PW4062 6 aircraft
Pratt & Whitney PW4062A 2 aircraft
Pratt & Whitney PW4090 2 aircraft
Pratt & Whitney PW4158 65 aircraft
Pratt & Whitney PW4168A 12 aircraft
Pratt & Whitney PW4460 10 aircraft
Pratt & Whitney PW4462 8 aircraft

Dates and paperwork

In force since
October 18, 2010
Published
September 13, 2010 (signed August 26, 2010)
Docket
FAA-2010-0217
Replaced by
2012-18-17
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 PW PW4052, PW4056, PW4060, PW4062, PW4062A, PW4074, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, PW4152, PW4156A, PW4158, PW4164, PW4168, PW4168A, PW4460, and PW4462 turbofan engines. This AD requires initial and repetitive fluorescent penetrant inspections (FPI) for cracks in the blade locking and loading slots of the high-pressure compressor (HPC) drum rotor disk assembly. This AD results from reports of cracked locking and loading slots in the HPC drum rotor disk assembly. We are issuing this AD to detect cracks in the locking and loading slots in the HPC drum rotor disk assemblies, which could result in rupture of the HPC drum rotor disk assembly and damage to the airplane.

The order itself the regulatory text, as published

Show the full text (4,143 characters)
2010-18-13 Pratt & Whitney: Amendment 39-16427. Docket No. FAA-2010- 0217; Directorate Identifier 2009-NE-23-AD. Effective Date (a) This airworthiness directive (AD) becomes effective October 18, 2010. Affected ADs (b) None. Applicability (c) This AD applies to Pratt & Whitney (PW) PW4052, PW4056, PW4060, PW4062, PW4062A, PW4074, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, PW4152, PW4156A, PW4158, PW4164, PW4168, PW4168A, PW4460, and PW4462 turbofan engines. These engines are installed on, but not limited to, Boeing 747-400, 767-200, 767-300, 777-200, and 777-300 airplanes; McDonnell Douglas MD-11 airplanes; and Airbus A300-600, A310-300, and A330-200 airplanes. Unsafe Condition (d) This AD results from reports of cracked locking and loading slots in the high-pressure compressor (HPC) drum rotor disk assembly. We are issuing this AD to detect cracks in the locking and loading slots in the HPC drum rotor disk assemblies, which could result in rupture of the HPC drum rotor disk assembly 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. Local Fluorescent Penetrant Inspection (f) Perform a local fluorescent penetrant inspection for cracks in the HPC drum rotor disk assembly blade locking and loading slots of the specific stages of the HPC drum rotor disk assemblies from which any of the blades are removed as specified in Table 1 of this AD. Table 1--Compliance Times and Service Bulletins by Engine Model For Engine Model Inspect whenever ... Use... (1) PW4074, PW4077, PW4077D, PW4084D, PW4090, and PW4090-3. Any of the 13thor 14thstage blades are removed during a shop visit. Paragraphs 1.A. through 1.B. of the Accomplishment Instructions of PW4G-112-72-264, Revision 2, dated February 23, 2010. (2) PW4164, PW4168, and PW4168A. Any of the 13th, 14th, or 15thstage blades are removed during a shop visit. Paragraphs 1.A. through 1.C of the Accomplishment Instructions of PW4G-100-72-186, Revision 1, dated September 2, 2004. (3) PW4052, PW4056, PW4060, PW4062, PW4062A, PW4152, PW4156A, PW4158, PW4460, and PW4462. Any of the 13th, 14th, or 15th stage blades are removed during a shop visit. Paragraphs 1.A. through 1.C. of the Accomplishment Instructions of PW4ENG 72-796, dated June 11, 2009. (g) Remove from service any HPC drum rotor disk assembly found with a crack in the blade loading and locking slots of the HPC drum rotor disk assembly. Alternative Methods of Compliance (h) The Manager, Engine 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 (i) Contact Rose Len, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA01803; e-mail: rose.len@faa.gov; telephone (781) 238-7772; fax (781) 238-7199, for more information about this AD. Material Incorporated by Reference (j) You must use the service information specified in the following Table 2 to perform the inspections required by this AD. The Director of the Federal Register approved the incorporation by reference of the documents listed in the following Table 2 in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Pratt & Whitney, 400 Main St., East Hartford, CT 06108; telephone (860) 565- 7700; fax (860) 565-1605, for a copy of this service information. You may review copies at the FAA, New England Region, 12 New England Executive Park, Burlington, MA; or 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. Table 2--Incorporation by Reference Pratt & Whitney Service Bulletin No. Page Revision Date PW4G-100-72-186 Total Pages: 11 ALL 1 September 2, 2004 PW4G-112-72-264 Total Pages: 11 ALL 2 February 23, 2010 PW4ENG 72-796 Total Pages: 22 ALL Original June 11, 2009

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/2010-18-13.json · aircraft systems.