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2005-17-17: Check valve piston in the lubrication unit

FAA order 2005-17-17 is an airworthiness directive in force since September 12, 2005. The FAA's subject line: Check valve piston in the lubrication unit. It names the Turbomeca (Safran) ARRIUS 2F engine: about 63 aircraft on the U.S. register today, 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
Turbomeca S.A.; Turbomeca S.A.; Turbomeca S.A.
Models
Arrius 2F
Engine series
Turbomeca (Safran) ARRIUS 2F 63 aircraft

Dates and paperwork

In force since
September 12, 2005
Published
August 26, 2005 (signed August 17, 2005)
Docket
FAA-2005-22039
Replaced by
2005-17-17R1
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 Turbomeca S.A. Arrius 2F turboshaft engines. This AD requires replacing certain O-rings on the check valve piston in the lubrication unit. This AD results from a report of a forced landing of a Eurocopter EC120B helicopter. We are issuing this AD to prevent an uncommanded in-flight shutdown of the engine, which could result in a forced autorotation landing and damage to the helicopter.

The order itself the regulatory text, as published

Show the full text (2,828 characters)
2005-17-17 Turbomeca S.A: Amendment 39-14238. Docket No. FAA-2005- 22039; Directorate Identifier 2005-NE-33-AD. Effective Date (a) This airworthiness directive (AD) becomes effective September 12, 2005. Affected ADs (b) None. Applicability (c) This AD applies to Turbomeca S.A. Arrius 2F turboshaft engines. These engines are installed on, but not limited to, Eurocopter EC120B helicopters. Unsafe Condition (d) This AD results from a report of a forced landing of a Eurocopter EC120B helicopter. We are issuing this AD to prevent an uncommanded in-flight shutdown of the engine, which could result in a forced autorotation landing and damage to the helicopter. 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. O-Ring Replacement (f) Replace the O-ring on the check valve piston in the lubrication unit at the intervals specified in Table 1 of this AD. Use the "Instructions to be Incorporated," 2.A. through 2.C. (2) of Turbomeca Alert Service Bulletin No. A319 79 4802, dated June 21, 2005, to replace the O-ring. Table 1.--Compliance Times for O-Ring Replacement If the class of oil is * * * Then replace the O-ring by the later of * * * Thereafter, replace the O- ring within * * * (1) HTS or unknown (2) STD 300 hours time-since-new (TSN) or 50 hours after the effective date of this AD. 450 hours TSN or 50 hours after the effective date of this AD. 300 hours time-since-last replacement (TSR). 500 hours TSR. Alternative Methods of Compliance (g) 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 (h) DGAC airworthiness directive F-2005-122, dated July 20, 2005, also addresses the subject of this AD. Material Incorporated byReference (i) You must use Turbomeca Alert Service Bulletin No. A319 79 4802, dated June 21, 2005 to perform the replacements required by this AD. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Turbomeca S.A., 40220 Tarnos, France; telephone 33 05 59 74 40 00, fax 33 05 59 74 45 15, for a copy of this service information. You may review copies at the Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL- 401, Washington, DC 20590-0001, on the Internet at http://dms.dot.gov; 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 .

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 3, 2026. Connections as data: /graph/directive/2005-17-17.json · aircraft systems.