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2013-20-01: Turbine Section

FAA order 2013-20-01 is an airworthiness directive in force since December 5, 2013. The FAA's subject line: Turbine Section. It names Agusta Spa A109: about 107 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
Aircraft
Makes
Agusta S.p.A.
Models
A109A, A109A II, A109C
On this site
Agusta Spa A109 107 registered

Dates and paperwork

In force since
December 5, 2013
Published
October 31, 2013 (signed September 20, 2013)
Docket
FAA-2013-0518
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 Agusta Model A109A, A109AII, and A109C helicopters with a certain third stage turbine wheel installed. This AD requires installing a placard on the instrument panel and revising the limitations section of the rotorcraft flight manual (RFM). This AD was prompted by several incidents of third stage engine turbine wheel failures, which were caused by excessive vibrations at certain engine speeds during steady-state operations. These actions are intended to alert pilots to avoid certain engine speeds during steady-state operations, prevent failure of the third stage engine turbine, engine power loss, and subsequent loss of control of the helicopter.

The order itself the regulatory text, as published

Show the full text (4,287 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): 2013-20-01 Agusta S.p.A. (Type Certificate Currently Held By Agustawestland S.p.A.) (Agusta): Amendment 39-17607; Docket No. FAA- 2013-0518; Directorate Identifier 2009-SW-021-AD. (a) Applicability This AD applies to Agusta Model A109A, A109AII, and A109C helicopters with a third stage turbine wheel, part number 23065833, installed, certificated in any category. (b) Unsafe Condition This AD defines the unsafe condition as a third stage turbine vibration, which could result in turbine failure, engine power loss, and subsequent loss of control of the helicopter. (c) Effective Date This AD becomes effective December 5, 2013. (d) Compliance You are responsible for performing each action required by this AD within the specified compliance time unless it has already been accomplished prior to that time. (e) Required Actions Within 30 days: (1) For Model A109A helicopters, revise the Power Plant Limitations section, page 1-7, of the Model A109A Rotorcraft Flight Manual (RFM) by inserting page 5 of Agusta Bollettino Tecnico No. 109-129, dated February 16, 2009 (BT 109-129). (2) For Model A109AII helicopters, revise the Power Plant Limitations section, page 1-6, of the Model A109AII RFM by inserting page 6 of BT 109-129. (3) For Model A109C helicopters, revise the Power Plant and Transmission Limitations section, page 1-8, of the Model A109C RFM by inserting page 7 of BT 109-129. (4) Install a placard on the instrument panel adjacent to the Engine and Rotor RPM Power Turbine (N2)Indicator that states: MIN. CONT. 97% N2--MIN. TRANS. 95% N2. (f) Alternative Methods of Compliance (AMOCs) (1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Chinh Vuong, Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110; email [email protected]. (2) For operations conducted under a 14 CFR part 119 operating certificate or under [[Page 65163]] 14 CFR part 91, subpart K, we suggest that you notify your principal inspector, or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC. (g) Additional Information (1) The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2009-0037-E, dated February 19, 2009. You may view the EASA AD on theinternet in the AD Docket at http://www.regulations.gov. (h) Subject Joint Aircraft Service Component (JASC) Code: 7250: Turbine Section. (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) Agusta Bollettino Tecnico No. 109-129, dated February 16, 2009. (ii) Reserved. (3) For Agusta service information identified in this AD, contact Agusta Westland, Customer Support & Services, Via Per Tornavento 15, 21019 Somma Lombardo (VA) Italy, ATTN: Giovanni Cecchelli; telephone 39-0331-711133; fax 39 0331 711180; or at http://www.agustawestland.com/technical-bullettins. (4) You may review this service information at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137. (5) You may also view this service information that is incorporated by reference 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.

Related safety bulletins advice on the same designs, not orders

2018-04-30SW-18-13 · Main Transmission Plate Fitting
2012-10-03SW-12-45 · Garmin Model 400W/500W Series GPS-WAAS Navigation System
2007-05-29SW-07-34 · VOR navigation loop antenna
2004-12-01SW-05-18 ·
2003-06-20SW-03-44 ·

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/2013-20-01.json · aircraft systems.