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2018-03-01: Main Rotor Blades

FAA order 2018-03-01 is an airworthiness directive in force since February 14, 2018. The FAA's subject line: Main Rotor Blades. It names Agusta Spa AB139, Agusta Spa AW139: about 22 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: rotorcraft systems.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Agusta S.p.A.
Models
AB139, AW139
On this site
Agusta Spa AB139 8 registered
Agusta Spa AW139 14 registered

Dates and paperwork

In force since
February 14, 2018
Published
January 30, 2018 (signed January 22, 2018)
Docket
FAA-2017-0939
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 S.p.A. (Agusta) Model AB139 and AW139 helicopters. This AD requires inspecting the main rotor blade (MRB) tip cap for disbonding. This AD is prompted by a report of the in-flight loss of an MRB tip cap. The actions of this AD are intended to prevent an unsafe condition on these helicopters.

The order itself the regulatory text, as published

Show the full text (4,303 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): 2018-03-01 Agusta S.p.A.: Amendment 39-19174; Docket No. FAA-2017- 0939; Product Identifier 2017-SW-057-AD. (a) Applicability This AD applies to Agusta S.p.A. Model AB139 and AW139 helicopters, certificated in any category, with a main rotor blade (MRB) part number (P/N) 3G6210A00131 with a serial number (S/N) 3615, 3634, 3667, or 3729 installed. (b) Unsafe Condition This AD defines the unsafe condition as disbonding of an MRB tip cap. This condition could result in loss of the MRB tip cap, severe vibrations, and subsequent loss ofcontrol of the helicopter. (c) Effective Date This AD becomes effective February 14, 2018. (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 (1) Within 5 hours time-in-service (TIS), using a tap hammer or equivalent, tap inspect each MRB tip cap for disbonding in the area depicted in Figure 1 of Leonardo Helicopters Emergency Alert Service Bulletin No. 139-508, dated September 12, 2017 (EASB). (i) If there is any disbonding, before further flight, remove the MRB from service. (ii) If there is no disbonding, within 10 hours TIS, remove the MRB from service. (2) After the effective date of this AD, do not install a MRB P/ N 3G6210A00131 with a S/N 3615, 3634, 3667, or 3729 on any helicopter. (f) Alternative Methods of Compliance (AMOCs) (1) The Manager, Safety Management Section, Rotorcraft Standards Branch, FAA, may approve AMOCs for this AD. Send your proposal to: Matt Fuller, Senior Aviation Safety Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email [email protected]. (2) For operations conducted under a 14 CFR part 119 operating certificate or under 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 The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2017-0175-E, dated September 13, 2017. You may view the EASA AD on the internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2017-0939. (h) Subject Joint Aircraft Service Component (JASC) Code: 6210 Main Rotor Blades. (i) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference 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) Leonardo Helicopters Emergency Alert Service Bulletin No. 139-508, dated September 12, 2017. (ii) Reserved. (3) For Leonardo Helicopters service information identified in this AD, contact Leonardo S.p.A. Helicopters, Matteo Ragazzi, Head of Airworthiness, Viale G.Agusta 520, 21017 C.Costa di Samarate (Va) Italy; telephone +39-0331-711756; fax +39-0331-229046; or at http://www.leonardocompany.com/-/bulletins. (4) You may view this service information at FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N- 321, Fort Worth, TX 76177. Forinformation on the availability of this material at the FAA, call (817) 222-5110. (5) You may 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

2010-01-07NM-10-12 · Navigation: Flight Management System

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/2018-03-01.json · aircraft systems.