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FAA orders · airworthiness directive · historical

2014-13-09: Tail Rotor

FAA order 2014-13-09 is an airworthiness directive in force since July 30, 2014. The FAA's subject line: Tail Rotor. It names Airbus Helicopters EC-135 now H135: about 397 aircraft on the U.S. register today, 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
Airbus Helicopters Deutschland GmbH
Models
EC135P1, EC135P2, EC135P2+, EC135T1, EC135T2, EC135T2+/EC635T2+
On this site
Airbus Helicopters EC-135 now H135 397 registered

Dates and paperwork

In force since
July 30, 2014
Published
July 15, 2014 (signed July 14, 2014)
Docket
FAA-2014-0440
Replaced by
2026-03-02
Status
Historical
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 AHD Model EC135P1, P2, P2+, T1, T2, and T2+ helicopters. This AD requires repetitive visual inspections of the ring frame X9227 for a crack and, if there is a crack, replacing the ring frame before further flight. This AD is prompted by a fatigue crack in the ring frame. These actions are intended to detect a crack in the ring frame and prevent loss of the tail rotor and subsequent loss of control of the helicopter.

The order itself the regulatory text, as published

Show the full text (4,759 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): 2014-13-09 Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter Deutschland GmbH): Amendment 39-17885; Docket No. FAA-2014-0440; Directorate Identifier 2013-SW-075-AD. (a) Applicability This AD applies to Model EC135P1, P2, P2+, T1, T2, and T2+ helicopters with mounting ring frame X9227, part number (P/N) L535H2120301, P/N L535H2120303, or P/N L535H2120304, installed, except those with frame reinforcement P/N L535H2100201 installed, certificated in any category. (b) Unsafe Condition This AD defines the unsafe condition as a fatigue crack in a ring frame. This condition could result in loss of a tail rotor and subsequent loss of control of the helicopter. (c) Effective Date This AD becomes effective July 30, 2014. (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) On or before 100 hours time-in-service (TIS), or within 50 hours TIS for helicopters with more than 100 hours TIS, and thereafter at intervals not to exceed 50 hours TIS, using a 10X or higher power magnifying glass and a light, visually inspect the ring frame X9227 for a crack between the rivets as shown in Figure 2 of Eurocopter Alert Service Bulletin ASB EC135-53A-029, Revision 0, dated November 19, 2013. Paint cracks are permissible. (2) If there is a crack, before further flight, replace the ring frame X9227 with an airworthy part.(f) Special Flight Permits Special flight permits are prohibited. (g) Alternative Methods of Compliance (AMOCs) (1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Matt Fuller, Senior Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110; email matthew.fuller@faa.gov. (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. (h) Additional Information (1) Eurocopter Safety Information Notice No. 2636-S-53, Revision 0, dated October 10, 2013, which is not incorporated by reference, contains additional information about the subject of this AD. You may review a copy of the service information at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137. (2) The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2013-0289-E, dated December 6, 2013. You may view the EASA AD on the Internet at http://www.regulations.gov in Docket No. FAA-2014-0440. (i) Subject Joint Aircraft Service Component (JASC) Code: 5302 Tail Rotor. (j) 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) Eurocopter Alert Service Bulletin ASB EC135-53A-029, Revision 0, dated November 19, 2013. (ii) Reserved. (3) For service information identified in this AD, contact Airbus Helicopters, Inc., 2701 N. Forum Drive, Grand Prairie, TX [[Page 41098]] 75052; telephone (972) 641-0000 or (800) 232-0323; fax (972) 641- 3775; or at http://www.airbushelicopters.com/techpub. (4) You may view this service information at FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137. For information 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. Issued in Fort Worth, Texas, on June 25, 2014.

Related safety bulletins advice on the same designs, not orders

2012-10-03SW-12-45 · Garmin Model 400W/500W Series GPS-WAAS Navigation System
2009-05-07SW-09-26 · Operation with Emergency Flotation System ARMED
2008-08-27SW-08-42 · Emergency Float with Liferaft Kits (kits)

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/2014-13-09.json · aircraft systems.