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2016-26-04: Main Rotor Blades

FAA order 2016-26-04 is an airworthiness directive in force since February 8, 2017. The FAA's subject line: Main Rotor Blades. It names Robinson R44, Robinson R66: about 2,354 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
Robinson Helicopter Company
Models
R44, R44 II, R66
On this site
Robinson R44 1,933 registered
Robinson R66 421 registered

Dates and paperwork

In force since
February 8, 2017
Published
January 4, 2017 (signed December 15, 2016)
Docket
FAA-2016-0733
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 Robinson Helicopter Company (Robinson) Model R44, R44 II, and R66 helicopters. This AD requires inspecting the main rotor blade (MRB). This AD was prompted by a determination that some MRBs may have reduced blade thickness due to blending out corrosion. The actions are intended to prevent the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,501 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): 2016-26-04 Robinson Helicopter Company: Amendment 39-18762; Docket No. FAA-2016-0733; Directorate Identifier 2015-SW-040-AD. (a) Applicability This AD applies to Robinson Helicopter Company (Robinson) Model R44 and R44 II helicopters with a main rotor blade (MRB) part number (P/N) C016-7, Revision AA through AE installed; and Model R66 helicopters with a MRB P/N F016-2, Revision A through E, installed; certificated in any category. (b) Unsafe Condition This AD defines the unsafe condition as a fatigue crack on an MRB. This condition could result in failure of an MRB and loss of helicopter control. (c) Effective Date This AD becomes effective February 8, 2017. (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 100 hours time-in-service or at the next annual inspection, whichever occurs first: (1) Clean each MRB in the area depicted in Figure 1 of Robinson R44 Service Bulletin SB-89, dated March 30, 2015 (SB-89), or Robinson R66 Service Bulletin SB-13, dated March 30, 2015 (SB-13), as applicable to your model helicopter. (2) Using 10X or higher power magnification and a light, visually inspect the upper and lower MRB surfaces and trailing edge as depicted in Figure 1 of SB-89 or SB-13, whichever applies to your helicopter, for a crack, a nick, a scratch, a dent, or corrosion. If there is a crack, a nick, a scratch, a dent, orany corrosion, repair the MRB to an airworthy configuration if the damage is within the maximum repair damage limits or remove the MRB from service. (3) Alter the MRB in accordance with Compliance Procedure, paragraphs 4 through 19, of SB-89 or SB-13, as applicable to your model helicopter. Equivalent tubing may be used for R7769-1 and R7769-6 tubes. Power tools may not be used for this procedure. (f) Alternative Methods of Compliance (AMOCs) (1) The Manager, Los Angeles Aircraft Certification Office, FAA, may approve AMOCs for this AD. Send your proposal to: Eric Schrieber, Aviation Safety Engineer, Los Angeles Aircraft Certification Office, Transport Airplane Directorate, FAA, 3960 Paramount Blvd., Lakewood, California 90712; telephone (562) 627- 5348; email 9-ANM-LAACO-AMOC-REQUESTS@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 aprincipal 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) Subject Joint Aircraft Service Component (JASC) Code: 6210, Main Rotor Blades. (h) 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) Robinson R44 Service Bulletin SB-89, dated March 30, 2015. (ii) Robinson R66 Service Bulletin SB-13, dated March 30, 2015. (3) For Robinson Helicopter Company service information identified in this AD, contact Robinson Helicopter Company, 2901 Airport Drive, Torrance, CA 90505; telephone (310) 539-0508; fax (310) 539-5198; or at http://www.robinsonheli.com. (4) You may view this service information at FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy, [[Page 718]] Room 6N-321, Fort Worth, TX 76177. 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.

Related safety bulletins advice on the same designs, not orders

2024-10-292024-05 · Engine/Transmission Coupling, Gearmotor Assembly
2022-11-212022-21 · EMERGENCY FLOTATION SECTION, Pop-Out Float Under-inflation.
2022-04-11AIR-22-08 · MAIN ROTOR DRIVE SYSTEM,TAIL ROTOR DRIVE SYSTEM
2022-03-03AIR-22-03 · Robinson Helicopter Company Model R22, R44, and R66 Helicopters; Emergency Locator Transmitter Retention
2021-08-24AIR-21-14 · Robinson R44 and R66 HeliSAS Autopilot/Garmin Primary Flight Display (PFD) Interface

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/2016-26-04.json · aircraft systems.