Federal Aviation Administration (FAA), DOT.
We are adopting a new airworthiness directive (AD) for certain Bell Model 206B and 206L helicopters. This AD requires installing a placard beneath the engine power dual tachometer and revising the operating 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.
This AD is effective December 10, 2013.
The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD as of December 10, 2013.
For service information identified in this AD, contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4; telephone (450) 437-2862 or (800) 363-8023; fax (450) 433-0272; or at http://www.bellcustomer.com/files/. You may review the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the Docket Operations Office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the foreign authority's AD, any incorporated-by-reference service information, the economic evaluation, any comments received, and other information. The street address for the Docket Operations Office (phone: 800-647-5527) is U.S. Department of Transportation, Docket Operations Office, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
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FOR FURTHER INFORMATION CONTACT:
Chinh Vuong, Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110; email email@example.com.
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On June 7, 2013, at 78 FR 34280, the Federal Register published our notice of proposed rulemaking (NPRM), which proposed to amend 14 CFR part 39 by adding an AD that would apply to Bell Model 206B helicopters, serial number (S/N) 004 through 4675, including helicopters converted from Model 206A and Model 206L helicopters, S/N 45001 through 45153, and 46601 through 46617. The NPRM proposed to require installing a placard on the instrument panel below the NR/N2 dual tachometer and revising the Operating Limitations section of the Model 206B RFM and 206L RFM to limit steady-state operation between speeds of 75% and 88%. The proposed requirements were 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 NPRM was prompted by AD No. CF-2007-13R2, dated November 10, 2009, issued by Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada. TCCA issued AD No. CF-2007-13R2 to correct an unsafe condition for certain Model 206B (including those converted from Model 206A) and 206L helicopters. TCCA advises of several failures of third stage turbine wheels used in Rolls Royce 250-C20. According to TCCA, Rolls Royce Start Printed Page 66253has determined that detrimental vibrations can occur within a particular range of turbine speeds, and may be a contributing factor to these failures. Bell has revised the RFM and has provided a corresponding decal to inform pilots to avoid steady-state operations between 75% and 88% turbine speeds.
The TCCA AD requires amending the RFMs, advising pilots of the change, and installing a decal as described in Bell Alert Service Bulletin (ASB) No. 206-07-115, Revision C, dated February 4, 2009, for Model 206B helicopters (ASB 206-07-115) and Bell ASB No. 206L-07-146, Revision B, dated March 3, 2009, for Model 206L helicopters (ASB 206L-07-146).
After our NPRM (78 FR 34280, June 7, 2013) was published, we received comments from one commenter.
Rolls-Royce Corporation requested that in addition to requiring the placard on the instrument panel, we allow operators the option to temporarily mark the Nr/Np gauge with colored tape, to provide a more visual aide to the pilot for the speed avoidance zone.
We disagree. Marking the glass surface of the gauge can create parallax issues when viewing the avoidance ranges on the gauge, resulting in erroneous readings.
These helicopters have been approved by the aviation authority of Canada and are approved for operation in the United States. Pursuant to our bilateral agreement with Canada, TCCA, its technical representative, has notified us of the unsafe condition described in the TCCA AD. We are issuing this AD because we evaluated all information provided by TCCA, reviewed the relevant information, considered the comment received, and determined the unsafe condition exists and is likely to exist or develop on other helicopters of the same type design and that air safety and the public interest require adopting the AD requirements as proposed.
Differences Between This AD and the TCCA AD
The TCCA AD requires compliance within 10 calendar days, while this AD requires compliance within 30 days.
Related Service Information
Bell has issued ASB 206-07-115 and ASB 206L-07-146, which contain procedures for installing a placard on the instrument panel below the main rotor RPM (Nr)/power turbine RPM (N2) dual tachometer and for inserting the RFM changes into the flight manual.
Costs of Compliance
We estimate that this AD will affect 970 helicopters of U.S. Registry. Based on an average labor rate of $85 per hour, we estimate that operators will incur the following costs in order to comply with this AD. Amending the RFM will require about 0.5 work-hour, for a cost per helicopter of about $43 and a cost to U.S. operators of $41,710. Installing the decal will require about 0.2 work-hour and required parts will cost $20, for a cost per helicopter of $37 and a cost to U.S. operators of $35,890. Based on these estimates, the total cost of this AD is $80 per helicopter and $77,600 for the U.S. operator fleet.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: “General requirements.” Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on helicopters identified in this rulemaking action.
This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a “significant regulatory action” under Executive Order 12866;
(2) Is not a “significant rule” under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979);
(3) Will not affect intrastate aviation in Alaska to the extent that it justifies making a regulatory distinction; and
(4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.
We prepared an economic evaluation of the estimated costs to comply with this AD and placed it in the AD docket.
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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
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1. The authority citation for part 39 continues to read as follows:End Amendment Part
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2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD):End Amendment Part
2013-20-13 Bell Helicopter Textron Canada Limited (Bell): Amendment 39-17619; Docket No. FAA-2013-0488; Directorate Identifier 2008-SW-002-AD.
This AD applies to the following helicopters, certificated in any category:
(1) Bell Model 206B, serial number (S/N) 004 through 4675, including helicopters converted from Model 206A; and
(2) Bell Model 206L, S/N 45001 through 45153, and 46601 through 46617.
(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 10, 2013.
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 206B helicopters:
(i) Revise the Operating Limitations section of the Model 206B Rotorcraft Flight Manual (RFM) by inserting Section 1, Operating Limitations, page 1-2A, of Bell BHT-206B-FM-1, revision B-50, dated December 8, 2008.
(ii) Remove placard part number (P/N) 230-075-213-121, if installed.
(iii) Install placard P/N 230-075-213-125, or equivalent, on the instrument panel directly below the dual tachometer.
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(i) Revise the Operating Limitations section of the Model 206L RFM by inserting Section 1, Operating Limitations, page 1-4B, of Bell BHT-206L-FM-1, revision 28, dated December 8, 2008.
(ii) Remove placard P/N 230-075-213-123, if installed.
(ii) Install placard P/N 230-075-213-127, or equivalent, on the instrument panel below the dual tachometer.
(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 firstname.lastname@example.org.
(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
(1) Bell Alert Service Bulletin (ASB) No. 206-07-115, Revision C, dated February 4, 2009, and Bell ASB No. 206L-07-146, Revision B, dated March 3, 2009, which are not incorporated by reference, contain additional information about the subject of this AD. For service information identified in this AD, contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4; telephone (450) 437-2862 or (800) 363-8023; fax (450) 433-0272; or at http://www.bellcustomer.com/files/. 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 Transport Canada Civil Aviation (TCCA) AD No. CF-2007-13R2, dated December 9, 2009. You may view the TCCA AD on the internet in the AD Docket at http://www.regulations.gov.
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) Page 1-2A of Section 1, Operating Limitations, of Bell Rotorcraft Flight Manual BHT-206B-FM-1, Revision B-50, dated December 8, 2008.
(ii) Page 1-4B of Section 1, Operating Limitations, of Bell Rotorcraft Flight Manual BHT-206L-FM-1, Revision 28, dated December 8, 2008.
(3) For Bell service information identified in this AD, contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4; telephone (450) 437-2862 or (800) 363-8023; fax (450) 433-0272; or at http://www.bellcustomer.com/files/.
(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.
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Issued in Fort Worth, Texas, on September 25, 2013.
Lance T. Gant,
Acting Directorate Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2013-24037 Filed 11-4-13; 8:45 am]
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