Airworthiness directives: Bell,

[Federal Register: October 12, 2001 (Volume 66, Number 198)]

[Proposed Rules]

[Page 52072-52073]

From the Federal Register Online via GPO Access [wais.access.gpo.gov]

[DOCID:fr12oc01-23]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2001-SW-21-AD]

RIN 2120-AA64

Airworthiness Directives; Bell Helicopter Textron Canada Model 430 Helicopters

AGENCY: Federal Aviation Administration, DOT.

ACTION: Notice of proposed rulemaking (NPRM).

SUMMARY: This document proposes the adoption of a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 430 helicopters. This proposal would require changes to the electrical power distribution system. This proposal is prompted by design deficiencies in the electrical systems. The actions specified by the proposed AD are intended to prevent failure of both generators, loss of primary electrical power, and subsequent loss of control of the helicopter.

DATES: Comments must be received on or before December 11, 2001.

ADDRESSES: Submit comments in triplicate to the Federal Aviation Administration (FAA), Office of the Regional Counsel, Southwest Region, Attention: Rules Docket No. 2001-SW-21-AD, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137. You may also send comments electronically to the Rules Docket at the following address: 9-asw-adcomments@faa.gov. Comments may be inspected at the Office of the Regional Counsel between 9 a.m. and 3 p.m., Monday through Friday, except Federal holidays.

FOR FURTHER INFORMATION CONTACT: Robert McCallister, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, Fort Worth, Texas 76193-0110, telephone (817) 222-5121, fax (817) 222-5961.

SUPPLEMENTARY INFORMATION:

Comments Invited

Interested persons are invited to participate in the making of the proposed rule by submitting such written data, views, or arguments as they may desire. Communications should identify the Rules Docket number and be submitted in triplicate to the address specified above. All communications received on or before the closing date for comments, will be considered before taking action on the proposed rule. The proposals contained in this document may be changed in light of the comments received.

Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the proposed rule. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons. A report summarizing each FAA-public contact concerned with the substance of this proposal will be filedin the Rules Docket.

Commenters wishing the FAA to acknowledge receipt of their mailed comments submitted in response to this proposal must submit a self- addressed, stamped postcard on which the following statement is made: ``Comments to Docket No. 2001-SW-21-AD.'' The postcard will be date stamped and returned to the commenter.

Availability of NPRMs

Any person may obtain a copy of this NPRM by submitting a request to the FAA, Office of the Regional Counsel, Southwest Region, Attention: Rules Docket No. 2001-SW-21-AD, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137.

Discussion

Transport Canada, the airworthiness authority for Canada, notified the FAA that an unsafe condition may exist on BHTC Model 430 helicopters. Transport Canada advises that the electrical system has a potential for single fault multiple system failures and does not comply with regulatory requirements for Instrument Flight Rules (IFR) or for Category A design. Transport Canada issued AD No. CF-2000-32R1, dated May 28, 2001, that mandated certain revisions to the Rotorcraft Flight Manual (RFM) to safely cope with this type of electrical failure.

BHTC has issued Alert Service Bulletin (ASB) No. 430-01-19, dated February 22, 2001, which specifies certain modifications to improve the electrical system for BHTC Model 430 helicopters, serial numbers (S/N) 49001 through 49069.

This helicopter model is manufactured in Canada and is type certificated for operation in the United States under the provisions of 14 CFR 21.29 and the applicable bilateral agreement. Pursuant to this bilateral agreement, Transport Canada has kept the FAA informed of the situation described above. The FAA has examined the findings of Transport Canada, reviewed all available information, and determined that AD action is necessary for products of this type design that are certificated for operation in the United States.

We have identified an unsafe condition that is likely to exist or develop on other BHTC Model 430 helicopters of the same type design registered in the United States. Therefore, the proposed AD would require, before further flight after March 31, 2002, accomplishing the electrical power distribution system changes in accordance with BHTC ASB No. 430-01-19, dated February 22, 2001, which is terminating action for the requirements of this AD.

The FAA estimates that this proposed AD would affect 33 helicopters of U.S. registry. The FAA estimates that that it would take approximately 48 work hours per helicopter to accomplish the changes to the electrical system. The average labor rate is $60 per work hour. The manufacturer states in the ASB that the parts will be provided at no cost before March 31, 2002. Based on these figures, the total cost impact of the proposed AD on U.S. operators is estimated to be $95,040.

The regulations proposed herein would 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. Therefore, it is determined that this proposal

[[Page 52073]]

would not have federalism implications under Executive Order 13132.

For the reasons discussed above, I certify that this proposed regulation (1) is not a ``significant regulatory action'' under Executive Order 12866; (2) is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) if promulgated, 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. A copy of the draft regulatory evaluation prepared for this action is contained in the Rules Docket. A copy of it may be obtained by contacting the Rules Docket at the location provided under the caption ADDRESSES.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Safety.

The Proposed Amendment

Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

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]

2. Section 39.13 is amended by adding a new airworthiness directive to read as follows:

   Bell Helicopter Textron Canada: Docket No. 2001-SW-21-AD.

   Applicability: Model 430 helicopters, serial numbers 49002 through 49071, certificated in any category.

   Note 1: This AD applies to each helicopter identified in the preceding applicability provision, regardless of whether it has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD. For helicopters that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

   Compliance: Required as indicated, unless accomplished previously.

   To prevent failure of both generators, loss of primary electrical power, and subsequent loss of control of the helicopter, accomplish the following:

   (a) Before further flight after March 31, 2002, perform the Accomplishment Instructions, paragraphs 1 through 124, of Bell Helicopter Textron Canada Alert Service Bulletin No 430-01-19, dated February 22, 2001, which is terminating action for the requirements of this AD.

   (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Regulations Group, Rotorcraft Directorate, FAA. Operators shall submit their requests through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Regulations Group.

   Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Regulations Group.

   (c) Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199 to operate the helicopter to a location where the requirements of this AD can be accomplished.

   Note 3: The subject of this AD is addressed in Transport Canada (Canada) AD No. CF-2000-32R1, dated May 28, 2001.

   Issued in Fort Worth, Texas, on October 3, 2001. Mark R. Schilling, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.

   [FR Doc. 01-25695Filed10-11-01; 8:45 am]

   BILLING CODE 4910-13-P