Airworthiness directives: Bell,
[Federal Register: September 5, 2002 (Volume 67, Number 172)]
[Rules and Regulations]
[Page 56747-56748]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr05se02-1]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002-SW-03-AD; Amendment 39-12868; AD 2002-17-03]
RIN 2120-AA64
Airworthiness Directives; Bell Helicopter Textron, a Division of Textron Canada, Model 407 Helicopters
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; request for comments.
SUMMARY: This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron, A Division of Textron Canada (BHT), Model 407 helicopters. This action requires a fuel filler cap assembly shimming and electrical bonding procedure. This amendment is prompted by the FAA's determination, based on information from the manufacturer, that electrical bonding may be inadequate. The actions specified in this AD are intended to prevent a lack of electrical bonding that could result in an electrical arc, ignition of fuel vapors, and an onboard fire.
DATES: Effective September 20, 2002.
The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of September 20, 2002.
Comments for inclusion in the Rules Docket must be received on or before November 4, 2002.
ADDRESSES: Submit comments in triplicate to the Federal Aviation Administration (FAA), Office of the Regional Counsel, Southwest Region, Attention: Rules Docket No. 2002-SW-03-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.
The service information referenced in this AD may be obtained from Bell Helicopter Textron Canada, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4, telephone (450) 437-2862 or (800) 363-8023, fax (450) 433-0272. This information may be examined at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Ed Cuevas, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, Fort Worth, Texas 76193-0111, telephone (817) 222-5355, fax (817) 222-5961.
SUPPLEMENTARY INFORMATION: Transport Canada, which is the airworthiness authority for Canada, notified the FAA that an unsafe condition may exist on BHT Model 407 helicopters. Transport Canada advises that electrical bonding may be inadequate between the retainer assembly, the fuel filler cap and adapter assembly, and the fuel cell fitting, which can cause arcing while refueling as a result of static discharge. This could ignite the fuel vapor.
BHT has issued Bell Helicopter Textron Alert Service Bulletin No. 407-01-41, dated May 23, 2001, which specifies the shimming of gaps and adding electrical bonding tape to ensure no gaps exist between the retainer assembly, part number (P/N) 206-062-304-101, the fuel filler cap and adapter assembly, P/N 206-362-002-103, and the fuel cell fitting. Transport Canada classified this service bulletin as mandatory and issued AD No. CF-2001-34, dated September 20, 2001, to ensure the continued airworthiness of these helicopters in Canada.
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 the applicable 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.
This unsafe condition is likely to exist or develop on other helicopters of the same type design registered in the United States. Therefore, this AD is being issued to prevent a lack of electrical bonding that could result in an electrical arc, ignition of fuel vapors, and an onboard fire. This AD requires the shimming of gaps and adding electrical bonding tape to ensure that no gaps exist between the retainer assembly, the fuel cap and adapter assembly, and the fuel cell fitting. The actions must be accomplished in accordance with the alert service bulletin described previously. The short compliance time involved is required because the previously described critical unsafe condition could result in substantial damage to a helicopter due to a fire. Some of the affected model helicopters may exceed 50 hours time- in-service (TIS) within a very short period of time. Therefore, the shimming of gaps and adding electrical bonding tape to ensure no gaps exist between the retainer assembly, the fuel filler cap and adapter assembly, and the fuel cell fitting is required within 50 hours TIS, and this AD must be issued immediately.
Since a situation exists that requires the immediate adoption of this regulation, it is found that notice and opportunity for prior public comment hereon are impracticable, and that good cause exists for making this amendment effective in less than 30 days.
The FAA estimates that 291 helicopters will be affected by this AD, that it will take approximately 8 work hours to accomplish the shimming and adding the electrical bonding tape, and that the average labor rate is $60 per work hour. The cost of parts is $111 for the kit required for each of 242 helicopters in the fleet, and $21 for the kit required for the remaining 49 helicopters in the fleet. Based on these figures, the total cost impact of the AD on U.S. operators is estimated to be $167,571.
Comments Invited
Although this action is in the form of a final rule that involves requirements affecting flight safety and, thus, was not preceded by notice and an opportunity for public comment, comments are invited on this rule. Interested persons are invited to comment on this rule by
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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 under the caption ADDRESSES. All communications received on or before the closing date for comments will be considered, and this rule may be amended in light of the comments received. Factual information that supports the commenter's ideas and suggestions is extremely helpful in evaluating the effectiveness of the AD action and determining whether additional rulemaking action would be needed.
Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the rule that might suggest a need to modify the rule. All comments submitted will be available in the Rules Docket for examination by interested persons. A report that summarizes each FAA-public contact concerned with the substance of this AD will be filedin the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their mailed comments submitted in response to this rule must submit a self- addressed, stamped postcard on which the following statement is made: ``Comments to Docket No. 2002-SW-03-AD.'' The postcard will be date stamped and returned to the commenter.
The regulations adopted herein 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. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132.
The FAA has determined that this regulation is an emergency regulation that must be issued immediately to correct an unsafe condition in aircraft, and that it is not a ``significant regulatory action'' under Executive Order 12866. It has been determined further that this action involves an emergency regulation under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979). If it is determined that this emergency regulation otherwise would be significant under DOT Regulatory Policies and Procedures, a final regulatory evaluation will be prepared and placed in the Rules Docket. A copy of it, if filed, may be obtained from the Rules Docket at the location provided under the caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
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Section 39.13 is amended by adding a new airworthiness directive to read as follows:
2002-17-03 Bell Helicopter Textron, a Division of Textron Canada: Amendment 39-12868. Docket No. 2002-SW-03-AD.
Applicability: Model 407 helicopters, with serial numbers less than 53480, 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 within 50 hours time-in-service, unless accomplished previously.
To prevent a lack of electrical bonding that could result in an electrical arc, ignition of fuel vapors, and an onboard fire, accomplish the following:
(a) Perform the fuel filler cap shimming and electrical bonding procedure in accordance with the Accomplishment Instructions in Bell Helicopter Textron Alert Service Bulletin No. 407-01-41, dated May 23, 2001.
(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.
(d) The shimming and electrical bonding procedure shall be done in accordance with the Accomplishment Instructions in Bell Helicopter Textron Alert Service Bulletin No. 407-01-41, dated May 23, 2001. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Bell Helicopter Textron Canada, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4. Copies may be inspected at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
(e) This amendment becomes effective on September 20, 2002.
Note 3: The subject of this AD is addressed in Transport Canada (Canada) AD No. CF-2001-34, dated September 20, 2001.
Issued in Fort Worth, Texas, on August 21, 2002. David A. Downey, Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 02-22174Filed9-4-02; 8:45 am]
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