[Federal Register Volume 64, Number 32 (Thursday, February 18, 1999)] [Proposed Rules] [Pages 8022-8024] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 99-3887] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-CE-04-AD] RIN 2120-AA64 Airworthiness Directives; Fairchild Aircraft, Inc. SA226-T, SA226-T(B), SA226-AT, and SA226-TC Airplanes AGENCY: Federal Aviation Administration, DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Fairchild Aircraft, Inc. (Fairchild) Models SA226-T, SA226-T(B), SA226-AT, and SA226-TC airplanes. The proposed AD would require replacing the existing brake master cylinders with brake master cylinders of improved design. The proposed AD is the result of an accident of a Model SA226-TC airplane where the master cylinder did not totally release the brake hydraulic pressure at the beginning of the takeoff roll. This caused the brakes to drag and the left-hand main wheel brakes to overheat, resulting in a wheel well area fire. The actions specified by the proposed AD are intended to prevent this situation from occurring on other airplanes, which could result in loss of control of the airplane and passenger injury during landing, takeoff, or taxi operations. DATES: Comments must be received on or before April 12, 1999. ADDRESSES: Submit comments in triplicate to the Federal Aviation Administration (FAA), Central Region, Office of the Regional Counsel, Attention: Rules Docket No. 99-CE-04-AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. Comments may be inspected at this location between 8 a.m. and 4 p.m., Monday through Friday, holidays excepted. Service information that applies to the proposed AD may be obtained from Fairchild Aircraft, Inc., P.O. Box 790490, San Antonio, Texas 78279-0490; telephone: (210) 824-9421; facsimile: (210) 820-8609. This information also may be examined at the Rules Docket at the address above. FOR FURTHER INFORMATION CONTACT: Werner Koch, FAA, Airplane Certification Office, 2601 Meacham Boulevard, Fort Worth, Texas 76193- 0150; telephone: (817) 222-5133; facsimile: (817) 222-5960. 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, specified above, will be considered before taking action on the proposed rule. The proposals contained in this notice 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 that summarizes each FAA-public contact concerned with the substance of this proposal will be filed in the Rules Docket. Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to this notice must submit a self-addressed, stamped postcard on which the following statement is made: ``Comments to Docket No. 99-CE-04-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, Central Region, Office of the Regional Counsel, Attention: Rules Docket No. 99-CE-04-AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. Discussion The FAA has received a report of an accident on a Fairchild Model SA226-TC airplane of Canadian registry. Analysis of the accident reveals that the master cylinder did not totally release the brake hydraulic pressure at the beginning of the takeoff roll. This caused the brakes to drag and the left-hand main wheel brakes to overheat, resulting in a wheel well area fire. This condition, if not corrected on other airplanes of the same type design, could result in a wheel well area fire, loss of control of the airplane, and passenger injury during landing, takeoff, or taxi operations. Relevant Service Information Fairchild has issued Service Bulletin 226-32-046, which incorporates the following pages: [[Page 8023]] ------------------------------------------------------------------------ Pages Revision level and date ------------------------------------------------------------------------ 4, 5, 6, 8, 9, and 10.................. Issued: November 29, 1983. 1, 2, 3, and 7......................... Revised: March 19, 1984. ------------------------------------------------------------------------ This service bulletin specifies procedures for replacing the existing brake master cylinders with brake master cylinders of improved design. The FAA's Determination After examining the circumstances and reviewing all available information related to the incidents described above, including the above-referenced service information, the FAA has determined that AD action should be taken to prevent the main wheel brakes from overheating because of the existing brake master cylinders not totally releasing the brake hydraulic pressure and causing the brakes to drag. This could result in loss of control of the airplane and passenger injury during landing, takeoff, or taxi operations. Explanation of the Provisions of the Proposed AD Since an unsafe condition has been identified that is likely to exist or develop in other Fairchild Models SA226-T, SA226-T(B), SA226- AT, and SA226-TC airplanes of the same type design, the FAA is proposing AD action. The proposed AD would require replacing the existing brake master cylinders with brake master cylinders of improved design. Accomplishment of the proposed replacement would be required in accordance with Fairchild Service Bulletin 226-32-046, which incorporates the following pages: ------------------------------------------------------------------------ Pages Revision level and date ------------------------------------------------------------------------ 4, 5, 6, 8, 9, and 10................. Issued: November 29, 1983. 1, 2, 3, and 7......................... Revised: March 19, 1984. ------------------------------------------------------------------------ Cost Impact The FAA estimates that 200 airplanes in the U.S. registry would be affected by the proposed AD, that it would take approximately 16 workhours per airplane to accomplish the proposed action, and that the average labor rate is approximately $60 an hour. Parts cost approximately $1,200 per airplane. Based on these figures, the total cost impact of the proposed AD on U.S. operators is estimated to be $432,000, or $2,160 per airplane. Regulatory Impact The regulations proposed herein would not have substantial direct effects 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, in accordance with Executive Order 12612, it is determined that this proposal would not have sufficient federalism implications to warrant the preparation of a Federalism Assessment. For the reasons discussed above, I certify that this action (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); 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 has been placed 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 part 39 of the Federal Aviation Regulations (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 (AD) to read as follows: Fairchild Aircraft, Inc.: Docket No. 99-CE-04-AD. Applicability: The following models and serial numbers, certificated in any category: ------------------------------------------------------------------------ Model Serial numbers ------------------------------------------------------------------------ SA226-T................................ T201 through T275, T277 through T291. SA226-T(B)............................. T(B)276, T(B)292 through T(B)417. SA226-AT............................... AT001 through AT069, AT071 through AT074. SA226-TC............................... TC201 through TC419. ------------------------------------------------------------------------ Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes 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 (d) 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 in the body of this AD, unless already accomplished. To prevent the main wheel brakes from overheating because of the existing brake master cylinders not totally releasing the brake hydraulic pressure and causing the brakes to drag, which could result in a wheel well area fire, loss of control of the airplane, and/or passenger injury during landing, takeoff, or taxi operations, accomplish the following: (a) Within the next 300 hours time-in-service (TIS) after the effective date of this AD, replace the existing brake master cylinders with improved design brake master cylinders as specified in the service information presented below (or FAA-approved equivalent part numbers). Accomplish this replacement in accordance with the ACCOMPLISHMENT INSTRUCTIONS section of Fairchild Service Bulletin 226-32-046, which incorporates the following pages: ------------------------------------------------------------------------ Pages Revision level and date ------------------------------------------------------------------------ 4, 5, 6, 8, 9, and 10.................. Issued: November 29, 1983. 1, 2, 3, and 7......................... Revised: March 19, 1984. ------------------------------------------------------------------------ (b) As of the effective date of this AD, no person may install, on any affected airplane, brake master cylinders that are not of improved design, part numbers as specified in the service information in paragraph (a) of this AD (or FAA-approved equivalent part numbers). (c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (d) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, FAA, Airplane Certification Office (ACO), 2601 Meacham Boulevard, Fort Worth, Texas 76193-0150. The request shall be forwarded through an appropriate FAA Maintenance Inspector, [[Page 8024]] who may add comments and then send it to the Manager, Fort Worth ACO. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Fort Worth ACO. (e) All persons affected by this directive may obtain copies of the document referred to herein upon request to Fairchild Aircraft, Inc., P.O. Box 790490, San Antonio, Texas 78279-0490; or may examine this document at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. Issued in Kansas City, Missouri, on February 9, 1999. Marvin R. Nuss, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 99-3887 Filed 2-17-99; 8:45 am] BILLING CODE 4910-13-P