[Federal Register Volume 61, Number 156 (Monday, August 12, 1996)] [Proposed Rules] [Pages 41753-41755] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 96-20395] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION 14 CFR Part 39 [Docket No. 96-CE-28-AD] RIN 2120-AA64 Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 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 Industrie Aeronautiche E Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. The proposed action would require replacing certain AlliedSignal Aerospace outflow/safety valves in the pressurization system with new or serviceable valves. Reports of cracking of the poppet within the primary and secondary outflow valves on two of the affected airplanes prompted the proposed action. Investigation has revealed problems during the manufacturing process of certain AlliedSignal outflow/safety valves. The actions specified by the proposed AD are intended to prevent outflow/safety valve cracking and subsequent failure, which could result in rapid decompression of the airplane. DATES: Comments must be received on or before October 7, 1996. ADDRESSES: Submit comments in triplicate to the Federal Aviation Administration (FAA), Central Region, Office of the Assistant Chief Counsel, Attention: Rules Docket No. 96-CE-28-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 AlliedSignal Aerospace, Technical Publications, Department 65-70, P.O. Box 52170, Phoenix, Arizona 85072-2170. This information also may be examined at the Rules Docket at the address above. FOR FURTHER INFORMATION CONTACT: Mr. Edward S. Chalpin, Program Manager, Brussels Aircraft Certification Office, FAA, Europe, Africa, and Middle East Office, c/o American Embassy, B-1000 Brussels, Belgium; telephone (322) 513-2717; facsimile (322) 230-6899; or Mr. Roman T. Gabrys, Project Officer, Small Airplane Directorate, Airplane Certification Service, FAA, 1201 Walnut, suite 900, Kansas City, Missouri 64105; telephone (816) 426-6932; facsimile (816) 426-2169. 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. 96-CE-28-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 Assistant Chief Counsel, Attention: Rules Docket No. 96-CE-28-AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. Discussion The Registro Aeronautico Italiano (RAI), which is the airworthiness authority for Italy, recently notified the FAA that an unsafe condition may exist on I.A.M. Model Piaggio P-180 airplanes. The RAI reports cracking of the poppet within the primary and secondary outflow/safety valves on two of the affected airplanes. Investigation has revealed problems during the manufacturing process of certain AlliedSignal Aerospace outflow/safety valves. The condition is traced to one of two lots (batch-runs) of molded poppets installed in valves during 1991. Research of these lots has revealed brittleness of these parts, which is characteristic of improper processing during injection molding. Tensile stress then develops upon installation of the poppet, which leads to hairline cracks. Small cracks have no effect, but can develop into larger cracks that cause an increase in the valve operating pressure, which could result in cabin depressurization. Applicable Service Information AlliedSignal Aerospace has issued Service Bulletin (SB) 103742-21- 4059 and SB 103744-21-4060, both dated March 31, 1995. These service bulletins specify procedures for determining whether an I.A.M. Model Piaggio P-180 airplane has one of the affected outflow/safety valves installed. The service bulletins also reference the applicable outflow/ safety valves as follows: ---------------------------------------------------------------------------------------------------------------- SB referenced in Valve model Valve serial Nos. ---------------------------------------------------------------------------------------------------------------- 103742-21-4059......................... 103742-ALL................ 21-121 through 21-131; 21-133 through 21- 136; 21-138 through 21-140; 59-105; 79-116 through 79-119; 95-101; and 95-102. [[Page 41754]] 103744-21-4060......................... 103744-ALL................ 40-120; 40-126; 40-129; 40-131 through 40- 134; 41-136; 41-137; 41-139; 59-105; 59- 108; and 59-111. ---------------------------------------------------------------------------------------------------------------- I.A.M. Rinaldo Piaggio SB No. 80-0084, dated July 7, 1995, references the above AlliedSignal Aerospace service bulletins. The RAI classified these service bulletins as mandatory and issued RAI AD 95-224, dated August 22, 1995, in order to assure the continued airworthiness of these airplanes in Italy. Evaluation of All Applicable Information This airplane model is manufactured in Italy and is type certificated for operation in the United States under the provisions of section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and the applicable bilateral airworthiness agreement. Pursuant to this bilateral airworthiness agreement, the RAI has kept the FAA informed of the situation described above. The FAA has examined the findings of the RAI; reviewed all available information, including the service information referenced above; and determined that AD action is necessary for products of this type design that are certificated for operation in the United States. Explanation of the Provisions of the Proposed AD Since an unsafe condition has been identified that is likely to exist or develop in other I.A.M. Model Piaggio P-180 airplanes of the same type design that are registered in the United States and have an AlliedSignal Aerospace outflow/safety valve (referenced above in the discussion of the service information) installed, the proposed AD would require replacing outflow/safety valves with new or serviceable valves. Accomplishment of the proposed replacement would be in accordance with the applicable maintenance or service manual. Compliance Time of the Proposed AD The FAA has determined that an interval of three calendar months is an appropriate compliance time to address the identified unsafe condition in a timely manner. This compliance time was deemed appropriate after considering the safety implications, the average utilization rate of the affected fleet, and the availability of the replacement parts. Cost Impact The FAA estimates that 3 airplanes in the U.S. registry would be affected by the proposed AD, that it would take approximately 32 workhours per airplane to accomplish the proposed action, and that the average labor rate is approximately $60 an hour. AlliedSignal will provide parts at no cost to the owner/operator. Based on these figures, the total cost impact of the proposed AD on U.S. operators is estimated to be $5,760 or $1,920 per airplane. The FAA knows of no affected airplane owner/operator (of the 3 affected) that has already accomplished the proposed action. 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 USC 106(g), 40101, 40113, 44701. Sec. 39.13 [Amended] 2. Section 39.13 is amended by adding a new airworthiness directive (AD) to read as follows: Industrie Aeronautiche E Mecchaniche: Docket No. 96-CE-28-AD. Applicability: Model Piaggio P-180 airplanes (all serial numbers), certificated in any category, that have one of the following AlliedSignal Aerospace outflow safety valves installed, as referenced in either AlliedSignal Aerospace Service Bulletin (SB) 103742-21-4059 or SB 103744-21-4060, both dated March 31, 1995: ------------------------------------------------------------------------ SB Referenced in Valve model Valve serial Nos. ------------------------------------------------------------------------ 103742-21-4059................ 103742-ALL....... 21-121 through 21- 131; 21-133 through 21-136; 21-138 through 21-140; 59- 105; 79-116 through 79-119; 95-101; and 95-102. 103744-21-4060................ 103744-ALL....... 40-120; 40-126; 40- 129; 40-131 through 40-134; 41-136 41- 137; 41-139; 59-105; 59-108; and 59-111. ------------------------------------------------------------------------ Note 1: The above AlliedSignal Aerospace service bulletins are referenced in I.A.M. Rinaldo Piaggio SB No. 80-0084, dated July 7, 1995. Note 2: 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 [[Page 41755]] this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it. Compliance: Required within the next three calendar months after the effective date of this AD, unless already accomplished. To prevent outflow/safety valve cracking and subsequent failure, which could result in rapid decompression of the airplane, accomplish the following: (a) Replace (with a new or serviceable valve) any outflow/safety valve that does not have one of the following: (1) The valve identification plate MOD RECORD stamped ``PCA'' (Poppet Change Accomplished); or (2) A valve with an inked ATD Quality Assurance ``Functional Test (FT)'' stamp that is dated June 1992, or later. (b) As of the effective date of this AD, no outflow/safety valve that is referenced in the ``Applicability'' section of this AD may be installed on an affected airplane. (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, Brussels Aircraft Certification Office (ACO), FAA, Europe, Africa, and Middle East Office, c/o American Embassy, B-1000 Brussels, Belgium. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Brussels ACO. Note 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Brussels ACO. (e) All persons affected by this directive may obtain copies of the documents referred to herein upon request to AlliedSignal Aerospace, Technical Publications, Department 65-70, P.O. Box 52170, Phoenix, Arizona 85072-2170; or may examine these documents at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. Issued in Kansas City, Missouri, on August 5, 1996. Henry A. Armstrong, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 96-20395 Filed 8-9-96; 8:45 am] BILLING CODE 4910-13-U