98-1860. Airworthiness Directives; Cessna Aircraft Company Model 182S Airplanes  

  • [Federal Register Volume 63, Number 17 (Tuesday, January 27, 1998)]
    [Rules and Regulations]
    [Pages 3809-3811]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 98-1860]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 97-CE-151-AD; Amendment 39-10292; AD 98-01-14]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Cessna Aircraft Company Model 182S 
    Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule; request for comments.
    
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    SUMMARY: This document publishes in the Federal Register an amendment 
    adopting Airworthiness Directive (AD) 98-01-14, which was sent 
    previously to all known U.S. owners and operators of Cessna Aircraft 
    Company (Cessna) Model 182S airplanes. This AD requires replacing the 
    left and right Aeroquip engine exhaust mufflers (P/N 71379-1254017-8) 
    with an FAA-approved equivalent part. Reports of carbon monoxide gas 
    entering the cabin heating system and the cabin of the Cessna Model 
    182S airplanes prompted this action. This condition, if not corrected, 
    could result in passenger and pilot injury with consequent loss of 
    control of the airplane.
    
    DATES: Effective February 23, 1998, to all persons except those to whom 
    it was made immediately effective by priority letter AD 98-01-14, 
    issued December 30, 1997, which contained the requirements of this 
    amendment.
        Comments for inclusion in the Rules Docket must be received on or 
    before March 27, 1998.
    
    ADDRESSES: Submit comments in triplicate to the Federal Aviation 
    Administration (FAA), Central Region, Office of the Regional Counsel, 
    Attention: Rules Docket 97-CE-151-AD, Room 1558, 601 E. 12th Street, 
    Kansas City, Missouri 64106.
        Service information that applies to this AD may be obtained from 
    The Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277, 
    telephone (316) 941-7550, facsimile (316) 942-9008.
    
    FOR FURTHER INFORMATION CONTACT: Mr. Paul Pendleton, Aerospace 
    Engineer, Wichita Aircraft Certification Office, 1801 Airport Road, Rm. 
    100, Mid-Continent Airport, Wichita, Kansas 67209, telephone (316) 946-
    4128; facsimile (316) 946-4407.
    
    SUPPLEMENTARY INFORMATION:
    
    Discussion
    
        On December 30, 1997, the FAA issued priority letter AD 98-01-14, 
    which applies to Cessna 182S airplanes. Cessna Aircraft Company has 
    recently reported that a quality control problem exists with Aeroquip 
    engine exhaust mufflers installed on certain Cessna Model 182S 
    airplanes. Nineteen Cessna Model 182S airplanes are equipped with these 
    mufflers.
        The problem was discovered during a delivery flight from the 
    manufacturing facility. Following this incident, three operators have 
    reported cracked mufflers during use, and two similar failures occurred 
    at Cessna's facility during production acceptance flight tests. Cessna 
    subsequently pressure-tested the Aeroquip muffler assemblies, which 
    revealed that 7 out of 10 mufflers showed gas leak paths through 
    defective weldments.
        These inadequate or failed weldments will permit exhaust gas 
    (including carbon monoxide) leakage from the muffler, and consequently 
    into the airplane's cabin and cockpit area.
        Cessna reports that 19 of these Model 182S airplanes are directly 
    affected. The serial numbers for these models are 18280050 through 
    18280060, 18280062, 18280063, 18280066, 18280067 through 18280070, and 
    18280083. All other Cessna Model 182S airplanes were manufactured with 
    Cessna mufflers, part number (P/N) 1254017-8. After examining the 
    circumstances and reviewing all information related to the situation 
    described above, the FAA has determined that AD action should be taken 
    to prevent carbon monoxide gas from entering the airplane's cabin 
    heating system and cabin, which, if not corrected, could result in 
    passenger and pilot injury with consequent loss of control of the 
    airplane.
    
    Relevant Service Information
    
        Cessna Aircraft Company Service Bulletin No. SB97-78-01, dated
    
    [[Page 3810]]
    
    December 23, 1997, titled ``Engine Exhaust Muffler Inspection'' 
    pertains to the subject of this priority letter AD.
    
    The FAA's Determination and Explanation of the AD
    
        Since an unsafe condition (carbon monoxide leakage into the cabin 
    area) has been identified that is likely to exist or develop in other 
    Cessna Model 182S airplanes of the same type design, the FAA issued 
    priority letter AD 98-01-14 to prevent carbon monoxide gas from 
    entering the airplane's cabin heating system and cabin, which, if not 
    corrected, could result in passenger and pilot injury with consequent 
    loss of control of the airplane. The AD requires replacing the left and 
    right Aeroquip engine exhaust mufflers (P/N 71379-1254017-8) with an 
    FAA-approved equivalent part.
    
    Determination of the Effective Date of the AD
    
        Since it was found that immediate corrective action was required, 
    notice and opportunity for prior public comment thereon were 
    impracticable and contrary to the public interest, and good cause 
    existed to make the AD effective immediately by individual letters 
    issued on December 30, 1997, to all known U.S. operators of Cessna 
    Model 182S airplanes. These conditions still exist, and the AD is 
    hereby published in the Federal Register as an amendment to section 
    39.13 of the Federal Aviation Regulations (14 CFR 39.13) to make it 
    effective as to all persons.
    
    Comments Invited
    
        Although this action is in the form of a final rule that involves 
    requirements affecting immediate flight safety and, thus, was not 
    preceded by notice and opportunity to comment, comments are invited on 
    this rule. Interested persons are invited to comment on this 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, 
    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, 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 
    AD will be filed in the Rules Docket.
        Commenters wishing the FAA to acknowledge receipt of their 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. 97-CE-151-AD.'' The postcard will be date stamped and 
    returned to the commenter.
    
    Regulatory Impact
    
        The regulations adopted herein will 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 final 
    rule does not have sufficient federalism implications to warrant the 
    preparation of a Federalism Assessment.
        The FAA has determined that this regulation is an emergency 
    regulation that must be issued immediately to correct an unsafe 
    condition in aircraft, and 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.
    
    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
    
        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:
    
    98-01-14 Cessna Aircraft Company. Amendment 39-10292; Docket No. 97-
    CE-151-AD.
    
        Applicability: Model 182S airplanes (all serial numbers), 
    certificated in any category.
    
        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, except to those operators receiving this 
    action by priority letter issued December 30, 1997, which made these 
    actions effective immediately upon receipt.
        To prevent carbon monoxide gas from entering the airplane's 
    cabin heating system and cabin, which, if not corrected, could 
    result in passenger and pilot injury with consequent loss of control 
    of the airplane, accomplish the following:
        (a) For Cessna Model 182S airplanes with serial numbers 18280050 
    through 18280060, 18280062, 18280063, 18280066, 18280067 through 
    18280070, and 18280083: Prior to further flight after the effective 
    date of this AD, replace the left and right engine exhaust mufflers 
    with an FAA-approved equivalent part in accordance with the 
    appropriate Cessna maintenance manual.
        (b) For all Cessna Model 182S airplanes: After the effective 
    date of this AD, no person may install any Aeroquip engine exhaust 
    muffler, part number 71379-1254017-8, on any airplane.
    
        Note 2: Cessna Aircraft Company Service Bulletin No. SB97-78-01, 
    dated December 23, 1997, titled ``Engine Exhaust Muffler 
    Inspection'' pertains to the subject of this AD.
    
        (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, Wichita Aircraft Certification Office, 1801 
    Airport Road, Rm. 100, Mid-Continent Airport, Wichita, Kansas 67209. 
    The request shall be forwarded through an appropriate FAA 
    Maintenance Inspector, who may add comments and then send it to the 
    Manager, Wichita Aircraft Certification Office.
    
    
    [[Page 3811]]
    
    
        Note 3: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Wichita Aircraft Certification Office.
    
        (e) Copies of the relative service information may be obtained 
    from The Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 
    67277. Copies of this document also may be inspected at the FAA, 
    Central Region, Office of the Regional Counsel, Room 1558, 601 E. 
    12th Street, Kansas City, Missouri 64106.
        (f) This amendment (39-10292) becomes effective on February 23, 
    1998, to all persons except those persons to whom it was made 
    immediately effective by priority letter AD 98-01-14, issued 
    December 30, 1997, which contained the requirements of this 
    amendment.
    
        Issued in Kansas City, Missouri, on January 20, 1998.
    Carolanne L. Cabrini,
    Acting Manager, Small Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 98-1860 Filed 1-26-98; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
2/23/1998
Published:
01/27/1998
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; request for comments.
Document Number:
98-1860
Dates:
Effective February 23, 1998, to all persons except those to whom it was made immediately effective by priority letter AD 98-01-14, issued December 30, 1997, which contained the requirements of this amendment.
Pages:
3809-3811 (3 pages)
Docket Numbers:
Docket No. 97-CE-151-AD, Amendment 39-10292, AD 98-01-14
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
98-1860.pdf
CFR: (1)
14 CFR 39.13