99-17552. Airworthiness Directives; Overland Aviation Services Fire Extinguishing System Bottle Cartridges  

  • [Federal Register Volume 64, Number 132 (Monday, July 12, 1999)]
    [Proposed Rules]
    [Pages 37471-37473]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-17552]
    
    
    
    [[Page 37471]]
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-CE-113-AD]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Overland Aviation Services Fire 
    Extinguishing System Bottle Cartridges
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Notice of proposed rulemaking (NPRM).
    
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    SUMMARY: This document proposes to adopt a new airworthiness directive 
    (AD) that would apply to certain Overland Aviation Services fire 
    extinguishing system bottle cartridges that were distributed during a 
    certain time period. The proposed AD would require removing from 
    service any of these fire extinguishing system bottle cartridges. The 
    proposed AD is the result of several incidents where the fire 
    extinguishing system bottle cartridges activated with excessive 
    energetic force. In one instance, the discharge valve outlet screen 
    fractured and the screen material went through the distribution 
    manifold. The actions specified by the proposed AD are intended to 
    prevent damage to fire extinguishing system components caused by a fire 
    extinguishing system bottle cartridge activating with excessive 
    energetic force, which could result in the fire extinguishing system 
    operating improperly.
    
    DATES: Comments must be received on or before September 3, 1999.
    
    ADDRESSES: Submit comments in triplicate to the Federal Aviation 
    Administration (FAA), Central Region, Office of the Regional Counsel, 
    Attention: Rules Docket No. 98-CE-113-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 Overland Aviation Services, 10271 Bach Boulevard, St. Louis, 
    Missouri; telephone: (314) 428-2062; facsimile: (314) 428-3403. This 
    information also may be examined at the Rules Docket at the address 
    above.
    
    FOR FURTHER INFORMATION CONTACT: Jeffrey D. Janusz, Aerospace Engineer, 
    FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Mid-
    Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-4148; 
    facsimile: (316) 946-4407.
    
    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. 98-CE-113-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. 98-CE-113-AD, Room 1558, 601 E. 12th Street, Kansas 
    City, Missouri 64106.
    
    Discussion
    
        The FAA has received reports of several incidents where fire 
    extinguishing system bottle cartridges that were manufactured by 
    Overland Aviation Services activated with excessive energetic force. In 
    one instance, the discharge valve outlet screen fractured and the 
    screen material went through the distribution manifold.
        The fire extinguishing system bottle cartridges are considered 
    critical parts. The fire extinguishing system is only required to 
    function after a failure or series of failures have occurred and 
    developed into the potential for a fire. In the above-referenced 
    incidents, the fire extinguishing system could not be relied on because 
    of the potential for damage to the fire extinguishing system components 
    that could result from a cartridge activating with excessive energetic 
    force. Overland Aviation Services distributed fire extinguishing system 
    bottle cartridges that could incorporate this problem from April 1, 
    1996, through September 15, 1997.
    
    Relevant Service Information
    
        Overland Aviation Services issued Service Bulletin 22-09-97, not 
    dated, which contains information pertaining to the above-referenced 
    condition.
    
    The FAA's Determination
    
        After examining the circumstances and reviewing all available 
    information related to the incidents described above, the FAA has 
    determined that AD action should be taken to prevent damage to fire 
    extinguishing system components caused by a fire extinguishing system 
    bottle cartridge activating with excessive energetic force, which could 
    result in the fire extinguishing system operating improperly.
    
    Explanation of the Provisions of the Proposed AD
    
        Since an unsafe condition has been identified that is likely to 
    exist or develop in Overland Aviation Services fire extinguishing 
    system bottle cartridges that were distributed from April 1, 1996, 
    through September 15, 1997, the FAA is proposing AD action. The 
    proposed AD would require removing from service any of these fire 
    extinguishing system bottle cartridges.
    
    Compliance Time of the Proposed AD
    
        The unsafe condition described in this proposed AD is not a direct 
    result of aircraft operation. The fire extinguishing system bottle 
    cartridges could activate with excessive energetic force the first time 
    they are used during flight. This could occur on an aircraft with 50 
    hours time-in-service (TIS) or an aircraft with 10,000 hours TIS. 
    Therefore, to assure that the unsafe condition is corrected in a timely 
    manner, the proposed AD is utilizing a compliance time of 120 days 
    after the effective date of the AD.
    
    Cost Impact
    
        The FAA estimates that 5,128 fire extinguishing system bottle 
    cartridges would be affected by the proposed AD, that it would take 
    approximately 8 workhours per cartridge to accomplish the proposed 
    action, and that the average labor rate is approximately $60 an hour. 
    Warranty credit from Overland Aviation Services will cover the cost of 
    replacement cartridges. Based on these
    
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    figures, the total cost impact of the proposed AD on U.S. operators is 
    estimated to be $2,461,440, or $480 per fire extinguishing system 
    bottle cartridge.
        Overland Aviation Services reports that 2,100 parts have been 
    removed from service. This reduces the cost impact of the proposed AD 
    from $2,504,640, to $1,453,440.
        The number of cartridges utilized varies from airplane to airplane. 
    The FAA has no way of determining which airplanes have the affected 
    fire extinguishing system bottle cartridges incorporated. Therefore, 
    the FAA has presented the cost impact of the proposed AD based upon the 
    number of fire extinguishing system bottle cartridges manufactured 
    instead of the number of airplanes affected.
    
    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:
    
    Overland Aviation Services: Docket No. 98-CE-113-AD.
    
        Applicability: The fire extinguishing system bottle cartridges 
    presented below that were distributed from April 1, 1996, through 
    September 15, 1997, and are installed on, but not limited to the 
    following aircraft:
    
    ----------------------------------------------------------------------------------------------------------------
                                      Walter Aerospace (WKA)
                                        fire extinguishing
    Overland Aviation Services (OAS)   system (Firex) bottle      Make/model of             Cartridge lot No.
           cartridge part Nos.          assembly basic part    applicable aircraft
                                                No.
    ----------------------------------------------------------------------------------------------------------------
    OA47200.........................  472073, 472420,         Aerospatiale ATR72     SBI 1-1
                                       472467, 897885,         Series ATR42-200, -   SBI 1-2
                                       897878, 899170.         300, - 320.
                                                              Embraer EMB-120
                                                               Series.
    OA841155........................  898768, 890532,         Boeing 707-100, -100B  SBI 1-3
                                       890598, 890599,         Series, -300 Series,  OAS 1-2
                                       891070, 891147,         720B.
                                       891814, 893675,        McDonnell Douglas DC-
                                       892308.                 8, -8F Series.
                                                              Lockheed 382, 382E,
                                                               382F, 382G.
                                                              Sabreliner NA-265
                                                               Series.
                                                              Bell 204B.
    OA873364........................  893523, 893524,         Gulfstream G-1159, G-  SBI 1-3
                                       893456, 893726,         1159B, G-1159A.
                                       472049, 472162,        Cessna 425, 441, 550,
                                       895353, 894703,         S550, 551, 552.
                                       472389, 472390,        Fokker F.28 Series.
                                       893572, 897770,
                                       898066, 898006.
                                                              SAAB 340 Series.
                                                              Bell 412.
    OA873571........................  893244, 899827,         Boeing 707-100, -100B  SBI 2-2
                                       899927, 892807,         Series, -300 Series,
                                       892857.                 720B.
                                                              McDonnell Douglas DC-
                                                               8, -8F Series, DC-9
                                                               Series.
                                                              Lockheed 382, 382E,
                                                               382F, 382G.
    OA876296........................  895240, 895678,         McDonnell Douglas DC-  SBI 1-1
                                       895683, 895564,         9-81, DC-9-82, DC-9-  OAS 1-1
                                       898150, 472603,         83, DC-10 Series.
                                       472602, 473598,        Airbus A300 Series.
                                       896054, 895877.
    OA876299........................  895656, 895752,         Lockheed L-1011        SBI 1-1
                                       895848, 897785,         Series.
                                       897797, 897798,
                                       472268, 896166,
                                       896165.
    OA897776........................  897869, 899486,         Canadair CL-600-1A11,  SBI 1-4
                                       897899, 897885,         CL-600-2A12, CL-600-  SBI 1-15
                                       899170, 472258,         2B16.                  SBI 1-16
                                       472428, 899074,        Embraer EMB-120, EMB-  OAS 1-1
                                       897775, 899066.         120RT
                                                              Sikorsky S-76A
                                                              SAAB 340 Series
    ----------------------------------------------------------------------------------------------------------------
    
        Note 1: Overland Aviation Services distributed the affected fire 
    extinguishing system bottle cartridges from April 1, 1996, through 
    September 15, 1997. Those cartridges incorporated on the aircraft 
    prior to April 1, 1996, would not be affected by this AD. This AD 
    allows the aircraft owner or pilot to check the maintenance records 
    to determine whether the fire extinguishing system bottle cartridges 
    were installed since April 1, 1996. See paragraph (d) of this AD for 
    authorization.
        Note 2: Procurement records may show if the owner/operator has 
    ever bought affected parts, for spares or time replacements, for 
    airplane installation, or to support a repair shop. These could be 
    cross-referenced to the lots that are suspect. Additionally, a 
    review of procurement records with respect to the part number, lot 
    number, and distribution date of the suspect lots would also reduce 
    the
    
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    owners'/operators' workload of having to examine all applicable Air 
    Transport Association (ATA) codes in the databases. A search of the 
    maintenance/inspection records and logbooks of a specific airplane 
    make and model and serial number could be beneficial.
        Note 3: The fire extinguishing system parts are installed up to 
    a hex wrenching flat on the cartridge body. These wrenching flats 
    have the part number, lot number, and date of manufacture stamped on 
    them, as well as safety wire holes. When installed, the safety wire 
    will probably cover up at least one bit of the above information. 
    Inspecting the wrenching flats could help determine whether the fire 
    extinguishing system bottle cartridges contain an affected part 
    number or lot number.
        Note 4: This AD applies to each aircraft that incorporates one 
    of the fire extinguishing system bottle cartridges identified in the 
    preceding applicability provision, regardless of whether the 
    aircraft has been modified, altered, or repaired in the area subject 
    to the requirements of this AD. For aircraft 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 (f) 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.
    
        Note 5: ``Unless already accomplished'' credit may be extended 
    to the records check allowed by this AD provided that the records 
    are checked to cover any time period that has elapsed since the 
    previous check.
    
        To prevent damage to fire extinguishing system components caused 
    by a fire extinguishing system bottle cartridge activating with 
    excessive energetic force, which could result in the fire 
    extinguishing system operating improperly, accomplish the following:
        (a) Within the next 120 calendar days after the effective date 
    of this AD, remove from service any fire extinguishing system bottle 
    cartridge referenced in the Applicability section of this AD, and 
    replace it with an FAA-approved fire extinguishing system bottle 
    cartridge that is not of the affected part numbers.
        (b) As of the effective date of this AD, no person shall 
    install, on any aircraft, any affected Overland Aviation Services 
    fire extinguishing system bottle cartridge that was distributed from 
    April 1, 1996, through September 15, 1997.
        (c) The FAA requests that any fire extinguishing system bottle 
    cartridge removed from service that has not been fired or cartridges 
    that are held in inventory be sent to the manufacturer for analysis. 
    Contact Jeff Janusz, Aerospace Engineer, at the FAA,Wichita Aircraft 
    Certification Office (ACO), for shipping instructions; telephone: 
    (316) 946-4148; e:mail: jeff.janusz@faa.gov. 
        (d) The owner/operator holding at least a private pilot 
    certificate as authorized by section 43.7 of the Federal Aviation 
    Regulations (14 CFR 43.7) may check the maintenance records to 
    determine whether any of the affected fire extinguishing system 
    bottle cartridges were installed since April 1, 1996. If an affected 
    fire extinguishing system bottle cartridge was installed prior to 
    April 1, 1996, the AD does not apply and the owner/operator must 
    make an entry into the aircraft records showing compliance with this 
    AD in accordance with section 43.9 of the Federal Aviation 
    Regulations (14 CFR 43.9).
        (e) 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.
        (f) An alternative method of compliance or adjustment of the 
    compliance times that provides an equivalent level of safety may be 
    approved by the Manager, Wichita ACO, 1801 Airport Road, Room 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 ACO.
    
        Note 6: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Wichita ACO.
    
        (g) All persons affected by this directive may obtain copies of 
    the documents referred to herein upon request to Overland Aviation 
    Services, 10271 Bach Boulevard, St. Louis, Missouri; or may examine 
    these documents 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 July 2, 1999.
    Marvin R. Nuss,
    Acting Manager, Small Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-17552 Filed 7-9-99; 8:45 am]
    BILLING CODE 4910-13-P
    
    
    

Document Information

Published:
07/12/1999
Department:
Federal Aviation Administration
Entry Type:
Proposed Rule
Action:
Notice of proposed rulemaking (NPRM).
Document Number:
99-17552
Dates:
Comments must be received on or before September 3, 1999.
Pages:
37471-37473 (3 pages)
Docket Numbers:
Docket No. 98-CE-113-AD
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-17552.pdf
CFR: (1)
14 CFR 39.13