99-3189. Airworthiness Directives; Transport Category Airplanes Equipped With Day-Ray Products, Inc., Fluorescent Light Ballasts  

  • [Federal Register Volume 64, Number 28 (Thursday, February 11, 1999)]
    [Rules and Regulations]
    [Pages 6788-6791]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-3189]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 96-NM-163-AD; Amendment 39-11034; AD 99-04-10]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Transport Category Airplanes Equipped 
    With Day-Ray Products, Inc., Fluorescent Light Ballasts
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
    -----------------------------------------------------------------------
    
    SUMMARY: This amendment adopts a new airworthiness directive (AD), 
    applicable to any transport category airplane that is equipped with 
    certain Day-Ray fluorescent light ballasts installed in the upper and/
    or lower cabin sidewall, that requires a visual inspection to determine 
    the type of fluorescent light ballasts installed in the cabin sidewall, 
    and the replacement of suspect ballasts with new or serviceable 
    ballasts. This amendment is prompted by reports of smoke, fumes, and/or 
    electrical fire emitting from the baggage bin of the aft passenger 
    compartment due to the failure of the fluorescent light ballasts. The 
    actions specified by this AD are intended to prevent fire in the 
    passenger compartment resulting from failure of the fluorescent light 
    ballast of the cabin sidewall.
    
    DATES: Effective March 18, 1999.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of March 18, 1999.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from Day-Ray Products, Inc., 1133 Mission Street, South 
    Pasadena, California 91031; or Hexcel Corporation, Heath Tecna 
    Interiors, 3225 Woburn Street, Bellingham, Washington 98226; or The 
    Boeing Company, Douglas Products Division, 3855 Lakewood Boulevard, 
    Long Beach, California 90846, Attention: Technical Publications 
    Business Administration, Department C1-L51 (2-60); or Boeing Commercial 
    Airplane Group, P.O. Box 3707, Seattle, Washington 98124-2207. This 
    information may be examined at the Federal Aviation Administration 
    (FAA), Transport Airplane Directorate, Rules Docket, 1601 Lind Avenue, 
    SW., Renton, Washington; or at the FAA, Transport Airplane Directorate, 
    Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, 
    Lakewood, California; or at the Office of the Federal Register, 800 
    North Capitol Street, NW., suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: J. Kirk Baker, Aerospace Engineer, 
    Systems and Equipment Branch, ANM-130L, FAA, Los Angeles Aircraft 
    Certification Office, 3960 Paramount Boulevard, Lakewood, California 
    90712; telephone (310) 627-5345; fax (310) 627-5210.
    
    SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal 
    Aviation Regulations (14 CFR part 39) to include an airworthiness 
    directive (AD) that is applicable to any transport category airplane 
    that is equipped with certain Day-Ray fluorescent light ballasts 
    installed in the upper and/or lower cabin sidewall was published as a 
    supplemental notice of proposed rulemaking (NPRM) in the Federal 
    Register on February 19, 1998 (63 FR 8374). That action proposed to 
    require a visual inspection to determine the type of fluorescent light 
    ballasts installed in the cabin sidewall, and the replacement of 
    suspect ballasts with new or serviceable ballasts.
    
    Comments
    
        Interested persons have been afforded an opportunity to participate 
    in the making of this amendment. Due consideration has been given to 
    the comments received.
    
    Support for the Proposal
    
        Several commenters support the proposed rule.
    
    Request To Revise Cost Impact Information
    
        One commenter states that, based on prior experience with replacing 
    the light ballasts on its airplanes, the work hours necessary to 
    accomplish the proposed replacement is greater than the estimate of 50 
    work hours per airplane, and the parts cost is greater than the 
    estimate of $8,550 per airplane (which were the estimates provided in 
    the proposed rule). The FAA infers that the commenter is requesting 
    that the estimates for the work hours and parts cost specified in the 
    cost impact information of the proposed rule be revised upward in the 
    final rule.
        The FAA does not concur with the commenter's request to revise the 
    cost impact information. As stated in the supplemental NPRM, the FAA 
    used an average of $150 per ballast parts cost and 57 light ballasts 
    per airplane to estimate the cost impact of the proposal. Also, the 
    estimate of 50 work hours necessary for the replacement is based on the 
    estimated average number of 57 ballasts per airplane. The FAA 
    recognizes that actual per-airplane costs will vary, because different 
    airplane models have different numbers of ballasts, and the cost of 
    parts and the number of work hours necessary to install those parts are 
    different for different airplane models. Also, because this final rule 
    is applicable to all transport category airplanes that are equipped 
    with Day-Ray fluorescent light ballasts having certain part numbers, 
    and is not limited to specific airplane models, it is not possible for 
    the FAA to provide precise cost estimates for all affected airplanes. 
    For these reasons, the FAA finds that no change to the cost impact 
    information stated in the final rule is necessary.
    
    Request To Remove Airplanes From Applicability
    
        Several commenters request that McDonnell Douglas DC-9-80 series 
    airplanes and MD-88 airplanes be excluded from the applicability of the 
    proposed rule. The commenters state that AD 97-08-07, amendment 39-9995 
    (62 FR 28798, May 28, 1997), already requires the removal and 
    replacement of Day-Ray ballasts from those airplanes.
        The FAA concurs with the commenters' request to remove McDonnell 
    Douglas DC-9-80 series airplanes and MD-88 airplanes from the 
    applicability of this AD. The FAA finds that these airplanes are 
    subject to the requirements of AD 97-08-07. Therefore, the 
    applicability statement of this final rule has been revised to 
    eliminate reference to McDonnell Douglas DC-9-80 series airplanes and 
    MD-88 airplanes. Also, Table 2 of this final rule has been revised to 
    remove two service bulletins that were listed in the proposed rule as 
    appropriate sources of service information for the
    
    [[Page 6789]]
    
    replacement of light ballasts on McDonnell Douglas DC-9-80 series 
    airplanes and MD-88 airplanes.
    
    Request To Reference New Service Information
    
        One commenter requests that the supplemental NPRM be revised to 
    reference McDonnell Douglas Service Bulletin DC9-33-111, dated May 6, 
    1997, in lieu of McDonnell Douglas Service Bulletin DC9-33-103, dated 
    May 30, 1996, which was cited in the supplemental NPRM as the 
    appropriate source of service information for accomplishment of certain 
    proposed actions. The commenter notes that McDonnell Douglas Service 
    Bulletin DC9-33-103 provides an option to install a protective cover 
    over the subject light ballast; however, the FAA issued the 
    supplemental NPRM to eliminate the option to install such protective 
    covers. The commenter states that the effectivity listing is the same 
    in both service bulletins.
        The FAA partially concurs with the commenter's request. The FAA has 
    reviewed and approved McDonnell Douglas Service Bulletin DC9-33-111, 
    and has determined that, for McDonnell Douglas Model DC-9-30, -40, and 
    -50 series airplanes, replacement of existing Day-Ray light ballasts 
    with new or serviceable light ballasts in accordance with that service 
    bulletin is an acceptable method of compliance for the requirements of 
    this AD.
        However, the FAA's intent is that McDonnell Douglas Service 
    Bulletin DC9-33-103 is an acceptable source of service information for 
    accomplishment of the requirements of paragraph (a) of this AD, 
    provided that no protective covers are installed. Therefore, Table 2 of 
    the final rule has been revised to add McDonnell Douglas Service 
    Bulletin DC9-33-111 as an acceptable source of service information for 
    accomplishment of the requirements of this AD. In addition, NOTE 2 has 
    been added to the final rule to specify that, ``Replacement of light 
    ballasts on McDonnell Douglas Model DC-9-30, -40, and -50 series 
    airplanes; in accordance with McDonnell Douglas Service Bulletin DC9-
    33-103, dated May 30, 1996; is acceptable for compliance with the 
    requirements of paragraph (a) of this AD, provided that no protective 
    covers are installed on the light ballasts.''
    
    Request To Allow Records Search in Lieu of Inspection
    
        One commenter requests that the FAA allow operators to search their 
    airplane records to determine if suspect ballasts are installed, in 
    lieu of performing the inspection specified in paragraph (a) of the 
    supplemental NPRM. The commenter provides no justification for its 
    request.
        The FAA does not concur with the commenter's request to allow a 
    records search in lieu of the inspection. The FAA finds that, although 
    some operators' records may be excellent, a records search may not 
    provide an adequate level of safety assurance for all airplanes in the 
    transport fleet. No change to the final rule is necessary in this 
    regard.
    
    Request To Extend Compliance Time
    
        Two commenters request that the compliance time for the replacement 
    of suspect ballasts be extended beyond the proposed 12 months to allow 
    accomplishment of the replacement during regularly scheduled ``C'' 
    checks. One of the commenters notes that there has not been a single 
    incident of a fire on McDonnell Douglas DC-10 series airplanes that was 
    attributed to the subject light ballast.
        The FAA does not concur with the commenters' request to extend the 
    compliance time. The FAA has considered the severity of the unsafe 
    condition (fire in the passenger compartment resulting from failure of 
    the fluorescent light ballast of the cabin sidewall) and has determined 
    that 12 months after the effective date of this AD represents an 
    appropriate compliance time to ensure the safety of the transport 
    airplane fleet. The FAA also has determined that a sufficient supply of 
    parts is available to allow for accomplishment of the replacement 
    within that timeframe. No change to the final rule is necessary in this 
    regard. However, under the provisions of paragraph (c) of this final 
    rule, the FAA may approve requests for adjustment of the compliance 
    time in cases where the operator presents evidence that an alternate 
    method of compliance would provide an acceptable level of safety.
    
    Request To Allow Use of Alternative Type of Replacement Ballast
    
        One commenter requests that the FAA allow a new type of replacement 
    ballast, manufactured by Day-Ray, to be installed as an alternative to 
    the light ballasts manufactured by Bruce Industries that were specified 
    in paragraph (a) of the supplemental NPRM. The commenter states that it 
    anticipates FAA approval of the design prior to issuance of the final 
    rule.
        The FAA does not concur with the commenter's request to approve the 
    use of a new Day-Ray ballast. The new replacement ballast to which the 
    commenter refers has not been approved as of the issuance of this final 
    rule, and the FAA cannot approve the installation of a particular part 
    prior to design approval of that part. Furthermore, the FAA finds that 
    to delay this rulemaking action would be inappropriate in light of the 
    identified unsafe condition. However, once a new ballast has been 
    approved, under the provisions of paragraph (c) of this final rule, the 
    FAA may approve requests for an alternative method of compliance to 
    allow use of such a new ballast. No change to the final rule is 
    necessary in this regard.
    
    Conclusion
    
        After careful review of the available data, including the comments 
    noted above, the FAA has determined that air safety and the public 
    interest require the adoption of the rule with the changes described 
    previously. The FAA has determined that these changes will neither 
    increase the economic burden on any operator nor increase the scope of 
    the AD.
    
    Cost Impact
    
        There are approximately 2,500 transport category airplanes of the 
    affected design in the worldwide fleet. The FAA estimates that 1,800 
    airplanes of U.S. registry will be affected by this AD.
        It will take approximately 25 work hours per airplane to accomplish 
    the required inspection, at an average labor rate of $60 per work hour. 
    Based on these figures, the cost impact of the AD on U.S. operators is 
    estimated to be $1,500 per airplane.
        Should an operator be required to accomplish the replacement of the 
    light ballasts, it will require approximately 50 work hours per 
    airplane, at an average labor rate of $60 per work hour. Required parts 
    will average approximately $8,550 per airplane, which represents a cost 
    of $150 per ballast and an average of 57 ballasts per airplane. Based 
    on these figures, the cost impact of the replacement required by this 
    AD on U.S. operators is estimated to be $11,550 per airplane.
        The cost impact figures discussed above are based on assumptions 
    that no operator has yet accomplished any of the requirements of this 
    AD action, and that no operator would accomplish those actions in the 
    future if this AD were not adopted.
    
    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
    
    [[Page 6790]]
    
    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.
        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) 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 final evaluation has been prepared for this action 
    and it is contained in the Rules Docket. A copy of it 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
    
        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 the following new 
    airworthiness directive:
    
    99-04-10 Transport Category Airplanes: Amendment 39-11034. Docket 
    96-NM-163-AD.
    
        Applicability: Airplanes equipped with Day-Ray Products, Inc., 
    cabin sidewall fluorescent light ballasts having part numbers listed 
    in Table 1 of this AD; including, but not limited to, McDonnell 
    Douglas Model DC-9, DC-10, and C-9 (military) series airplanes; and 
    Boeing Model 707, 727, and 737 series airplanes; certificated in any 
    category.
    
             Table 1.--Fluorescent Light Ballasts Subject to this AD
    ------------------------------------------------------------------------
                        Name                               Part No.
    ------------------------------------------------------------------------
    Day-Ray....................................  69-10
                                                 69-10-1
                                                 69-68
                                                 69-68-1
                                                 69-69
                                                 69-69-1
                                                 70-94
                                                 70-94-1
                                                 83-12
                                                 83-12-1
    ------------------------------------------------------------------------
    
        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 (c) 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, unless accomplished 
    previously.
        To prevent fire in the passenger compartment resulting from 
    failure of the fluorescent light ballast of the cabin sidewall, 
    accomplish the following:
        (a) Within 12 months after the effective date of this AD, 
    perform a one-time visual inspection to determine the type of 
    fluorescent light ballasts installed in the upper and lower cabin 
    sidewall. If any ballast installed has a part number that is listed 
    in Table 1 of this AD, prior to further flight, remove the Day-Ray 
    light ballast and replace it with a light ballast manufactured by 
    Bruce Industries, in accordance with the applicable service 
    bulletin(s) listed in Table 2 of this AD.
    
      Table 2.--Service Bulletins Containing Instructions for Accomplishing
                           the Requirements of this AD
    ------------------------------------------------------------------------
        Service bulletin number and date            Affected airplanes
    ------------------------------------------------------------------------
    McDonnell Douglas, DC-9 Service          Model DC-9-30, -40, and -50
     Bulletin DC9-33-103, May 30, 1996.       series airplanes listed in
                                              effectivity of service
                                              bulletin.
    McDonnell Douglas, DC-9 Service           Model DC-9-30, -40, and -50
     Bulletin DC9-33-111, May 6, 1997.        series airplanes listed in
                                              effectivity of service
                                              bulletin.
    McDonnell Douglas, DC-10 Service         Model DC-10-10, -15, -30, and -
     Bulletin DC10-33-073, June 18, 1996.     40 series airplanes and KC-10A
                                              airplanes listed in
                                              effectivity of service
                                              bulletin.
    Heath Tecna, Alert Service Bulletin      McDonnell Douglas Model DC-8
     MarkI-33-A2, Revision 1, July 24, 1996.  series airplanes retrofitted
                                              with Heath Tecna Mark I
                                              interior.
    Heath Tecna, Alert Service Bulletin      Boeing Model 707 series
     MarkI-33-A3, Revision 1, July 24, 1996.  airplanes retrofitted with the
                                              Heath Tecna Mark I interior.
    Heath Tecna, Alert Service Bulletin      Boeing Model 727 series
     MarkI-33-A4, Revision 1, July 24, 1996.  airplanes retrofitted with the
                                              Heath Tecna Mark I interior.
    Heath Tecna, Alert Service Bulletin      Boeing Model 737 series
     MarkI-33-A5, Revision 1, July 24, 1996.  airplanes retrofitted with the
                                              Heath Tecna Mark I interior.
    Heath Tecna, Alert Service Bulletin      Boeing Model 727 series
     Spmk-33-A1, Revision 1, July 24, 1996.   airplanes, retrofitted with
                                              the Heath Tecna Spacemaker II
                                              or Spacemaker IIa interior.
    Heath Tecna, Alert Service Bulletin      Boeing Model 737 series
     Spmk-33-A2, Revision 1, July 24, 1996.   airplanes, retrofitted with
                                              the Heath Tecna Spacemaker II
                                              or Spacemaker IIa interior.
    ------------------------------------------------------------------------
    
        Note 2: Replacement of light ballasts on McDonnell Douglas Model 
    DC-9-30, -40, and -50 series airplanes; in accordance with McDonnell 
    Douglas Service Bulletin DC9-33-103, dated May 30, 1996; is 
    acceptable for compliance with the requirements of paragraph (a) of 
    this AD, provided that no protective covers are installed on the 
    light ballasts.
    
        (b) As of the effective date of this AD, no person shall install 
    in the upper or lower cabin sidewall of any airplane a Day-Ray 
    fluorescent light ballast having a part number listed in Table 1 of 
    this AD.
        (c) 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, Los Angeles Aircraft Certification 
    Office (ACO), FAA, Transport Airplane Directorate. Operators shall 
    submit their requests through an appropriate FAA Principal 
    Maintenance
    
    [[Page 6791]]
    
    Inspector, who may add comments and then send it to the Manager, Los 
    Angeles ACO.
    
        Note 3: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Los Angeles ACO.
    
        (d) Special flight permits may be issued in accordance with 
    Secs. 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.
        (e) The replacement shall be done in accordance with the 
    following McDonnell Douglas and Heath Tecna service bulletins, as 
    applicable, which contain the specified list of effective pages:
    
    ----------------------------------------------------------------------------------------------------------------
     Service bulletin referenced and                               Revision level shown on
                   date                         Page No.                    page               Date shown on page
    ----------------------------------------------------------------------------------------------------------------
    McDonnell Douglas, DC9-33-103,     1-10.....................  Original................  May 30, 1996.
     May 30, 1996.
    McDonnell Douglas, DC9-33-111,     1-10.....................  Original................  May 6, 1997.
     May 6, 1997.
    McDonnell Douglas, DC10-33-073,    1-9......................  Original................  June 18, 1996.
     June 18, 1996.
    Heath Tecna, Alert Service         1-3,5....................  New.....................  April 3, 1996.
     Bulletin, MarkI-33-A2, Revision   4........................  1.......................  July 24, 1996.
     1, July 24, 1996.
    Heath Tecna, Alert Service         1-2......................  New.....................  April 4, 1996.
     Bulletin, MarkI-33-A3, Revision   3-4......................  1.......................  July 24, 1996.
     1, July 24, 1996.
    Heath Tecna, Alert Service         1-2......................  New.....................  April 8, 1996.
     Bulletin, MarkI-33-A4, Revision   3-4......................  1.......................  July 24, 1996.
     1, July 24, 1996.
    Heath Tecna, Alert Service         1-2......................  New.....................  April 9, 1996.
     Bulletin, MarkI-33-A5, Revision   3-4......................  1.......................  July 24, 1996.
     1, July 24, 1996.
    Heath Tecna, Alert Service         1-2......................  New.....................  April 10, 1996.
     Bulletin, Spmk-33-A1, Revision    3-4......................  1.......................   July 24, 1996.
     1, July 24, 1996.
    Heath Tecna, Alert Service         1-2......................  New.....................  April 11, 1996.
     Bulletin, Spmk-33-A2, Revision    3-4......................  1.......................  July 24, 1996.
     1, July 24, 1996.
    ----------------------------------------------------------------------------------------------------------------
    
    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 Day-Ray Products, Inc., 1133 Mission 
    Street, South Pasadena, California 91031; or Hexcel Corporation, 
    Heath Tecna Interiors, 3225 Woburn Street, Bellingham, Washington 
    98226; or The Boeing Company, Douglas Products Division, 3855 
    Lakewood Boulevard, Long Beach, California 90846, Attention: 
    Technical Publications Business Administration, Department C1-L51 
    (2-60); or Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, 
    Washington 98124-2207. Copies may be inspected at the FAA, Transport 
    Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 
    at the FAA, Transport Airplane Directorate, Los Angeles Aircraft 
    Certification Office, 3960 Paramount Boulevard, Lakewood, 
    California; or at the Office of the Federal Register, 800 North 
    Capitol Street, NW., suite 700, Washington, DC.
        (f) This amendment becomes effective on March 18, 1999.
    
        Issued in Renton, Washington, on February 4, 1999.
    John J. Hickey,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-3189 Filed 2-10-99; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
3/18/1999
Published:
02/11/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
99-3189
Dates:
Effective March 18, 1999.
Pages:
6788-6791 (4 pages)
Docket Numbers:
Docket No. 96-NM-163-AD, Amendment 39-11034, AD 99-04-10
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-3189.pdf
CFR: (1)
14 CFR 39.13