98-10054. Airworthiness Directives; Boeing Model 747 and 767 Series Airplanes Equipped With General Electric (GE) CF6-80C2 Engines  

  • [Federal Register Volume 63, Number 73 (Thursday, April 16, 1998)]
    [Rules and Regulations]
    [Pages 18817-18819]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 98-10054]
    
    
    
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    Federal Register / Vol. 63, No. 73 / Thursday, April 16, 1998 / Rules 
    and Regulations
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-NM-79-AD; Amendment 39-10472; AD 98-08-23]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Boeing Model 747 and 767 Series 
    Airplanes Equipped With General Electric (GE) CF6-80C2 Engines
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule; request for comments.
    
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    SUMMARY: This amendment supersedes an existing airworthiness directive 
    (AD), applicable to certain Boeing Model 747 and 767 series airplanes, 
    that currently requires revising the FAA-approved Airplane Flight 
    Manual (AFM) to prohibit the use of certain fuels; and either replacing 
    the existing placard on the door of the fueling control panel with a 
    new placard, or replacing all dribble flow fuel nozzles (DFFN's) with 
    standard fuel nozzles, which terminates the requirements for a placard 
    and AFM revision. This amendment continues these requirements and adds 
    additional airplanes to the applicability. This amendment is prompted 
    by a report of an engine flameout due to the use of JP-4 or Jet B fuel 
    during certification testing on an engine with DFFN's installed. The 
    actions specified in this AD are intended to prevent such engine 
    flameouts and consequent engine shutdown.
    
    DATES: Effective May 1, 1998.
        The incorporation by reference of certain publications, as listed 
    in the regulations, was previously approved by the Director of the 
    Federal Register as of November 12, 1997 (62 FR 55728, October 28, 
    1997).
        Comments for inclusion in the Rules Docket must be received on or 
    before June 15, 1998.
    
    ADDRESSES: Submit comments in triplicate to the Federal Aviation 
    Administration (FAA), Transport Airplane Directorate, ANM-114, 
    Attention: Rules Docket No. 98-NM-79-AD, 1601 Lind Avenue, SW., Renton, 
    Washington 98055-4056.
        The service information referenced in this AD may be obtained from 
    Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 
    98124-2207. This information may be examined at the FAA, Transport 
    Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at 
    the Office of the Federal Register, 800 North Capitol Street, NW., 
    suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: Dionne Stanley, Aerospace Engineer, 
    Propulsion Branch, ANM-140S, Seattle Aircraft Certification Office, 
    FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, 
    Washington 98055-4056; telephone (425) 227-2250; fax (425) 227-1181.
    
    SUPPLEMENTARY INFORMATION: On October 17, 1997, the FAA issued AD 97-
    22-04, amendment 39-10175 (62 FR 55728, October 28, 1997), applicable 
    to certain Boeing Model 747 and 767 series airplanes, to require 
    revising the FAA-approved Airplane Flight Manual (AFM) to prohibit the 
    use of certain fuels; and either replacing the existing placard on the 
    door of the fueling control panel with a new placard, or replacing all 
    dribble flow fuel nozzles (DFFN's) with standard fuel nozzles, which 
    terminates the requirements for a placard and AFM revision. That action 
    was prompted by a report indicating that, during certification testing, 
    a General Electric CF6-80C2 engine with DFFN's installed experienced 
    flameout due to the use of JP-4 or Jet B fuel. The actions required by 
    that AD are intended to prevent such engine flameouts and consequent 
    engine shutdown.
    
    Restatement of the Relevant Service Information
    
        The FAA has reviewed and approved Boeing Alert Service Bulletins 
    747-11A2052 (for Model 747 series airplanes) and 767-11A0031 (for Model 
    767 series airplanes), both dated September 11, 1997, which describe 
    procedures for removing the existing placard on the door of the fueling 
    control panel and replacing it with a new placard that prohibits the 
    use of JP-4 and Jet B fuels (wide cut fuels).
        Additionally, these alert service bulletins describe procedures for 
    removing the DFFN's and replacing them with standard fuel nozzles. 
    Accomplishment of this replacement on the operator's entire fleet 
    eliminates the need for a placard that prohibits the use of wide cut 
    fuels.
    
    Explanation of the Requirements of the Rule
    
        Since an unsafe condition has been identified that is likely to 
    exist or develop on other airplanes of this same type design that are 
    equipped with DFFN's, this AD is being issued to continue to require 
    revisions to the FAA-approved AFM to prohibit the use of wide cut 
    fuels. This AD also is being issued to continue to require either 
    replacement of the existing placard on the door of the fueling control 
    panel with a new placard, or replacement of all DFFN's with standard 
    fuel nozzles (the latter option terminates the requirements for an AFM 
    revision and a new placard). In addition, this amendment expands the 
    applicability to include all Boeing Model 747 and 767 series airplanes 
    with GE CF6-80C2 engines and those airplanes delivered subsequent to 
    the issuance of AD 97-22-04. These actions are required to be 
    accomplished in accordance with the service bulletins described 
    previously, except as discussed below.
    
    Differences Between This AD and the Previous AD
    
        Operators should note that, in addition to the list of effective 
    airplanes referenced in Boeing Alert Service Bulletin 747-11A2052 (for 
    Model 747 series airplanes) or Boeing Alert Service Bulletin 767-
    11A0031 (for Model 767 series airplanes), both dated September 11, 
    1997, this amendment expands the applicability to all Boeing Model 747 
    and 767 series airplanes equipped with General Electric CF6-80C2 
    engines, regardless of whether or not the airplanes are equipped with 
    DFFN's. The FAA finds that there is a likelihood that operators with a 
    mixed fleet (e.g., airplanes equipped with GE CF6-80C2 engines with 
    DFFN's installed and those without DFFN's installed) could 
    inadvertently use the incorrect type of fuel. To eliminate this 
    likelihood, the
    
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    FAA requires that if any airplane in an operator's fleet is equipped 
    with GE CF6-80C2 engines with DFFN's installed, the use of wide-cut 
    fuels is prohibited for the entire fleet. The previous AD was 
    applicable only to airplanes having GE CF6-80C2 engines equipped with 
    DFFN's; this rule is applicable to all airplanes having GE CF6-80C2 
    engines. The applicability is expanded in this AD to ensure that each 
    specific operator uses the correct type of fuel throughout its entire 
    fleet. Additionally, airplanes that were released from production into 
    service subsequent to the release of these service bulletins and that 
    were not covered by AD 97-22-04 are now included in the applicability 
    of this amendment.
    
    Determination of Rule's Effective Date
    
        Since a situation exists that requires the immediate adoption of 
    this regulation, it is found that notice and opportunity for prior 
    public comment hereon are impracticable, and that good cause exists for 
    making this amendment effective in less than 30 days.
    
    Comments Invited
    
        Although this action is in the form of a final rule that involves 
    requirements affecting flight safety and, thus, was not preceded by 
    notice and an opportunity for public 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 shall identify the Rules Docket number and be 
    submitted in triplicate to the address specified under the caption 
    ADDRESSES. 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 Number 98-NM-79-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 that it 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, 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 removing amendment AD 97-22-04, 39-
    10175 (62 FR 55728, November 12, 1997), and by adding a new 
    airworthiness directive (AD), amendment 39-10472, to read as follows:
    
    98-08-23  Boeing: Amendment 39-10472. Docket 98-NM-79-AD. Supersedes 
    AD 97-22-04, amendment 39-10175.
    
        Applicability: All Model 747 and 767 series airplanes having 
    General Electric CF6-80C2 engines, 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 (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, unless accomplished 
    previously.
        To prevent engine flameouts due to the use of JP-4 or Jet B fuel 
    on certain engines with dribble flow fuel nozzles (DFFN's) installed 
    and consequent shutdown, accomplish the following:
    
    Restatement of Requirements of AD 97-22-04
    
        (a) For airplanes with DFFN's installed: Within 14 days after 
    November 12, 1997 (the effective date of AD 97-22-04), revise 
    Section 1 of the Limitations Section of the FAA-approved Airplane 
    Flight Manual (AFM) to include the following procedures. This may be 
    accomplished by inserting a copy of this AD into the AFM.
        (1) Revise paragraph 1 of the Engine Fuel System section to read 
    as follows: ``The fuel designation is General Electric (GE) 
    Specification D50TF2, as revised. Fuel conforming to commercial jet 
    fuel specification ASTM-D-1655, Jet A, and Jet A-1 are authorized 
    for unlimited use in this engine. Fuels conforming to MIL-T-5624 
    grade JP-5 and MIL-T-83113 grade JP-8 are acceptable alternatives. 
    The engine will operate satisfactorily with any of the foregoing 
    fuels or any mixture thereof.'' And,
        (2) Add the following sentence to paragraph 2 of the Engine Fuel 
    System section: ``The use of Jet B and JP-4 fuel is prohibited.''
        (b) For airplanes with DFFN's installed: Within 30 days after 
    November 12, 1997, accomplish the requirements of paragraph (b)(1) 
    or (b)(2) of this AD, in accordance with either Boeing Alert Service 
    Bulletin 747-11A2052 (for Model 747 series airplanes) or 767-11A0031 
    (for Model 767 series airplanes), both dated September 11, 1997; as 
    applicable.
        (1) Remove the existing placard on the door of the fueling 
    control panel and replace it with a new placard that restricts the 
    use of JP-4 and Jet B fuels (wide cut fuels), in accordance with the 
    applicable alert service bulletin. Or
        (2) Remove the DFFN's, and replace them with standard fuel 
    nozzles, in accordance
    
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    with the applicable alert service bulletin. When an operator's 
    entire fleet has had all DFFN's replaced with standard fuel nozzles, 
    the AFM revision required by paragraph (a) of this AD may be removed 
    from the AFM and the placard required by paragraph (b)(1) of this AD 
    may be removed from each airplane.
    
    New Requirements of This AD
    
        (c) If a DFFN is installed on any airplane in a specific 
    operator's fleet, accomplish the requirements of paragraphs (c)(1) 
    and (c)(2) of this AD; in accordance with either Boeing Alert 
    Service Bulletin 747-11A2052 (for Model 747 series airplanes) or 
    Boeing Alert Service Bulletin 767-11A0031 (for Model 767 series 
    airplanes), both dated September 11, 1997; as applicable.
        (1) Within 14 days after the effective date of this AD, all 
    airplanes in a specific operator's fleet must revise Section 1 of 
    the Limitations Section of the FAA-approved AFM to include the 
    following procedures. This may be accomplished by inserting a copy 
    of this AD in the AFM.
        (i) Revise paragraph 1 of the Engine Fuel System section to read 
    as follows: ``The fuel designation is General Electric (GE) 
    Specification D50TF2, as revised. Fuel conforming to commercial jet 
    fuel specification ASTM-D-1655, Jet A, and Jet A-1 are authorized 
    for unlimited use in this engine. Fuels conforming to MIL-T-5624 
    grade JP-5 and MIL-T-83113 grade JP-8 are acceptable alternatives. 
    The engine will operate satisfactorily with any of the foregoing 
    fuels or any mixture thereof.'' And,
        (ii) Add the following sentence to paragraph 2 of the Engine 
    Fuel System section: ``The use of Jet B and JP-4 fuel is 
    prohibited.''
        (2) Within 30 days after the effective date of this AD, all 
    airplanes in a specific operator's fleet must accomplish the actions 
    required by paragraph (c)(2)(i) or (c)(2)(ii) of this AD, as 
    applicable.
        (i) Remove the existing placard on the door of the fueling 
    control panel and replace it with a new placard that restricts the 
    use of JP-4 and Jet B fuels (wide cut fuels), in accordance with the 
    applicable alert service bulletin. Or
        (ii) Remove the DFFN, and replace it with a standard fuel 
    nozzle, in accordance with the applicable alert service bulletin. 
    When an operator's entire fleet has had all DFFN's replaced with 
    standard fuel nozzles, the AFM revision required by paragraphs 
    (c)(1)(i) and (c)(1)(ii) of this AD may be removed from the AFM, and 
    the new placard required by paragraph (c)(2)(i) of this AD may be 
    removed from each airplane.
        (d) Except as provided by paragraph (e) of this AD, if a DFFN is 
    not installed on any airplane in a specific operator's fleet, no 
    further action is required by this AD.
        (e) As of the effective date of this AD, no person shall install 
    any DFFN having General Electric part number 9331M72P33, 9331M72P34, 
    or 9331M72P41 on any airplane unless the requirements specified by 
    paragraphs (c)(1)(i), (c)(1)(ii), and (c)(2)(i) of this AD have been 
    accomplished for the operator's entire fleet.
        (f) 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, Seattle Aircraft Certification 
    Office (ACO), FAA, Transport Airplane Directorate. Operators shall 
    submit their requests through an appropriate FAA Principal 
    Maintenance Inspector, who may add comments and then send it to the 
    Manager, Seattle ACO.
    
        Note 2: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Seattle ACO.
    
        (g) 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 (except no loading 
    of JP-4 or Jet B fuel).
        (h) Except as provided by paragraph (a) of this AD, the actions 
    shall be done in accordance with Boeing Alert Service Bulletin 747-
    11A2052, dated September 11, 1997, or Boeing Alert Service Bulletin 
    767-11A0031, dated September 11, 1997; as applicable. The 
    incorporation by reference of these service bulletins was approved 
    previously by the Director of the Federal Register as of November 
    12, 1997 (62 FR 55728, October 28, 1997). Copies may be obtained 
    from 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 Office of the Federal Register, 800 North Capitol Street, 
    NW., suite 700, Washington, DC.
        (i) This amendment becomes effective on May 1, 1998.
    
        Issued in Renton, Washington, on April 9, 1998.
    John J. Hickey,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 98-10054 Filed 4-15-98; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
5/1/1998
Published:
04/16/1998
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; request for comments.
Document Number:
98-10054
Dates:
Effective May 1, 1998.
Pages:
18817-18819 (3 pages)
Docket Numbers:
Docket No. 98-NM-79-AD, Amendment 39-10472, AD 98-08-23
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
98-10054.pdf
CFR: (1)
14 CFR 39.13