97-13468. Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes  

  • [Federal Register Volume 62, Number 99 (Thursday, May 22, 1997)]
    [Proposed Rules]
    [Pages 27986-27987]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 97-13468]
    
    
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    Proposed Rules
                                                    Federal Register
    ________________________________________________________________________
    
    This section of the FEDERAL REGISTER contains notices to the public of 
    the proposed issuance of rules and regulations. The purpose of these 
    notices is to give interested persons an opportunity to participate in 
    the rule making prior to the adoption of the final rules.
    
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    Federal Register / Vol. 62, No. 99 / Thursday, May 22, 1997 / 
    Proposed Rules
    
    [[Page 27986]]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 96-NM-211-AD]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Notice of proposed rulemaking (NPRM).
    
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    SUMMARY: This document proposes the adoption of a new airworthiness 
    directive (AD) that is applicable to certain Saab Model SAAB 2000 
    series airplanes. This proposal would require performing a one-time 
    inspection of the dropout boxes of the passenger oxygen system to 
    detect discrepancies and determine whether the system operates 
    properly; correcting any discrepancy found; and reworking or installing 
    new components, if necessary. This proposal is prompted by a report 
    indicating that the oxygen system failed to operate correctly after 
    activation at a low cabin pressure due to the incorrect installation of 
    the oxygen masks or oxygen generators during manufacturing. The actions 
    specified by the proposed AD are intended to ensure that a sufficient 
    supply of oxygen is provided to airplane passengers in the event of 
    rapid decompression of the airplane.
    
    DATES: Comments must be received by July 3, 1997.
    
    ADDRESSES: Submit comments in triplicate to the Federal Aviation 
    Administration (FAA), Transport Airplane Directorate, ANM-103, 
    Attention: Rules Docket No. 96-NM-211-AD, 1601 Lind Avenue, SW., 
    Renton, Washington 98055-4056. Comments may be inspected at this 
    location between 9:00 a.m. and 3:00 p.m., Monday through Friday, except 
    Federal holidays.
        The service information referenced in the proposed rule may be 
    obtained from Saab Aircraft AB, Saab Aircraft Product Support, S-
    581.88, Linkping, Sweden. This information may be examined at the FAA, 
    Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, 
    Washington.
    
    FOR FURTHER INFORMATION CONTACT: Ruth Harder, Aerospace Engineer, 
    Standardization Branch, ANM-113, FAA, Transport Airplane Directorate, 
    1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
    227-1721; fax (425) 227-1149.
    
    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 shall 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 summarizing 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 Number 96-NM-211-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, Transport Airplane Directorate, ANM-103, Attention: Rules 
    Docket No. 96-NM-211-AD, 1601 Lind Avenue, SW., Renton, Washington 
    98055-4056.
    
    Discussion
    
        The Luftfartsverket (LFV), which is the airworthiness authority for 
    Sweden, notified the FAA that an unsafe condition may exist on certain 
    Saab Model SAAB 2000 series airplanes. The LFV advises of reports 
    indicating that the passenger oxygen system failed to operate correctly 
    in an airplane after activation at a low cabin pressure due to the 
    improper packing of the mask assemblies or incorrect installation of 
    the oxygen generators or masks during manufacturing. The following 
    failures were noted for some of the oxygen system components:
        1. Lids to the dropout boxes did not open.
        2. Oxygen mask hoses became disconnected from the generator outlet 
    connections.
        3. Oxygen masks were not released from the dropout boxes.
        In addition, subsequent inspection of the passenger oxygen system 
    on one Model SAAB 2000 series airplane revealed that two oxygen 
    generators were released along with the oxygen masks, which indicates 
    that the oxygen mask assembly was incorrectly packed in the dropout 
    boxes.
        Improper functioning of the passenger oxygen system, if not 
    corrected, could result in an insufficient supply of oxygen being 
    provided to airplane passengers in the event of rapid decompression of 
    the airplane.
    
    Explanation of Relevant Service Information
    
        Saab has issued Service Bulletin 2000-35-001, dated February 20, 
    1996, which describes procedures for performing a one-time inspection 
    of the dropout boxes of the passenger oxygen system to detect 
    discrepancies and determine whether the system operates properly; 
    correcting any discrepancy found; and reworking or installing new 
    components, if necessary.
        The LFV classified this service bulletin as mandatory and issued 
    Swedish airworthiness directive (SAD) 1-091, dated February 20, 1996, 
    in order to assure the continued airworthiness of these airplanes in 
    Sweden.
    
    FAA's Conclusions
    
        This airplane model is manufactured in Sweden and is type 
    certificated for operation in the United States under the provisions of 
    section 21.29 of the
    
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    Federal Aviation Regulations (14 CFR 21.29) and the applicable 
    bilateral airworthiness agreement. Pursuant to this bilateral 
    airworthiness agreement, the LFV has kept the FAA informed of the 
    situation described above. The FAA has examined the findings of the 
    LFV, reviewed all available information, and determined that AD action 
    is necessary for products of this type design that are certificated for 
    operation in the United States.
    
    Explanation of Requirements of Proposed Rule
    
        Since an unsafe condition has been identified that is likely to 
    exist or develop on other airplanes of the same type design registered 
    in the United States, the proposed AD would require performing a one-
    time inspection of the dropout boxes of the passenger oxygen system to 
    detect discrepancies and determine whether the system operates 
    properly; correcting any discrepancy found; and reworking or installing 
    new components, if necessary. These actions would be required to be 
    accomplished in accordance with the service bulletin described 
    previously.
    
    Cost Impact
    
        The FAA estimates that 3 Saab Model SAAB 2000 series airplanes of 
    U.S. registry would be affected by this proposed AD, that it would take 
    approximately 3 work hours per airplane to accomplish the proposed 
    actions, and that the average labor rate is $60 per work hour. Based on 
    these figures, the cost impact of the proposed AD on U.S. operators is 
    estimated to be $540, or $180 per airplane.
        The cost impact figure discussed above is based on assumptions that 
    no operator has yet accomplished any of the proposed 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 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 proposed 
    regulation: (1) Is not a ``significant regulatory action'' under 
    Executive Order 12866; (2) is not a ``significant rule'' under the 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 is contained 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 the following new 
    airworthiness directive:
    
    SAAB Aircraft AB: Docket 96-NM-211-AD.
    
        Applicability: Model SAAB 2000 series airplanes, having serial 
    numbers -003 through -039 inclusive; certificated in any category.
    
        Note 1: This AD applies to each airplane identified in the 
    preceding applicability provision, regardless of whether it has been 
    otherwise 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 (b) 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 an insufficient supply of oxygen being provided to 
    airplane passengers in the event of rapid decompression of the 
    airplane, accomplish the following:
        (a) Within 30 days after the effective date of this AD, perform 
    a one-time inspection of the dropout boxes of the passenger oxygen 
    system to detect discrepancies and determine whether the system 
    operates properly, in accordance with the Accomplishment 
    Instructions of Saab Service Bulletin 2000-35-001, dated February 
    20, 1996.
        (1) If the passenger oxygen system operates properly and no 
    discrepancy is found in this system, no further action is required 
    by this AD.
        (2) If any discrepancy is found in the passenger oxygen system, 
    prior to further flight, perform rework or install new components, 
    as applicable, in accordance with the service bulletin.
        (b) 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, Standardization Branch, ANM-113, 
    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, 
    Standardization Branch, ANM-113.
    
        Note 2: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Standardization Branch, ANM-113.
        (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.
    
        Issued in Renton, Washington, on May 16, 1997.
    Darrell M. Pederson,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 97-13468 Filed 5-21-97; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Published:
05/22/1997
Department:
Federal Aviation Administration
Entry Type:
Proposed Rule
Action:
Notice of proposed rulemaking (NPRM).
Document Number:
97-13468
Dates:
Comments must be received by July 3, 1997.
Pages:
27986-27987 (2 pages)
Docket Numbers:
Docket No. 96-NM-211-AD
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
97-13468.pdf
CFR: (1)
14 CFR 39.13