98-16703. Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes  

  • [Federal Register Volume 63, Number 122 (Thursday, June 25, 1998)]
    [Rules and Regulations]
    [Pages 34591-34592]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 98-16703]
    
    
    
    [[Page 34591]]
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-NM-115-AD; Amendment 39-10629; AD 98-13-38]
    RIN 2120-AA64
    
    
    Airworthiness Directives; British Aerospace (Jetstream) Model 
    4101 Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
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    SUMMARY: This amendment adopts a new airworthiness directive (AD), 
    applicable to certain British Aerospace (Jetstream) Model 4101 
    airplanes, that requires installation of a warning placard for the fire 
    extinguisher exhaust port located in the rear baggage bay. This 
    amendment is prompted by issuance of mandatory continuing airworthiness 
    information by a foreign civil airworthiness authority. The actions 
    specified by this AD are intended to prevent blockage of the fire 
    extinguisher exhaust port, which could result in reduced fire 
    protection in the rear baggage bay and consequent injury to the 
    passengers and crewmembers.
    
    DATES: Effective July 30, 1998.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of July 30, 1998.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from AI(R) American Support, Inc., 13850 Mclearen Road, 
    Herndon, Virginia 20171. 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 
    Office of the Federal Register, 800 North Capitol Street, NW., suite 
    700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: Norman B. Martenson, Manager, 
    International Branch, ANM-116, FAA, Transport Airplane Directorate, 
    1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
    227-2110; fax (425) 227-1149.
    
    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 certain British Aerospace 
    (Jetstream) Model 4101 airplanes was published in the Federal Register 
    on April 21, 1998 (63 FR 19688). That action proposed to require 
    installation of a warning placard for the fire extinguisher exhaust 
    port located in the rear baggage bay.
    
    Comments
    
        Interested persons have been afforded an opportunity to participate 
    in the making of this amendment. Due consideration has been given to 
    the single comment received.
        The commenter supports the proposed rule.
    
    Conclusion
    
        After careful review of the available data, including the comment 
    noted above, the FAA has determined that air safety and the public 
    interest require the adoption of the rule as proposed.
    
    Cost Impact
    
        The FAA estimates that 57 airplanes of U.S. registry will be 
    affected by this AD, that it will take approximately 1 work hour per 
    airplane to accomplish the required installation, and that the average 
    labor rate is $60 per work hour. Required parts cost will be minimal. 
    Based on these figures, the cost impact of the installation required by 
    this AD on U.S. operators is estimated to be $3,420, or $60 per 
    airplane.
        The cost impact figure discussed above is 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 
    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:
    
    98-13-38  British Aerospace [Formerly Jetstream Aircraft Limited; 
    British Aerospace (Commercial Aircraft) Limited]: Amendment 39-
    10629. Docket 98-NM-115-AD.
    
        Applicability: Model 4101 airplanes, constructor's numbers 41004 
    through 41100 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 
    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 blockage of the fire extinguisher exhaust port, which 
    could result in reduced fire protection in the rear baggage bay and 
    consequent injury to the passengers and crewmembers, accomplish the 
    following:
        (a) Within 4 months after the effective date of this AD, install 
    a warning placard near the fire extinguisher exhaust port in the 
    rear baggage bay, in accordance with British Aerospace Regional 
    Aircraft Service Bulletin J41-11-020, dated November 10, 1997.
        (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, International Branch, ANM-116, FAA, 
    Transport Airplane Directorate. Operators shall submit their request 
    through an appropriate FAA Principal Maintenance
    
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    Inspector, who may add comments and then send it to the Manager, 
    International Branch, ANM-116.
    
        Note 2: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the International Branch, ANM-116.
        (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) The installation shall be done in accordance with British 
    Aerospace Regional Aircraft Service Bulletin J41-11-020, dated 
    November 10, 1997. 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 AI(R) American 
    Support, Inc., 13850 Mclearen Road, Herndon, Virginia 20171. 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.
    
        Note 3: The subject of this AD is addressed in British 
    airworthiness directive 015-11-97.
    
        (e) This amendment becomes effective on July 30, 1998.
    
        Issued in Renton, Washington, on June 17, 1998.
    Darrell M. Pederson,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 98-16703 Filed 6-24-98; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
7/30/1998
Published:
06/25/1998
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
98-16703
Dates:
Effective July 30, 1998.
Pages:
34591-34592 (2 pages)
Docket Numbers:
Docket No. 98-NM-115-AD, Amendment 39-10629, AD 98-13-38
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
98-16703.pdf
CFR: (1)
14 CFR 39.13