96-27240. Airworthiness Directives; Jetstream Model 4100 Series Airplanes  

  • [Federal Register Volume 61, Number 216 (Wednesday, November 6, 1996)]
    [Rules and Regulations]
    [Pages 57300-57301]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 96-27240]
    
    
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    DEPARTMENT OF TRANSPORTATION
    14 CFR Part 39
    
    [Docket No. 96-NM-68-AD; Amendment 39-9796; AD 96-22-07]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Jetstream Model 4100 Series 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 Jetstream Model 4100 series airplanes, that 
    requires replacement of the existing decompression panel on the aft 
    bulkhead of the toilet compartment with a modified decompression panel. 
    This amendment is prompted by a report that a decompression panel that 
    does not meet flammability requirements was installed on these 
    airplanes during manufacture. The actions specified by this AD are 
    intended to prevent injury to the crew and passengers and damage to the 
    airplane structure due to the incapability of the decompression panel 
    to contain a fire.
    
    DATES: Effective December 11, 1996.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of December 11, 1996.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from Jetstream Aircraft Limited, Customer Support Department, 
    Prestwick International Airport, Ayrshire KA9 2RW, Scotland. 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: William Schroeder, Aerospace Engineer, 
    Standardization Branch, ANM-113, FAA, Transport Airplane Directorate, 
    1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (206) 
    227-2148; fax (206) 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 Jetstream Model 4100 
    series airplanes was published in the Federal Register on August 7, 
    1996 (61 FR 41039). That action proposed to require replacement of the 
    existing decompression panel on the aft bulkhead of the toilet
    
    [[Page 57301]]
    
    compartment with a modified decompression panel.
        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 17 Jetstream Model 4100 series airplanes of 
    U.S. registry will be affected by this AD, that it will take 
    approximately 6 work hours per airplane to accomplish the required 
    actions, and that the average labor rate is $60 per work hour. Required 
    parts will be supplied by the manufacturer at no cost to operators. 
    Based on these figures, the cost impact of the AD on U.S. operators is 
    estimated to be $6,120, or $360 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:
    
    96-22-07  Jetstream: Amendment 39-9796. Docket 96-NM-68-AD.
    
        Applicability: Model 4100 series airplanes; constructors numbers 
    41004 through 41017 inclusive, and 41019 through 41033 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 (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 injury to the crew and passengers and damage to the 
    airplane structure due to the incapability of the decompression 
    panel to contain a fire, accomplish the following:
        (a) Within 60 days after the effective date of this AD, replace 
    the existing decompression panel on the aft bulkhead of the toilet 
    compartment with a modified decompression panel, in accordance with 
    Jetstream Service Bulletin J41-25-068, dated November 9, 1995.
        (b) As of the effective date of this AD, no person shall install 
    a decompression panel having part number 04125106-403 on the 
    bulkhead assembly of any airplane.
        (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, 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.
    
        (d) 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.
        (e) The replacement shall be done in accordance with Jetstream 
    Service Bulletin J41-25-068, dated November 9, 1995. 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 Jetstream Aircraft Limited, Customer 
    Support Department, Prestwick International Airport, Ayrshire KA9 
    2RW, Scotland. 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.
        (f) This amendment becomes effective on December 11, 1996.
    
        Issued in Renton, Washington, on October 17, 1996.
    Darrell M. Pederson,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 96-27240 Filed 11-5-96; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
12/11/1996
Published:
11/06/1996
Department:
Transportation Department
Entry Type:
Rule
Action:
Final rule.
Document Number:
96-27240
Dates:
Effective December 11, 1996.
Pages:
57300-57301 (2 pages)
Docket Numbers:
Docket No. 96-NM-68-AD, Amendment 39-9796, AD 96-22-07
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
96-27240.pdf
CFR: (1)
14 CFR 39.13