98-12513. Airworthiness Directives; Bombardier Model CL-600-2B16 Series Airplanes  

  • [Federal Register Volume 63, Number 95 (Monday, May 18, 1998)]
    [Rules and Regulations]
    [Page 27195]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 98-12513]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-NM-21-AD; Amendment 39-10425; AD 97-25-11R1]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Bombardier Model CL-600-2B16 Series 
    Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Direct final rule; confirmation of effective date.
    
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    SUMMARY: This document confirms the effective date of a direct final 
    rule published on March 27, 1998 which revised an existing 
    airworthiness directive (AD), applicable to certain Bombardier Model 
    CL-600-2B16 series airplanes, that currently requires disabling the 
    remote fuel/defuel panel in the cockpit; and provides for an optional 
    modification of the remote fuel/defuel panel, which would terminate the 
    requirement to disable the panel. The direct final rule amendment 
    reduces the applicability of the existing AD. The direct final rule 
    amendment was prompted by reports of in-flight failure of the panel 
    that resulted when a circuit breaker on a battery bus opened due to 
    insufficient current flow capacity. The actions specified in this AD 
    are intended to prevent the circuit breakers from opening during 
    flight, which could result in irreversible loss of engine indicating 
    and fuel quantity systems in the cockpit.
    
    DATES: The direct final rule published at 63 FR 14804 is effective on 
    June 25, 1998.
    
    FOR FURTHER INFORMATION CONTACT: Brett Portwood, Aerospace Engineer, 
    Systems and Equipment Branch, ANM-130L, FAA, Transport Airplane 
    Directorate, Los Angeles Aircraft Certification Office, 3960 Paramount 
    Boulevard, Lakewood, California 90712; telephone (562) 627-5350; fax 
    (562) 627-5210.
    
    SUPPLEMENTARY INFORMATION: The FAA published the direct final rule with 
    request for comments in the Federal Register on March 27, 1998 (63 FR 
    14804). The FAA uses the direct final rulemaking procedure for a non-
    controversial rule where the FAA anticipates that there will be no 
    adverse public comment. The direct final rule advised the public that 
    no adverse comments were anticipated, and that unless a written adverse 
    comment, or a written notice of intent to submit such an adverse 
    comment, was received within the comment period, the regulation would 
    become effective on June 25, 1998. No adverse comments were received, 
    and thus this document confirms that this final rule will become 
    effective on that date, with the airworthiness directive (AD) number 
    shown at the beginning of this document.
    
        Issued in Renton, Washington, on May 5, 1998.
    John J. Hickey,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 98-12513 Filed 5-15-98; 8:45 am]
    BILLING CODE 4910-13-P
    
    
    

Document Information

Effective Date:
6/25/1998
Published:
05/18/1998
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Direct final rule; confirmation of effective date.
Document Number:
98-12513
Dates:
The direct final rule published at 63 FR 14804 is effective on June 25, 1998.
Pages:
27195-27195 (1 pages)
Docket Numbers:
Docket No. 98-NM-21-AD, Amendment 39-10425, AD 97-25-11R1
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
98-12513.pdf
CFR: (1)
14 CFR 39