Airworthiness Directives; Bombardier Model CL-215-1A10 and CL- 215-6B11 Series Airplanes; Correction

[Federal Register Volume 63, Number 85 (Monday, May 4, 1998)]
[Rules and Regulations]
[Page 24389]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-11560]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98-NM-05-AD; Amendment 39-10458]
RIN 2120-AA64


Airworthiness Directives; Bombardier Model CL-215-1A10 and CL-
215-6B11 Series Airplanes; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Direct final rule; correction.

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SUMMARY: This document corrects an error that appeared in amendment 39-
10458 that was published in the Federal Register on April 10, 1998 (63 
FR 17672). The error resulted in the inadvertent omission of the 
applicability statement of the amendment. This amendment is applicable 
to certain Bombardier Model CL-215-1A10 and CL-215-6B11 series 
airplanes. This amendment requires repetitive inspections to detect 
cracking on certain wing to fuselage frame-angles, and repair, if 
necessary.

DATES: Effective July 9, 1998.
    The incorporation by reference of certain publications listed in 
the regulations was previously approved by the Director of the Federal 
Register as of July 9, 1998 (63 FR 17672, April 10, 1998).

FOR FURTHER INFORMATION CONTACT: Serge Napoleon, Aerospace Engineer, 
Airframe and Propulsion Branch, ANE-171, FAA, Engine and Propeller 
Directorate, New York Aircraft Certification Office, 10 Fifth Street, 
Third Floor, Valley Stream, New York 11581; telephone (516) 256-7512; 
fax (516) 568-2716.

SUPPLEMENTARY INFORMATION: Amendment 39-10458, applicable to certain 
Bombardier Model CL-215-1A10 and CL-215-6B11 series airplanes, was 
published in the Federal Register on April 10, 1998 (63 FR 17672). That 
amendment requires repetitive inspections to detect cracking on certain 
wing to fuselage frame-angles, and repair, if necessary.
    As published, the applicability statement of the amendment was 
omitted inadvertently. The FAA has determined that this omission must 
be corrected. In all other respects, the original document is correct.
    Since no other part of the regulatory information has been changed, 
the direct final rule is not being republished.
    The effective date of this amendment remains July 9, 1998.


Sec. 39.13  [Corrected]

    1. On page 17674, in the first column, the airworthiness directive, 
amendment 39-10458, is corrected by adding the applicability statement 
preceding Note 1 to read as follows:
* * * * *
    Applicability: Model CL-215-1A10 and CL-215-6B11 series 
airplanes, serial numbers 1001 through 1125 inclusive, certificated 
in any category.
* * * * *
    Issued in Renton, Washington, on April 24, 1998.
Gary L. Killion,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 98-11560 Filed 5-1-98; 8:45 am]
BILLING CODE 4910-13-U

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