Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes; Correction

[Federal Register Volume 66, Number 229 (Wednesday, November 28, 2001)]
[Rules and Regulations]
[Pages 59357-59358]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 01-29492]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-CE-28-AD; Amendment 39-12504; AD 2001-23-07]
RIN 2120-AA64


Airworthiness Directives; Reims Aviation S.A. Model F406 
Airplanes; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2001-23-07, which was published in the Federal Register on 
November 15, 2001 (66 FR 57364), and concerns certain Reims Model F406 
airplanes. The FAA incorrectly referenced the AD number as ``AD 2001-
01-07'' instead of
    ``AD 2001-23-07.'' This AD requires repetitive inspections of the 
canted rib upper cap in the center wing carry-through area for cracks, 
and, if cracks are found, immediate repair of the cracks or 
modification of this area depending on the extent of any cracks found. 
This AD also requires modifying the canted rib upper cap at a certain 
time period as terminating action for the repetitive inspections. This 
action corrects the AD to reflect the correct AD number.

EFFECTIVE DATE: The effective date of this AD remains January 7, 2002.

FOR FURTHER INFORMATION CONTACT: Brian A. Hancock, Aerospace Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4143, facsimile: (816) 329-4090.

SUPPLEMENTARY INFORMATION:

Discussion

    On November 6, 2001, FAA issued AD 2001-01-07, Amendment 39-12504 
(66 FR 57364, November 15, 2001), which applies to certain Reims Model 
F406 airplanes. This AD currently requires repetitive inspections of 
the canted rib upper cap in the center wing carry-through area for 
cracks, and, if cracks are found, immediate repair of the cracks or 
modification of this area depending on the extent of any cracks found. 
This AD also requires modifying the canted rib upper cap at a certain

[[Page 59358]]

time period as terminating action for the repetitive inspections.

Need for the Correction

    We incorrectly referenced the AD number as ``AD 2001-01-07'' 
instead of ``AD 2001-23-07.'' If we did not correct the AD number, then 
the logbooks of the affected airplane would reference compliance with 
the wrong AD.

Correction of Publication

    Accordingly, the publication of November 15, 2001 (66 FR 57364), of 
Amendment 39-12504; AD 2001-01-07, which was the subject of FR Doc. 01-
28571, is corrected as follows:


Sec. 39.13  [Corrected]

    On page 57364, under heading 14 CFR part 39, in the second column, 
the 22nd line from the bottom of the page; and on page 57366, in 
Sec. 39.13, in the second column, the 1st line from the top of the 
page, correct ``2001-01-07'' to ``2001-23-07''.
    Action is taken herein to correct these references in AD 2001-23-07 
and to add this AD correction to Sec. 39.13 of the Federal Aviation 
Regulations (14 CFR 39.13).
    The effective date remains January 7, 2002.

    Issued in Kansas City, Missouri, on November 15, 2001.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 01-29492 Filed 11-27-01; 8:45 am]
BILLING CODE 4910-13-U

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