[Federal Register Volume 70, Number 189 (Friday, September 30, 2005)]
[Proposed Rules]
[Pages 57221-57222]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-19558]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22403; Directorate Identifier 2005-NM-144-AD]
RIN 2120-AA64


Airworthiness Directives; Bombardier Model DHC-8-400 Series 
Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Notice of proposed rulemaking (NPRM); correction.

-----------------------------------------------------------------------

SUMMARY: The FAA is correcting a typographical error in an NPRM that 
was published in the Federal Register on September 14, 2005 (70 FR 
54316). The error resulted in an incorrect Docket No. The NPRM applies 
to certain Bombardier Model DHC-8-400 series airplanes. The NPRM would 
require an inspection of the laminated shims for cracks, damage, or 
extrusion between the forward attachment fittings of the horizontal 
stabilizer and the top rib of the vertical stabilizer; a torque check 
of the attachment bolts in the attachment fittings of the front, 
middle, and rear spars; and corrective actions if necessary.

FOR FURTHER INFORMATION CONTACT: George Duckett, Aerospace Engineer, 
Airframe and Propulsion Branch, ANE-171, FAA, New York Aircraft 
Certification Office, 1600 Stewart Avenue, suite 410, Westbury, New 
York 11590; telephone (516) 256-7525; fax (516) 794-5531.

SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued a 
notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include 
an AD that would apply to certain Bombardier Model DHC-8-400 series 
airplanes. That NPRM was published in the Federal Register on September 
14, 2005 (70 FR 54316). That NPRM proposed to require an inspection of 
the laminated shims for cracks, damage, or extrusion between the 
forward attachment fittings of the horizontal stabilizer and the top 
rib of the vertical stabilizer; a torque check of the attachment bolts 
in the attachment

[[Page 57222]]

fittings of the front, middle, and rear spars; and corrective actions 
if necessary.
    As published, that NPRM specifies an incorrect Docket No. (i.e., 
FAA-2005-20403) throughout preamble and the regulatory text of the AD. 
The correct Docket No. is FAA-2005-22403.
    No other part of the regulatory information has been changed; 
therefore, the NPRM is not republished in the Federal Register.
    The last date for submitting comments to the NPRM remains October 
14, 2005.


Sec.  39.13  [Corrected]

    In the Federal Register of September 14, 2005, on page 54318, in 
the first column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES of 
NPRM, Docket No. FAA-2005-22403, Directorate Identifier 2005-NM-144-AD 
is corrected to read as follows:
* * * * *
Bombardier, Inc. (Formerly de Havilland, Inc.): Docket No. FAA-2005-
22403; Directorate Identifier 2005-NM-144-AD.
* * * * *

    Issued in Renton, Washington, on September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-19558 Filed 9-29-05; 8:45 am]
BILLING CODE 4910-13-P