Airworthiness Directives; Pilatus Britten-Norman Ltd. BN-2A and BN-2A Mk 111 Series Airplanes; Correction

[Federal Register Volume 62, Number 133 (Friday, July 11, 1997)]
[Rules and Regulations]
[Pages 37130-37131]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 97-18139]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 96-CE-24-AD; Amendment 39-10058; AD 97-14-01]
RIN 2120-AA64


Airworthiness Directives; Pilatus Britten-Norman Ltd. BN-2A and 
BN-2A Mk 111 Series 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) 97-14-01, which was published in the Federal Register on July 2, 
1997 (62 FR 35670), and is applicable to Pilatus Britten-Norman Ltd. 
(PBN) BN-2A and BN-2A Mk 111 series airplanes. This AD currently has an 
issue date and effective date of August 18, 1997. The AD currently 
requires inspecting the LH rudder bar assembly for wall thickness

[[Page 37131]]

of the slider tube unit and modifying the rudder bar assembly by 
replacing the LH slider tube with a new strengthened slider tube unit. 
This action changes the issue date of this AD to June 24, 1997 and 
leaves the effective date at August 18, 1997.

EFFECTIVE DATE: August 18, 1997.

FOR FURTHER INFORMATION CONTACT: Mr. S.M. Nagarajan, Project Officer, 
Small Airplane Directorate, Aircraft Certification Service, FAA, 1201 
Walnut, suite 900, Kansas City, Missouri 64106; telephone (816) 426-
6932; facsimile (816) 426-2169.

SUPPLEMENTARY INFORMATION:

Discussion

    On June 24, 1997, the FAA issued AD 97-14-01, Amendment 39-10058 
(62 FR 35670, July 2, 1997), which applies to Pilatus Britten-Norman 
Ltd. (PBN) BN-2A and BN-2A Mk 111 series airplanes. This AD requires 
inspecting the left-hand (LH) rudder bar assembly for wall thickness of 
the slider tube unit and modifying the rudder bar assembly by replacing 
the LH slider tube with a new strengthened slider tube unit.

Need for the Correction

    This AD currently has the wrong issue date of August 18, 1997. The 
last sentence of the AD reads ``Issued in Kansas City, Missouri on 
August 18, 1997.'' This is the effective date of this AD and was 
repeated as the issue date by mistake.

Correction of Publication

    Accordingly, the publication of July 2, 1997 (62 FR 35670), of 
Amendment 39-10058; AD 97-14-01, which was the subject of FR Doc. 97-
17098, is corrected as follows:


Sec. 39.13  [Corrected]

    In AD 97-14-01, the issue date before the signature block of the 
AD, Federal Register page number 35672, third column should read 
``Issued in Kansas City, Missouri on June 24, 1997''.
    Action is taken herein to correct this reference in AD 97-14-01 and 
to add this AD correction to section 39.13 of the Federal Aviation 
Regulations (14 CFR 39.13).
    The effective date of the AD remains August 18, 1997.

    Issued in Kansas City, Missouri on July 2, 1997.
James E., Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 97-18139 Filed 7-10-97; 8:45 am]
BILLING CODE 4910-13-P

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