Airworthiness Directives; Goodrich Avionics Systems, Inc. TAWS8000 Terrain Awareness Warning System

[Federal Register Volume 69, Number 101 (Tuesday, May 25, 2004)]
[Rules and Regulations]
[Page 29651]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-11704]



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Federal Register / Vol. 69, No. 101 / Tuesday, May 25, 2004 / Rules 
and Regulations

[[Page 29651]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-CE-47-AD; Amendment 39-13584; AD 2004-08-15]
RIN 2120-AA64


Airworthiness Directives; Goodrich Avionics Systems, Inc. 
TAWS8000 Terrain Awareness Warning System

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2004-08-15, which was published in the Federal Register on April 
21, 2004 (69 FR 21393), and applies to all Goodrich Avionics Systems, 
Inc. (Goodrich) TAWS8000 terrain awareness warning systems (TAWS) that 
are installed on airplanes. We incorrectly referred to paragraph (d)(1) 
in the Compliance column of paragraph (e)(2). The correct reference is 
(e)(1). This action corrects the table in paragraph (e) of AD 2004-08-
15, Amendment 39-13584.

EFFECTIVE DATE: The effective date of this AD remains June 7, 2004.

FOR FURTHER INFORMATION CONTACT: Brenda S. Ocker, Aerospace Engineer, 
FAA, Chicago Aircraft Certification Office, 2300 East Devon Avenue, Des 
Plaines, Illinois 60018; telephone: (847) 294-7126; facsimile: (847) 
294-7834.

SUPPLEMENTARY INFORMATION:

Discussion

    On April 13, 2004, FAA issued AD 2004-08-15, Amendment 39-13584 (69 
FR 21393), that applies to all Goodrich TAWS8000 terrain awareness 
warning systems (TAWS) that are installed on airplanes. This AD 
requires you to inspect the TAWS installation and modify any TAWS where 
both the TAWS and any other device are connected to the same baro set 
potentiometer. This AD also prohibits future installation or 
reconfiguration of any TAWS8000 TAWS that does not incorporate hardware 
``Mod C''.

Need for the Correction

    The FAA incorrectly referred to paragraph (d)(1) in the Compliance 
column of paragraph (e)(2). The correct reference is (e)(1). This 
action corrects the table in paragraph (e) of AD 2004-08-15, Amendment 
39-13584.
    This correction is needed to ensure that the affected airplane 
owners/operators do the corrective action after the inspection required 
in paragraph (e)(1).

Correction of Publication

0
Accordingly, the publication of April 21, 2004 (69 FR 21393), of 
Amendment 39-13584; AD 2004-08-15, which was the subject of FR Doc. 04-
8792, is corrected as follows:

PART 39--AIRWORTHINESS DIRECTIVES


Sec.  39.13  [Corrected]

0
On page 21395, in Sec.  39.13 [Amended], 2., replace the text in the 
Compliance column of paragraph (e)(2) of the AD with the following 
text: Before further flight after the inspection required in paragraph 
(e)(1) of this AD.''
0
Action is taken herein to correct this reference in AD 2004-08-15 and 
to add this AD correction to Sec.  39.13 of the Federal Aviation 
Regulations (14 CFR 39.13).
    The effective date remains June 7, 2004.

    Issued in Kansas City, Missouri, on May 18, 2004.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 04-11704 Filed 5-24-04; 8:45 am]
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