Airworthiness Directives; Raytheon Aircraft Company 90, 99, 100, 200, and 1900 Series Airplanes; Correction

[Federal Register Volume 62, Number 85 (Friday, May 2, 1997)]
[Rules and Regulations]
[Pages 24014-24015]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 97-11196]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 96-CE-11-AD; Amendment 39-9963; AD 97-06-06]
RIN 2120-AA64


Airworthiness Directives; Raytheon Aircraft Company 90, 99, 100, 
200, and 1900 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) 97-06-06, which was published in the Federal Register on March 13, 
1997 (62 FR 11764), and concerns Raytheon Aircraft Company (Raytheon) 
90, 99, 100, 200, and 1900 series airplanes (formerly referred to as 
Beech 90, 99, 100, 200, and 1900 series airplanes). This AD currently 
has two paragraph (f)'s. The AD currently requires inspecting the pilot 
and copilot chairs to ensure that the locking pins will fully engage in 
the seat tracks, and modifying any chair where the locking pin fails to 
fully engage or is misaligned. This action changes the second paragraph 
(f) to paragraph (g).

EFFECTIVE DATE: May 9, 1997.


[[Page 24015]]


FOR FURTHER INFORMATION CONTACT: Mr. Steve Potter, Aerospace Engineer, 
Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Wichita, 
Kansas 67209; telephone (316) 946-4124; facsimile (316) 946-4407.

SUPPLEMENTARY INFORMATION:

Discussion

    On March 5, 1997, the FAA issued AD 97-06-06, Amendment 39-9963 (62 
FR 11764, March 13, 1997), which applies to Raytheon 90, 99, 100, 200, 
and 1900 series airplanes (formerly referred to as Beech 90, 99, 100, 
200, and 1900 series airplanes). This AD requires currently requires 
inspecting the pilot and copilot chairs to ensure that the locking pins 
will fully engage in the seat tracks, and modifying any chair where the 
locking pin fails to fully engage or is misaligned.

Need for the Correction

    This AD currently has two paragraph (f)'s. The second paragraph (f) 
gives the effective date of the AD and should be referenced as 
paragraph (g). As written, operators of Raytheon 90, 99, 100, 200, and 
1900 series airplanes may inadvertently not notice or miss the second 
paragraph (f) of the AD because there was already one paragraph (f); 
thereby, missing the effective date of the AD.

Correction of Publication

    Accordingly, the publication of March 13, 1997 (62 FR 11764), of 
Amendment 39-9963; AD 97-06-06, which was the subject of FR Doc. 97-
6255, is corrected as follows:


Sec. 39.13  [Corrected]

    On page 11766, in the third column, Sec. 39.13, in AD 97-06-06, the 
second paragraph (f) is correctly designated as paragraph (g).
    Action is taken herein to correct this reference in AD 97-06-06 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 May 9, 1997.

    Issued in Kansas City, Missouri on April 24, 1997.
Larry A. Malir,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 97-11196 Filed 5-1-97; 8:45 am]
BILLING CODE 4910-13-U

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