[Federal Register Volume 62, Number 62 (Tuesday, April 1, 1997)]
[Rules and Regulations]
[Page 15373]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 97-8250]
[[Page 15373]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 96-CE-09-AD; Amendment 39-9872; AD 97-01-01]
RIN 2120-AA64
Airworthiness Directives; The New Piper Aircraft, Inc. PA24,
PA28R, PA30, PA32R, PA34, and PA39 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) 97-01-01, which was published in the Federal Register on January
2, 1997 (62 FR 10), and concerns The New Piper Aircraft, Inc. (Piper)
PA24, PA28R, PA30, PA32R, PA34, and PA39 series airplanes. The
amendment number in this AD is incorrectly referenced as Amendment 39-
9782 instead of 39-9872 in two places. All other reference is correct.
The AD currently requires repetitively inspecting the main gear
sidebrace studs for cracks, and replacing any main gear sidebrace stud
found cracked. This action corrects the AD to reflect the right
amendment number throughout the entire document.
EFFECTIVE DATE: February 7, 1997.
FOR FURTHER INFORMATION CONTACT: Christina Marsh, Aerospace Engineer,
FAA, Atlanta Aircraft Certification Office, Campus Building, 1701
Columbia Avenue, suite 2-160, College Park, Georgia 30337-2748;
telephone (404) 305-7362; facsimile (404) 305-7348.
SUPPLEMENTARY INFORMATION:
Discussion
On December 23, 1996, the FAA issued AD 97-01-01, Amendment 39-9872
(62 FR 10, January 2, 1997), which applies to Piper PA24, PA28R, PA30,
PA32R, PA34, and PA39 series airplanes. This AD requires repetitively
inspecting the main gear sidebrace studs for cracks, and replacing any
main gear sidebrace stud found cracked.
Need for the Correction
The amendment number in this AD is incorrectly referenced as 39-
9782, instead of 39-9872, in two different places. All other reference
is correct. As written, operators of Piper PA24, PA28R, PA30, PA32R,
PA34, and PA39 series airplanes may log compliance with the right AD
number, but the wrong amendment number, therefore causing the potential
for confusion as to whether they are in compliance with the AD.
Correction of Publication
Accordingly, the publication of January 2, 1997 (62 FR 10), of
Amendment 39-9872; AD 97-01-01, which was the subject of FR Doc. 96-
33231, is corrected as follows:
Sec. 39.13 [Corrected]
On page 11, in the third column, section 39.13, the 12th line from
the top of the column, correct ``Amendment 39-9782'' to ``Amendment 39-
9872''.
On page 14, in the second column, section 39.13, in paragraph (h)
of the AD, the 24th line from the bottom of the column, correct ``(39-
9782)'' to ``(39-9872)''.
Action is taken herein to correct this reference in AD 97-01-01 and
to add this AD correction to section 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
The effective date remains February 7, 1997.
Issued in Kansas City, Missouri on March 26, 1997.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 97-8250 Filed 3-31-97; 8:45 am]
BILLING CODE 4910-13-U
