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2010-09-24
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Airworthiness Directives; The New Piper Aircraft, Inc. PA24, PA28R, PA30, PA32R, PA34, and PA39 Series Airplanes
Rules and Regulations
D09002ee1be027191
D09002ee1be027967
United States
Department of Transportation
originator
org
United States Government Agency or Subagency
United States
Federal Aviation Administration
originator
org
United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD) that supersedes AD 95-20-07, which currently requires repetitively inspecting the main gear sidebrace studs for cracks on certain The New Piper Aircraft, Inc. (Piper) PA24, PA28R, PA30, PA32R, PA34, and PA39 series airplanes, and replacing any cracked main gear sidebrace stud. This AD retains the repetitive inspection and possible replacement requirements of AD 95-20-07; specifies in the ``Applicability'' section of the AD that certain Model PA34-200T airplanes could contain a certain main gear sidebrace assembly configuration that is not affected; and incorporates additional modification and replacement options. This AD results from additional information received by the Federal Aviation Administration (FAA) after the issuance of AD 95-20-07 on the design and service history of the affected airplanes concerning this subject. The actions specified by this AD are intended to prevent a main landing gear collapse caused by main gear sidebrace stud cracks, which could result in loss of control of the airplane during landing operations.
62 FR 10
https://www.govinfo.gov/app/details/FR-1997-01-02/96-33231
96-33231
fr02ja97-3
RIN 2120-AA64
4910-13-U
Docket No. 96-CE-09-AD
Amendment 39-9872
AD 97-01-01
https://www.govinfo.gov/app/details/FR-1997-01-02/96-33231
https://www.govinfo.gov/content/pkg/FR-1997-01-02/html/96-33231.htm
https://www.govinfo.gov/content/pkg/FR-1997-01-02/pdf/96-33231.pdf
6 p.
10
15
62 FR 10
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; The New Piper Aircraft, Inc. PA24, PA28R, PA30, PA32R, PA34, and PA39 Series Airplanes; Federal Register Vol. 62, Issue
RULE
96-33231
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Docket No. 96-CE-09-AD
Amendment 39-9872
AD 97-01-01
4910-13-U
96-33231
Final rule.
This amendment adopts a new airworthiness directive (AD) that supersedes AD 95-20-07, which currently requires repetitively inspecting the main gear sidebrace studs for cracks on certain The New Piper Aircraft, Inc. (Piper) PA24, PA28R, PA30, PA32R, PA34, and PA39 series airplanes, and replacing any cracked main gear sidebrace stud. This AD retains the repetitive inspection and possible replacement requirements of AD 95-20-07; specifies in the ``Applicability'' section of the AD that certain Model PA34-200T airplanes could contain a certain main gear sidebrace assembly configuration that is not affected; and incorporates additional modification and replacement options. This AD results from additional information received by the Federal Aviation Administration (FAA) after the issuance of AD 95-20-07 on the design and service history of the affected airplanes concerning this subject. The actions specified by this AD are intended to prevent a main landing gear collapse caused by main gear sidebrace stud cracks, which could result in loss of control of the airplane during landing operations.
February 7, 1997.
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.
Federal Register
Vol. 62, no. 1
Office of the Federal Register, National Archives and Records Administration
1997-01-02
continuing
daily
deposited
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312 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-1997-01-02
P0b002ee180a348bf
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr02ja97
https://www.govinfo.gov/app/details/FR-1997-01-02
https://www.govinfo.gov/content/pkg/FR-1997-01-02/pdf/FR-1997-01-02.pdf
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299
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2010-09-24
2023-05-06
FR-1997-01-02
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FR
FR-1997-01-02
62
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