Published 2012-10-17 · Federal Register document 2012-25254
Airworthiness Directives; Piaggio Aero Industries S.p.A.
Publication summary
We are rescinding an airworthiness directive (AD) for all Piaggio Aero Industries S.p.A Model P-180 airplanes. That AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. We issued that AD to prevent the brake hydraulic fluid from leaking because of the brake assembly rods contacting the brake valve tubing, which could result in the inability to adequately stop the airplane during ground operations. Since we issued that AD, we have determined this is no longer an unsafe condition and that regularly scheduled annual inspections address this subject.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:39.502075+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2012-08bffa249ae9a205
- Source row
- results[327]
- Raw source SHA-256
- 08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2000-07-11 R1
- Effective date printed in this edition
- 2012-11-21
Read 4 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) becomes effective November 21,
2012.
Exact source excerpt. Text positions 7499–7596, end exclusive, in the original decoded publication. SHA-256: 47e25a06dbb5d0e2ac23ab24cb5303de7714c9026219e5bb13ef92484b61e8fd
Affected ADs
(b) Affected ADs
This AD rescinds AD 2000-07-11 (65 FR 19305, April 11, 2000).
[[Page 63714]]
Exact source excerpt. Text positions 7596–7697, end exclusive, in the original decoded publication. SHA-256: 49208c87fee7bfc5781beab5a5a7a05a0335ad11355634a7265ea7c050cc2ec3
Applicability wording · Applicability
(c) Applicability
This AD applies to Piaggio Aero Industries S.p.A. Model P-180
airplanes, all serial numbers, certificated in any category.
Exact source excerpt. Text positions 7697–7845, end exclusive, in the original decoded publication. SHA-256: f6a0c4738df5a293bf084256edb18c8ceb6e39c3d3544b78abb3da4ccb219d9f
Subject
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 32; Landing Gear.
Exact source excerpt. Text positions 7845–7969, end exclusive, in the original decoded publication. SHA-256: b82646d13c29254af51cfa93ebd9a5fc3ab61a29d20a06c66d78b7ae88cd4283
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2000-07-11 R1 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: cea0bdaa1ff089cbee108bac838f53220e375700caf0f8547490908827852e04. Source manifest: 1762eacca4351cf22fbba99facd529dfc801a39ef70ad85c6dd10d3c56b5fa41.
Official source · 2012-10-17
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 77, Number 201 (Wednesday, October 17, 2012)]
[Rules and Regulations]
[Pages 63712-63714]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-25254]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0755; Directorate Identifier 99-CE-65-AD;
Amendment 39-17217; AD 2000-07-11 R1]
RIN 2120-AA64
Airworthiness Directives; Piaggio Aero Industries S.p.A.
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; rescission.
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[[Page 63713]]
SUMMARY: We are rescinding an airworthiness directive (AD) for all
Piaggio Aero Industries S.p.A Model P-180 airplanes. That AD was
prompted by mandatory continuing airworthiness information (MCAI)
issued by the airworthiness authority for Italy. We issued that AD to
prevent the brake hydraulic fluid from leaking because of the brake
assembly rods contacting the brake valve tubing, which could result in
the inability to adequately stop the airplane during ground operations.
Since we issued that AD, we have determined this is no longer an unsafe
condition and that regularly scheduled annual inspections address this
subject.
DATES: This AD is effective November 21, 2012.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at Document Management Facility, U.S.
Department of Transportation, Docket Operations, M-30, West Building
Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC
20590.
FOR FURTHER INFORMATION CONTACT: Mike Kiesov, Aerospace Safety
Engineer, FAA, Small Airplane Directorate, 901 Locust, Kansas City,
Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090; email:
[email protected].
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by rescinding AD 2000-07-11 (65 FR 19305, April 11, 2000) that
applies to the specified products. That NPRM was published in the
Federal Register on July 19, 2012 (77 FR 42454). The MCAI states:
After a 1999 training session during which conflicting inputs
were given to the brake pads between pilot and copilot, a brake
system rod was found deflected. The rod, in this bent condition,
could possibly wear and damage the tubings connected to the brake
valves, with consequent fluid leakage.
Prompted by these findings, PAI issued Service Bulletin (SB) 80-
0107, providing instructions for repetitive inspections of the
affected rods and tubings. As this was considered to be a
potentially unsafe condition, Registro Aeronautico Italiano (RAI),
the predecessor of ENAC (Ente Nazionale per l'Aviazione Civile),
issued Prescrizione di Aeronavigabilit[agrave] (PA) No. 1999-219,
which required the repetitive inspections as detailed in PAI SB 80-
0107 and, depending on findings, replacement of rod or tubing.
Since that AD was issued, the repetitive inspections of SB 80-
0107 have been included as regular tasks into the maintenance
schedule of both Avanti and Avanti II aeroplanes. In addition, no
other cases of brake system bent rods have been reported, nor have
any rods been replaced for damage in the P.180 fleet since that
occurrence. Based on the available information, this is no longer
considered to be an unsafe condition. Prompted by this
determination, PAI issued Revision ZZ of SB 80-0107, which cancels
the original SB 80-0107.
For the reasons described above, this Notice is issued to cancel
ENAC PA no. 1999-219 dated 03 May 1999.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (77 FR 42454, July 19,
2012) or on the determination of the cost to the public.
Conclusion
We reviewed the relevant data and determined that rescinding the AD
will not affect air safety and will reduce the burden on the public. We
will rescind the AD as proposed except for minor editorial changes. We
have determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (77 FR 42454, July 19, 2012) for correcting the unsafe condition;
and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (77 FR 42454, July 19, 2012).
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation in Alaska, and
(4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains the NPRM, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (telephone (800) 647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by removing airworthiness directive (AD)
2000-07-11, Amendment 39-11665 (65 FR 19305, April 11, 2000), and
adding the following new AD:
2000-07-11 R1 Piaggio Aero Industries S.p.A.: Amendment 39-17217;
Docket No. FAA-2012-0755; Directorate Identifier 99-CE-65-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective November 21,
2012.
(b) Affected ADs
This AD rescinds AD 2000-07-11 (65 FR 19305, April 11, 2000).
[[Page 63714]]
(c) Applicability
This AD applies to Piaggio Aero Industries S.p.A. Model P-180
airplanes, all serial numbers, certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 32; Landing Gear.
Issued in Kansas City, Missouri, on October 9, 2012.
Earl Lawrence
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2012-25254 Filed 10-16-12; 8:45 am]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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