Airworthiness directive · Landing Gear · Piaggio Aero Industries P-180

Effective
November 21, 2012
Published
October 17, 2012 · 77 FR 63712–63714
Issued
October 9, 2012
Supersedes
AD2000-07-11
Model
P-180
Data sheet
TCDSA59EU
Registered aircraft
109 matched by model
Product
Aircraft · Small airplane
ATA chapter
32 · Landing gear
Amendment
39-17217
Docket
FAA-2012-0755
Project
99-CE-65-AD
Issued as
Final rule; rescission

Unofficial copy from the Federal Register XML, document 2012-25254. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

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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.

The airworthiness directive

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

PDF page 2

This airworthiness directive (AD) becomes effective November 21, 2012.

(b) Affected ADs

PDF page 2

This AD rescinds AD 2000-07-11 (65 FR 19305, April 11, 2000).

(c) Applicability

PDF page 3

This AD applies to Piaggio Aero Industries S.p.A. Model P-180 airplanes, all serial numbers, certificated in any category.

(d) Subject

PDF page 3

Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 32; Landing Gear.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 2

This AD is effective November 21, 2012.

AddressesPage 2

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 contactPage 2

Mike Kiesov, Aerospace Safety Engineer, FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090; email: mike.kiesov@faa.gov.

DiscussionPage 2

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 Aeronavigabilità (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.

CommentsPage 2

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.

ConclusionPage 2

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:

• Are consistent with the intent that was proposed in the NPRM (77 FR 42454, July 19, 2012) for correcting the unsafe condition; and

• 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 RulemakingPage 2

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 findingsPage 2

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 DocketPage 2

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.

Adoption of the AmendmentPage 2

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

Adoption of the amendmentPage 2

1. The authority citation for part 39 continues to read as follows:

2. The FAA amends § 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:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 109

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Piaggio Aero Industries56 aircraft
  • Piaggio50 aircraft
  • Iam Piaggio S P A2 aircraft
  • Piaggio Aero Industries S P A1 aircraft
By year built
19902022
Registered aircraft by year built: 95 aircraft
19901
19914
19925
19961
20003
20015
20026
20035
20048
20056
20064
200713
200815
20096
20102
20114
20122
20131
20141
20171
20222

14 with no year recorded

By model

Aircraft

See all 109 aircraft