AD 2009-21-08 R1

Historical

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

Effective
December 14, 2009
Published
January 7, 2010 · 75 FR 904–906
Issued
December 30, 2009
Supersedes
AD2009-21-08
Superseded by
AD2014-09-04
Model
P-180
Data sheet
TCDSA59EU
Registered aircraft
109 matched by model
Product
Aircraft · Small airplane
ATA chapter
32 · Landing gear
Amendment
39-16169
Docket
FAA-2009-0699 Directorate Identifier 2009-CE-042-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document E9-31364. Only the govinfo PDF is the legal edition. DRS record last changed August 7, 2025.

On this page

Summary

We are clarifying information contained in Airworthiness Directive (AD) 2009-21-08, which applies to PIAGGIO AERO INDUSTRIES S.p.A. (Piaggio) Model PIAGGIO P-180 airplanes. AD 2009-21-08 currently requires repetitive functional tests of the manifold system and replacement of any system that does not pass the functional tests ( i.e., movement of the steering system). The language in AD 2009-21-08 incorrectly references not passing the functional tests as “movement of the manifold,” and it should read “movement of the steering system” as specified in the service bulletin. The notice of proposed rulemaking (NPRM) referenced it as specified in the service bulletin. This document incorporates the intent of the action as already proposed in the NPRM. We are issuing this AD to prevent a potentially dangerous veer along the runway. The steering system must be in the `off' position during landing and takeoff (in this case when airspeed is higher than 60 knots) according to the aircraft flight manual limitations.

The airworthiness directive

2009-21-08 R1 PIAGGIO AERO INDUSTRIES S.p.A.: Amendment 39-16169; Docket No. FAA-2009-0699; Directorate Identifier 2009-CE-042-AD.

(a) Effective Date

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(a) The effective date of this AD is December 14, 2009, which is the same as AD 2009-21-08.

(b) Affected ADs

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(b) None.

(c) Applicability

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(c) This AD applies to Model PIAGGIO P-180 airplanes, all serial numbers (S/N), certificated in any category.

(d) Subject

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(d) Air Transport Association of America (ATA) Code 32: Landing Gear.

(e) Reason

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(e) The mandatory continuing airworthiness information (MCAI) states:

Some cases of uncommanded steering action were observed, while the steering system was switched off.

A leakage in the Steering Select/Bypass Valve, installed in the Steering Manifold, when closed, is suspected to have caused the uncommanded steering.

If left uncorrected, this condition could lead to a potentially dangerous veer along the runway; in fact, according to the Aircraft Flight Manual limitations, the steering system must be in `off' position during landing and takeoff (in this case when airspeed is higher than 60 knots). For the reasons stated above, this new AD mandates repetitive inspections for leakage of the Nose Landing Gear steering manifold.

The MCAI requires, if any inspection finds internal leakage of the steering manifold, the replacement of the steering manifold.

(f) Actions and Compliance

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(f) Unless already done, do the following actions:

(1) Within the next 6 months after December 14, 2009 (the effective date of this AD and AD 2009-21-08) or within the next 100 hours time-in-service (TIS) after December 14, 2009 (the effective date of this AD and AD 2009-21-08), whichever occurs first, and repetitively thereafter at intervals not to exceed every 165 hours TIS, do a functional test of the nose landing gear (NLG) steering manifold. Follow the accomplishment instructions of PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (Mandatory) N. 80-0249 (includes CONFIRMATION SLIP), Rev. 1, dated May 27, 2009.

(2) Upon installation of a NLG steering manifold on any airplane, do a functional test of the NLG steering manifold. Repetitively thereafter at intervals not to exceed every 165 hours TIS, do a functional test of the NLG steering manifold. Follow the accomplishment instructions of PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (Mandatory) N. 80-0249 (includes CONFIRMATION SLIP), Rev. 1, dated May 27, 2009.

(3) If during any inspection required in paragraphs (f)(1) and (f)(2) of this AD, any manifold system does not pass the functional tests ( i.e., movement of the steering system), using the compliance times in the accomplishment instructions of PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (Mandatory) N. 80-0249 (includes CONFIRMATION SLIP), Rev. 1, dated May 27, 2009, replace the NLG steering manifold following (for S/N 1004 through 1104) pages 1 through 8 dated March 1, 2006; 201, 202, 204, and 206 through 216, dated June 16, 2008; 203 and 205, dated March 1, 2006; and 501 through 506, dated March 1, 2006, of PIAGGIO AERO PIAGGIO P.180 AVANTI Maintenance Manual, Report No. 9066, 32-50-00, Revision No. D2, revised June 16, 2008; or (for S/N 1105 and greater) pages 1 through 8, dated June 30, 2005; 201, 202, and 207 through 209, dated December 19, 2008; 203 and 205, dated June 30, 2005; 204, 206, and 210 through 216, dated September 14, 2007; and 501 through 506, dated June 30, 2005, of PIAGGIO AERO PIAGGIO P.180 AVANTI II Maintenance Manual, Report No. 180-MAN-0200-01105, 32-50-00, Revision No. A3, revised December 19, 2008.

FAA AD Differences

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Note:

This AD differs from the MCAI and/or service information as follows: No differences.

(g) Other FAA AD Provisions

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(g) The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Sarjapur Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4145; fax: (816) 329-4090. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.

(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service.

(3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056.

(h) Related Information

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(h) Refer to MCAI EASA AD 2009-0129, dated June 19, 2009; PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (Mandatory) N. 80-0249 (includes CONFIRMATION SLIP), Rev. 1, dated May 27, 2009; PIAGGIO AERO PIAGGIO P. 180 AVANTI Maintenance Manual, Report No. 9066, 32-50-00, revised June 16, 2008, pages 1 through 8, 201 through 216, and 501 through 506; and PIAGGIO AERO PIAGGIO P. 180 AVANTI II Maintenance Manual, Report No. 180-MAN-0200-01105, 32-50-00, revised December 19, 2008, pages 1 through 8, 201 through 216, and 501 through 506, for related information.

(i) Material Incorporated by Reference

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(i) You must use the service information specified in Table 1 of this AD to do the actions required by this AD, unless the AD specifies otherwise.

(1) On December 14, 2009 (74 FR 57561, November 9, 2009), the Director of the Federal Register previously approved the incorporation by reference of the service information listed in Table 1 of this AD.

(2) For service information identified in this AD, contact Piaggio Aero Industries S.p.a., Via Cibrario, 4—16154 Genoa, Italy; telephone +39 010 06481 741; fax: +39 010 6481 309; Internet: http://www.piaggioaero.com, or e-mail: MMicheli@piaggioaero.it.

(3) You may review copies of the service information incorporated by reference for this AD at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the Central Region, call (816) 329-3768.

(4) You may also review copies of the service information incorporated by reference for this AD at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Table 1—Material Incorporated by Reference
Service information titlePage(s)RevisionDate
PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (Mandatory) N. 80-02491 through 9Rev. 1May 27, 2009.
PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (Mandatory) N. 80-0249CONFIRMATION SLIPRev. 1Not Dated.
PIAGGIO AERO PIAGGIO P. 180 AVANTI Maintenance Manual, Report No. 9066, 32-50-00CoverNo. D2Revised June 16, 2008.
PIAGGIO AERO PIAGGIO P. 180 AVANTI Maintenance Manual, Report No. 9066, 32-50-001 through 8Not ApplicableMarch 1, 2006.
PIAGGIO AERO PIAGGIO P. 180 AVANTI Maintenance Manual, Report No. 9066, 32-50-00201, 202, 204, and 206 through 216Not ApplicableJune 16, 2008.
PIAGGIO AERO PIAGGIO P. 180 AVANTI Maintenance Manual, Report No. 9066, 32-50-00203 and 205Not ApplicableMarch 1, 2006.
PIAGGIO AERO PIAGGIO P. 180 AVANTI Maintenance Manual, Report No. 9066, 32-50-00501 through 506Not ApplicableMarch 1, 2006.
PIAGGIO AERO PIAGGIO P. 180 AVANTI II Maintenance Manual, Report No. 180-MAN-0200-01105, 32-50-00CoverNo. A3Revised December 19, 2008.
PIAGGIO AERO PIAGGIO P. 180 AVANTI II Maintenance Manual, Report No. 180-MAN-0200-01105, 32-50-001 through 8Not ApplicableJune 30, 2005.
PIAGGIO AERO PIAGGIO P. 180 AVANTI II Maintenance Manual, Report No. 180-MAN-0200-01105, 32-50-00201, 202, and 207 through 209Not ApplicableDecember 19, 2008.
PIAGGIO AERO PIAGGIO P. 180 AVANTI II Maintenance Manual, Report No. 180-MAN-0200-01105, 32-50-00203 and 205Not ApplicableJune 30, 2005.
PIAGGIO AERO PIAGGIO P. 180 AVANTI II Maintenance Manual, Report No. 180-MAN-0200-01105, 32-50-00204, 206, and 210 through 216Not ApplicableSeptember 14, 2007.
PIAGGIO AERO PIAGGIO P. 180 AVANTI II Maintenance Manual, Report No. 180-MAN-0200-01105, 32-50-00501 through 506Not ApplicableJune 30, 2005.

Rule preamble

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

DatesPage 1

The effective date of this AD is December 14, 2009, which is the same as AD 2009-21-08.

As of December 14, 2009 (74 FR 57561, November 9, 2009), the Director of the Federal Register approved the incorporation by reference of the following documents listed in this AD:

AddressesPage 1

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 1

Sarjapur Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4145; fax: (816) 329-4090.

DiscussionPage 1

On October 7, 2009, we issued AD 2009-21-08, Amendment 39-16047 (74 FR 57561, November 9, 2009), to require repetitive functional tests of the manifold system and replacement of any system that does not pass the functional tests ( i.e., movement of the steering system) on Piaggio Model PIAGGIO P-180 airplanes.

The language in AD 2009-21-08 incorrectly references not passing the functional tests as “movement of the manifold,” and it should read “movement of the steering system” as specified in the service bulletin. The NPRM referenced it as specified in the service bulletin. This document incorporates the intent of the action as already proposed in the NPRM.

Consequently, the FAA sees a need to clarify AD 2009-21-08 to assure that the proper criteria are utilized for the required functional test and is revising the AD to incorporate the language discussed above and to add the amendment to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13).

Since this action only clarifies the intent of what was originally proposed in the NPRM, it has no adverse economic impact and imposes no additional burden on any person than was already proposed. Therefore, the FAA has determined that prior notice and opportunity for public comment are unnecessary.

Adoption of the amendmentPage 2

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

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

2. The FAA amends § 39.13 by removing Airworthiness Directive (AD) 2009-21-08, Amendment 39-16047 74 FR 57561, November 9, 2009), 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

NTSB investigations that cite this AD · 1

Their narratives or probable cause name AD 2009-21-08, often to say whether the aircraft complied with it.