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2010-23-01: Stabilizers

FAA order 2010-23-01 is an airworthiness directive in force since December 10, 2010. The FAA's subject line: Stabilizers. It names Piaggio Aero Industries Spa P180: about 57 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Piaggio Aero Industries S.p.A.
Models
P-180
On this site
Piaggio Aero Industries Spa P180 57 registered

Dates and paperwork

In force since
December 10, 2010
Published
November 5, 2010 (signed October 21, 2010)
Docket
FAA-2010-0778
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: Some cases of corrosion were detected in the interface between the elevator hinges fittings (metallic) and the horizontal stabilizer (carbon fibre); investigation identified the cause in galvanic corrosion between dissimilar materials. If left uncorrected, this situation could lead to a structural failure of the elevator, which could result in possible loss of control of the aeroplane. We are issuing this AD to require actions to correct the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (6,239 characters)
2010-23-01 Piaggio Aero Industries S.p.A.: Amendment 39-16490; Docket No. FAA-2010-0778; Directorate Identifier 2010-CE-034-AD. Effective Date (a) This airworthiness directive (AD) becomes effective December 10, 2010. Affected ADs (b) None. Applicability (c) This AD applies to Model PIAGGIO P-180 airplanes, serial numbers 1002 and 1004 through 1191, certificated in any category. Subject (d) Air Transport Association of America (ATA) Code 55: Stabilizers. Reason (e) The mandatory continuing airworthiness information (MCAI) states: Some cases of corrosion were detected in the interface between the elevator hinges fittings (metallic) and the horizontal stabilizer (carbon fibre); investigation identified the cause in galvanic corrosion between dissimilar materials. If left uncorrected, this situation could lead to a structural failure of the elevator, which could result in possible loss of control of the aeroplane. This AD requires: (1) Inspection of the hinges fittings for corrosion and of the stabilizer for delamination; (2) Repair of the stabilizer, if necessary; (3) Replacement of the fittings, if corroded; (4) Improvement of fittings installation; (5) Installation of aluminum strips in the stabilizer to improve bonding, in accordance with Piaggio Aero Industries (PAI) Service Bulletin (SB) 80-0262 Revision 2. Actions and Compliance (f) Unless already done, do the following actions: (1) Within the next 1,500 hours time-in-service (TIS) after December 10, 2010 (the effective date of this AD) or within 4 years after December 10, 2010 (the effective date of this AD), whichever occurs first, do the following: (i) Remove the left-hand (LH) and the right-hand (RH) elevators and do all of the inspections and corrective actions following the Accomplishment Instructions in Parts A, B, C, D, and E of PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (MANDATORY) N.: SB-80-0262, Revision 2, dated March 17, 2010. (ii) Reinstall the LH and RH elevators and do the final checks following the Accomplishment Instructions, Part F, of PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (MANDATORY) N.: SB-80-0262 Revision 2, dated March 17, 2010. (2) We will allow "unless already done'' credit for inspections and corrective actions already done, before the effective date of this AD, following PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletins (MANDATORY) N.: SB-80-0262, original issue dated September 24, 2009; or Revision 1 dated December 23, 2009, for compliance with the requirements of this AD. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (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 proceduresfound 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; e- mail: [email protected]. 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, a federal agency may not conduct or sponsor, and a person is not requiredto respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. Related Information (h) Refer to MCAI EASA AD No.: 2010-0124 (Correction: June 22, 2010), dated June 22, 2010; and PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin(MANDATORY) N.: SB-80-0262, Revision 2, dated March 17, 2010, for related information. Material Incorporated by Reference (i) You must use PIAGGIO AERO INDUSTRIES S.p.A. Service Bulletin (MANDATORY) N.: SB-80-0262, Revision 2, dated March 17, 2010, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Piaggio Aero Industries S.p.a., Via Cibrario, 4-16154 Genoa, Italy; phone: +39 010 6481 800; fax: +39 010 6481 374; e-mail: [email protected]; Internet: http://www.piaggioaero.com. (3) You may review copies of the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call 816-329-4148. (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.

Related safety bulletins advice on the same designs, not orders

2011-11-02CE-12-05 · Navigation: Water freezing in Pitot-Static System

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/2010-23-01.json · aircraft systems.