2022-19-07: Pitot/Static System

1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2022-19-07 Piaggio Aviation S.p.A.: Amendment 39-22176; Docket No. FAA-2022-0452; Project Identifier MCAI-2021-01356-A. (a) Effective Date This airworthiness directive (AD) is effective November 3, 2022. (b) Affected ADs None. (c) Applicability This AD applies to Piaggio Aviation S.p.A. Model P-180 airplanes, all serial numbers (S/Ns), certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code 3411, Pitot/Static System. (e) Unsafe Condition This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as accumulation of water and subsequent freezing in the pitot-tube. The FAA is issuing this AD to prevent blockage of the pitot-tube. The unsafe condition, if not addressed, could result in temporary air data indications failure, which could result in loss of control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions (1) For all airplanes: Within 30 days after the effective date of this AD, revise the existing airplane flight manual (AFM) for your airplane by adding into the Emergency Procedures and Normal Procedures sections the information in Piaggio Aviation P.180 AVANTI Temporary Change No. 36, dated April 11, 2019; or by incorporating into the Limitations and Normal Procedures sections the information in Piaggio Aviation P.180 Avanti II/EVO Temporary Change No. 79, dated September 17, 2018; as applicable to your airplane S/N. Using a different document with language identical to that in Piaggio Aviation P.180 AVANTI Temporary Change No. 36, dated April 11, 2019; or Piaggio Aviation P.180 Avanti II/EVO Temporary Change No. 79, dated September 17, 2018; is acceptable for compliance with this requirement. (2) For airplanes identified in paragraph (g)(2)(i) and (ii) of this AD: Within 660 hours time-in-service (TIS) after the effective date of this AD or 24 months after the effective date of this AD, whichever occurs first, modify the total air temperature (TAT) probe heater electrical circuit by following the Accomplishment Instructions, paragraphs (6) through (27), in Piaggio Aero Industries S.p.A. A.S. Service Bulletin No. 80-0457, Revision 1, dated February 12, 2020. (i) S/N 1105, if Piaggio Aero Industries Service Bulletin No. 80-0454, Revision 0, dated March 6, 2017, is not incorporated. (ii) S/Ns 1106 through 1234 inclusive, if Piaggio Aero Industries S.p.A. Service Bulletin No. 80-0425 up to Revision 2 is not incorporated. (3) For airplanes identified in paragraphs (g)(3)(i) through (iii) of this AD: Within 660 hours TIS after the effective date of this AD or 24 months after the effective date of this AD, whichever occurs first, modify the TAT probe heater electrical circuit by following the Accomplishment Instructions, Paragraphs (6) through (21), in Piaggio Aviation S.p.A. Service Bulletin No. 80-0430, Revision 1, dated April 30, 2019, or Accomplishment Instructions, paragraphs (6) through (21) and (25), in Piaggio Aero Industries S.p.A. in A.S. Service Bulletin No. 80-0430, Revision 2, dated July 20, 2021. (i) S/Ns 1002, 3001, 3003, 3004, 3006, and 3007. (ii) S/N 1105, if Piaggio Aero Industries Service Bulletin No. 80-0454, Revision 0, dated March 6, 2017, is incorporated. (iii) S/Ns 1106 through 1234 inclusive, if Piaggio Aero Industries S.p.A. Service Bulletin No. 80-0425 up to Revision 2 is incorporated. (h) Credit for Previous Actions This paragraph provides credit for the modification required by paragraph (g)(3) of this AD, if the modification was done before the effective date of this AD using Piaggio Aero Industries S.p.A. Service Bulletin No. 80-0430, Revision 0, dated August 10, 2017. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in paragraph (j)(1) of this AD and email to: 9-AVS-AIR-730-AMOC@faa.gov . (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (j) Related Information (1) For more information about this AD, contact Mike Kiesov, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 901 Locust, Room 301, Kansas City, MO 64106; phone: (816) 329-4144; email: mike.kiesov@faa.gov . (2) Refer to European Union Aviation Safety Agency (EASA) AD 2019-0144, dated June 19, 2019, for more information. You may examine the EASA AD in the AD docket at regulations.gov by searching for and locating Docket No. FAA-2022-0452. (k) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Piaggio Aviation S.p.A. Service Bulletin No. 80-0430, Revision 1, dated April 30, 2019. (ii) Piaggio Aero Industries S.p.A. in A.S. Service Bulletin No. 80-0430, Revision 2, dated July 20, 2021. (iii) Piaggio Aero Industries Service Bulletin S.p.A. A.S. No. 80-0457, Revision 1, dated February 12, 2020. (iv) Piaggio Aviation P.180 AVANTI II/EVO Temporary Change No. 79, dated September 17, 2018. (v) Piaggio Aviation P.180 AVANTI Temporary Change No. 36, dated April 11, 2019. (3) For service information identified in this AD, contact Piaggio Aero Industries S.p.A, P180 Customer Support, Via Pionieri e Aviatori d'Italia, snc-16154 Genoa, Italy; phone: (+39) 331 679 74 93; email: technicalsupport@piaggioaerospace.it . (4) You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email: fr.inspection@nara.gov, or go to: www.archives.gov/federal-register/cfr/ibr-locations.html . Issued on September 6, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022-20957 Filed 9-28-22; 8:45 am]BILLING CODE 4910-13-P