2011-20-08: Modules and related connectors

Adoption of the Amendment Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (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. Section 39.13 is amended by adding a new airworthiness directive to read as follows: 2011-20-08 AGUSTA S.p.A.: Amendment 39-16819; Docket No. FAA-2011- 1036; Directorate Identifier 2010-SW-088-AD. Applicability: Models AB139 and AW139 helicopters, serial number (S/N) 31005 through S/N 31157 (except S/Ns 31007, 31094 and 31149) and S/N 41001 through S/N 41023, certificated in any category. Compliance: Within 30 hours time-in-service (TIS) or 30 days, whichever occurs earlier, unless done previously: To detect corrosion of certain modules, to preventthe display of misleading data to the flight crew, disengagement of the flight director modes of the autopilot or other alert system, increased workload of the flight crew, and subsequent loss of control of the helicopter, do the following: (a)(1) Remove the following items related to the Numbers 1 and 2 Modular Avionics Unit (MAU): (i) Power supply (PS) module, part number (P/N) 7024440-1901; (ii) Custom Input/Output (CSIO) module, P/N 7025410-1901; (iii) Control Input/Output (CIO) module, P/N 7026534-1902; (iv) MAU cabinet; and (2) Inspect the PS, CSIO, CIO, and MAU cabinet and all related connectors for corrosion. (i) If there is corrosion on a connector, before further flight, clean the connector. [[Page 68299]] (ii) If there is corrosion on a module, before further flight, replace the module with an airworthy module. (b) Modify the Number 2 MAU ventilation duct by following the Compliance Instructions, paragraphs 6 through 11, of Agusta Bollettino Tecnico No. 139-166, dated April 6, 2009 (BT). (c) Install and operationally test the Number 1 and Number 2 MAUs and the related PS module, CSIO module, CIO module, MAU cabinet, and all related connectors. (d) Reinstall the AFT right float assembly or the lower panel, P/N 3P5340A01631, whichever was removed during the modification process required by paragraph (b) of this AD. (e) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Contact the Manager, Safety Management Group, ATTN: George Schwab, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Safety Management Group, 2601 Meacham Blvd., Fort Worth, Texas 76137, telephone (817) 222-5114, fax (817) 222-5961. (f) The Joint Aircraft System/Component (JASC) Code is 3425: Navigation, Integrated Flight Director System. (g) Modifying the ventilation duct shall be done by following specified portions of Agusta Bollettino Tecnico No. 139-166, dated April 6, 2009. The Director of the Federal Register approved this incorporation by reference in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Agusta, Via Giovanni Agusta, 520 21017 Cascina Costa di Samarate (VA), Italy, telephone 39 0331-229111, fax 39 0331-229605/222595, or at http://customersupport.agusta.com/technical_advice.php. Copies may be inspected at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas, or 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. (h) This amendment becomes effective on November 21, 2011. Note: The subject of this AD is addressed in the European Aviation Safety Agency (Italy) AD No. 2010-0189, dated September 23, 2010.