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2018-03-13 |
GENERAL ELECTRIC COMPANY: Amendment 39-19186; Docket No. FAA-2017-0943; Product Identifier 2017-NE-34-AD. |
(a) EFFECTIVE DATE This AD is effective February 28, 2018. (b) AFFECTED ADS None. (c) APPLICABILITY This AD applies to General Electric Company (GE) CT7-5A2, CT7-5A3, CT7-7A, CT7-7A1, CT7-9B, CT7-9B1, CT7-9B2, CT7-9C and CT7-9C3 model turboprop engines with main propeller shaft, part number 77581-11, in- stalled. (d) SUBJECT Joint Aircraft System Component (JASC) Code 7210, Turbine Engine Re- duction Gear. (e) UNSAFE CONDITION This AD was prompted by the failure of a main propeller shaft. We are issuing this AD to prevent failure of the main propeller shaft. The unsafe condition, if not addressed, could result in in-flight loss of the propeller, loss of engine thrust control, and damage to the air- plane. (f) COMPLIANCE Comply with this AD within the compliance times specified, unless al- ready done. (g) REQUIRED ACTIONS (1) For propeller gear boxes (PGBs) with 46,000 hours time since new (TSN) or more, perform cleaning, visual inspection and fluorescent-penetrant inspection (FPI) within 150 hours time in service (TIS) after the effective date of this AD, or one month after the effective date of this AD, whichever occurs first. (2) For PGBs with 40,000 hours TSN or more, but less than 46,000 hours TSN perform cleaning, visual inspection and FPI within 500 hours TIS after the effective date of this AD, not to exceed 46,150 TSN or four months after the effective date of this AD, whichever occurs first. (3) For PGBs with 30,000 hours TSN or more, but less than 40,000 hours TSN perform cleaning, visual inspection, and FPI within 1,000 hours TIS after the effective date of this AD, not to exceed 40,500 TSN or eight months after the effective date of this AD, whichever occurs first. (4) For PGBs with less than 30,000 hours TSN, perform cleaning, visual in- spection, and FPI at the next propeller removal, not to exceed 31,000 hour TSN. (5) Perform the cleaning, visual inspection and FPI, as follows: (i) Clean the main propeller shaft flange. Use the instructions in para- graph 5, "Main Propeller Shaft," in MM 72-10-00, PROPELLER GEARBOX - CLEANING from GE CT7B Maintenance Manual SEI-576, Rev. 60, dated October 1, 2017. (ii) Visually inspect the main propeller shaft for wear, corrosion, and cracking. Use the instructions in paragraph 5.A., "Main Propeller Shaft," in MM 72-10-00, PROPELLER GEARBOX – INSPECTION from GE CT7B Maintenance Manual SEI-576, Rev. 60, dated October 1, 2017. (iii) Spot-fluorescent-penetrant inspect the area on the main propeller shaft flange face within 0.5 inches radially adjacent to the dowel pin holes for cracks. Use the instructions in SPM 70-32-03, SPOT- FLUORESCENT PENETRANT-INSPECTION, Task 70-32-03-230-002 from GE GEK 9250, Commercial Engine Standard Practices Manual, Rev. 106, dated April 1, 2007. (6) Repeat the cleaning, visual inspection, and FPI of the main propeller shaft at each removal of the propeller. (7) Before further flight, remove from service any main propeller shaft found cracked, or with corrosion or wear beyond the limits specified in SPM 70-32-03, SPOTFLUORESCENT PENETRANT-INSPECTION, Task 70-32-03- 230-002, from GE GEK 9250, Commercial Engine Standard Practices Manual Rev. 106, dated April 1, 2007. (h) CREDIT FOR PREVIOUS ACTIONS Main propeller shafts that were replaced with new zero-time parts at an overhaul of the PGB within the last 10,000 hours TIS, or inspected in accordance with GE Service Bulletin (SB) CT7-TP S/B 72-0531, dated June 22, 2017, or GE SB CT7-TP S/B 72-0533, dated October 3, 2017, satisfy the requirements specified in paragraph (g)(5) of this AD. (i) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS) (1) The Manager, ECO 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 in- spector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ECO Branch, send it to the attention of the person identified in paragraph (j) of this AD. You may email your request to: ANE-AD-AMOC@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal in- spector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (j) RELATED INFORMATION For more information about this AD, contact Michael Richardson-Bach, Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7747; fax: 781-238-7199; email: michael. richardson-bach@faa.gov. (k) MATERIAL INCORPORATED BY REFERENCE (1) The Director of the Federal Register approved the incorporation by reference (IBR) 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) SPM 70-32-03, SPOT-FLUORESCENT PENETRANT INSPECTION, TASK 70-32-03-230 -002, from the GE Commercial Engine Standard Practices Manual GEK 9250 Rev. 106, dated April 01, 2007. (ii) MM 72-10-00, PROPELLER GEARBOX INSPECTION, from the GE CT7B Mainte- nance Manual SEI-576, Rev. 60, dated October 1, 2017. (iii) MM 72-10-00, PROPELLER GEARBOX – CLEANING, from the GE CT7B Mainte- nance Manual SEI-576, Rev. 60, dated October 1, 2017. (3) For GE service information identified in this AD, contact General Electric Company, GE-Aviation, Room 285, 1 Neumann Way, Cincinnati, OH 45215; phone: 513-552-3272; fax: 513-552-3329; email: geae.aoc@ge.com. (4) You may view this service information at FAA, Engine and Propeller Standards Branch, 1200 District Avenue, Burlington, MA 01803. For in- formation on the availability of this material at the FAA, call 781- 238-7759. (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, call 202 -741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr- locations.html. Issued in Burlington, Massachusetts, on February 8, 2018. Robert J Ganley, Acting Manager, Engine and Propeller Standards Branch, Aircraft Certifica- tion Service. FOR FURTHER INFORMATION CONTACT: Michael Richardson-Bach, Aerospace Engi- neer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7747; fax: 781-238-7199; email: michael.richardson-bach@faa.gov.
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DEPARTMENT OF TRANSPORTATION
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