[Federal Register Volume 64, Number 123 (Monday, June 28, 1999)] [Unknown Section] [Pages 34523-34525] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 99-15924] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 97-ANE-36-AD; Amendment 39-11206; AD 97-21-01 R1] RIN 2120-AA64 Airworthiness Directives; MT-Propeller Entwicklung GMBH Model MTV-3-B-C Propellers AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: This amendment revises an existing airworthiness directive (AD), applicable to MT-Propeller Entwicklung GMBH Model MTV-3-B-C propellers, that currently requires initial and repetitive dye penetrant or eddy current inspections for cracks in the propeller hub, and rework of the propeller hub or replacement with a new model propeller hub. This amendment allows the repetitive dye penetrant inspections to be performed on-wing as opposed to at approved propeller repair stations, and to mark B-050 propeller hubs that have been modified in accordance with [[Page 34524]] the current AD or this revision. This amendment is prompted by issuance of a revised service bulletin that describes procedures for on-wing inspections. The actions specified by this AD are intended to detect and prevent propeller hub cracks, which could result in propeller blade separation and possible loss of control of the airplane. DATES: Effective August 27, 1999. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of August 27, 1999. ADDRESSES: The service information referenced in this AD may be obtained from MT-Propeller Entwicklung GMBH, Airport Straubing- Wallmuhle, D-94348 Atting, Germany; telephone (0 94 29) 84 33, fax (0 94 29) 84 32, Internet: ``[email protected]''. This information may be examined at the Federal Aviation Administration (FAA), New England Region, Office of the Regional Counsel, 12 New England Executive Park, Burlington, MA; or at the Office of the Federal Register, 800 North Capitol Street, NW, 7th Floor, suite 700, Washington, DC. FOR FURTHER INFORMATION CONTACT: Terry Fahr, Aerospace Engineer, Boston Aircraft Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7155, fax (781) 238-7199. SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) by revising airworthiness directive (AD) 97-21-01, Amendment 39-62 FR 52225, October 7, 1997), which is applicable to MT-Propeller Entwicklung GMBH Model MTV-3-B-C propellers, was published in the Federal Register on December 1, 1998 (63 FR 66078). The action proposed to allow repetitive dye penetrant inspections to be performed on-wing as opposed to at approved propeller repair stations, and to mark B-050 propeller hubs that have been modified in accordance with the current AD or this revised AD. Interested persons have been afforded an opportunity to participate in the making of this amendment. No comments were received on the proposal or the FAA's determination of the cost to the public. The FAA has determined that air safety and the public interest require the adoption of the rule as proposed. There are approximately 122 propellers of the affected design in the worldwide fleet. The FAA estimates that 57 propellers installed on aircraft of U.S. registry will be affected by this AD, that it will take approximately 5 work hours per propeller to accomplish the required actions, and that the average labor rate is $60 per work hour. Based on these figures, the total cost impact of the AD on U.S. operators is estimated to be $17,100. The regulations adopted herein will not have substantial direct effects on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. Therefore, in accordance with Executive Order 12612, it is determined that this final rule does not have sufficient federalism implications to warrant the preparation of a Federalism Assessment. For the reasons discussed above, I certify that this action (1) is not a ``significant regulatory action'' under Executive Order 12866; (2) is not a ``significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. A final evaluation has been prepared for this action and it is contained in the Rules Docket. A copy of it may be obtained from the Rules Docket at the location provided under the caption ADDRESSES. List of Subjects in 14 CFR Part 39 Air Transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. 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 Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 2. Section 39.13 is amended by removing Amendment 39-10154 (62 FR 52225, October 7, 1997) and by adding a new airworthiness directive, Amendment 39-11206, to read as follows: 97-21-01 R1 MT-Propeller Entwicklung GMBH: Amendment 39-11206. Docket 97-ANE-36-AD. Revises AD 97-21-01, Amendment 39-10154. Applicability: MT-Propeller Entwicklung GMBH Model MTV-3-B-C/ L250-21 propellers. These propellers are installed on but not limited to Sukhoi 29 aircraft. Note 1: This airworthiness directive (AD) applies to each propeller identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For propellers that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (c) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it. Compliance: Required as indicated, unless accomplished previously. To prevent propeller hub cracks, which could result in propeller blade separation and possible loss of control of the airplane, accomplish the following: (a) Within 50 hours time-in-service (TIS) after the effective date of this AD, accomplish the following: (1) Perform an initial dye penetrant or eddy current inspection of propeller hub, part number (P/N) B-050 or A-909-A, in accordance with paragraph (a) of MT-Propeller Entwicklung GMBH Service Bulletin (SB) No. 12C, dated March 4, 1998. The dye penetrant inspection may be done on-wing, but the eddy current inspection must be performed in an FAA-approved propeller repair station. (2) If the propeller hub is found to be cracked, prior to further flight, remove the existing propeller hub and replace with a serviceable propeller hub. (3) Rework propeller hubs, P/N B-050, by chamfering the hub bore to 0.08 inch x 45 degrees (for further information, see Detail Y of MT-Propeller Entwicklung GMBH SB No. 12C, dated March 4, 1998). Mark hubs that have been reworked in accordance with AD 97-21-01, or this revised AD, with the letters SB12C using a metal impression stamp (1/8 inch round bottom characters) above the propeller hub serial number and part number, located in the transition area between propeller blades 1 and 2 and the pitch change cylinder. (b) Thereafter, perform dye penetrant or eddy current inspections, in accordance with paragraph (a) of MT-Propeller Entwicklung GMBH SB No. 12C, dated March 4, 1998. The dye penetrant inspection may be done on-wing, but the eddy current inspection must be performed in an FAA-approved propeller repair station: (1) For propellers with hubs, P/N B-050, inspect at intervals not to exceed 50 hours TIS, or 6 months since last inspection, whichever occurs first. (2) For propellers with hubs, P/N A-909-A, inspect at intervals not to exceed 200 hours TIS, or 12 months since last inspection, whichever occurs first. (3) If the propeller hub is found to be cracked, prior to further flight, remove the existing propeller hub and replace with a serviceable propeller hub. (c) An alternative method of compliance or adjustment of the compliance time that [[Page 34525]] provides an acceptable level of safety may be used if approved by the Manager, Boston Aircraft Certification Office. Operators shall submit their requests through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Boston Aircraft Certification Office. Note 2: Information concerning the existence of approved alternative methods of compliance with this airworthiness directive, if any, may be obtained from the Boston Aircraft Certification Office. (d) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the aircraft to a location where the inspection requirements of this AD can be accomplished. (e) The actions required by this AD shall be accomplished in accordance with the following MT-Propeller Entwicklung GMBH SB: ------------------------------------------------------------------------ Document No. Pages Date ------------------------------------------------------------------------ 12C............................... 1-3 March 4, 1998. Total pages: 3. ------------------------------------------------------------------------ This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from MT-Propeller Entwicklung GMBH, Airport Straubing-Wallmuhle, D-94348 Atting, Germany; telephone (0 94 29) 84 33, fax (0 94 29) 84 32, Internet: ``[email protected]''. Copies may be inspected at the FAA, New England Region, Office of the Regional Counsel, 12 New England Executive Park, Burlington, MA; or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC. (f) This amendment becomes effective on August 27, 1999. Issued in Burlington, Massachusetts, on June 16, 1999. Jorge Fernandez, Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 99-15924 Filed 6-25-99; 8:45 am] BILLING CODE 4910-13-P