[4910-13-P] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2013-0447; Directorate Identifier 2013-NE-17-AD; Amendment 39-17536; AD 2013-15-20] RIN 2120-AA64 Airworthiness Directives; General Electric Comp any Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: We are superseding emergency airw orthiness directive (AD) 2013-14-51 for General Electric Company (GE) GE90-110B 1 and GE90-115B turbofan engines with affected transfer gearbox assembly (TGB ) radial gearshafts installed. AD 2013-14-51 was sent previously to all known U.S. ow ners and operators of GE90-110B1 and GE90- 115B turbofan engines. AD 2013- 14-51 prohibited operation of an airplane if more than one installed engine has an affected TGB ra dial gearshaft. This AD contains the same prohibition as AD 2013-14-51 and al so prohibits operation of a ny airplane 60 days after the effective date of this new AD if any in stalled engine has an affected TGB radial gearshaft. This new AD also revises the applicability by adding GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B, and GE90-113B tu rbofan engine models and adds a mandatory terminating action. This new AD was prompted by reports of three failures of TGB radial gearshafts which resulted in in-f light shutdowns (IFSDs). We are issuing this new AD to prevent failure of the TGB radial ge arshaft, which could result in IFSD of one or more engines, loss of thrust co ntrol, and damage to the airplane. DATES: This AD is effective [INSER T DATE 15 DAYS AFTER DATE OF PUBLICATION IN THE FEDERAL REGISTER].2 We must receive any comments on this AD by [INSERT DATE 45 DAYS AFTER DATE OF PUBLICATION IN THE FEDERAL REGISTER]. ADDRESSES: You may send comments by any of the following methods: • Federal eRulemaking Portal: Go to http://www.regulations.gov . Follow the instructions for submitting comments. • Fax: 202-493-2251. • Mail: U.S. Department of Transpor tation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. • Hand Delivery: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W 12-140, 1200 New Jersey Avenue SE., Washington, DC 20590, between 9 a.m. a nd 5 p.m., Monday through Friday, except Federal holidays. For service information identified in th is AD, contact General Electric Company, One Neumann Way, Room 285, Cincinnati, OH; phone: 513-552-3272; email: geae.aoc@ge.com. You may view this serv ice information at the FAA, Engine & Propeller Directorate, 12 New England Ex ecutive Park, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov ; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.3 FOR FURTHER INFORMATION CONTACT: Carlos Fernandes, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7189; fax: 781-238- 7199; email: carlos.fernandes@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion On May 16, 2013, we issued emergenc y AD 2013-10-52 (issued on June 16, 2013, as a Final Rule, Request for Comments (78 FR 38195, June 26, 2013)), which was immediately effective to owners and ope rators of GE GE90-110B1 and GE90-115B turbofan engines. That AD resulted from reports of two failures of TGB radial gearshafts that resulted in IFSDs. That AD prohibited operation of an ai rplane with affected TGBs installed on both engines. On July 12, 2013, we issued emergency AD 2013-14-51, superseding AD 2013- 10-52 (78 FR 38195, June 26, 2013). AD 2013-14-51 also prohibits operation of an airplane with affected TGB radial gearsh afts installed on both engines. AD 2013-14-51 resulted from a report of an additional failure of a TGB radial gearshaft, outside the population identified in AD 2013-10-52. We issued ADs 2013-10-52 and 2013-14-51 to prevent failure and separation of the TGB radial gearshaft, which could result in IFSD of one or more engines, loss of thrust control, and damage to the airplane.
Actions Since AD 2013-14-51 was Issued Since we issued emergency AD 2013-14-51, dated July 12, 2013, we determined that airplanes with an installed engine with an affected TGB radial gearshaft should not be allowed to operate more than 60 days after the effective date of this new AD. We also revised the Applicability of this new AD si nce we determined that the affected TGB radial gearshafts are installed on additio nal GE90 engine models besides the GE90-4 110B1 and GE90-115B. We also determined the need to add a mandatory terminating action.
Relevant Service Information We reviewed GE GE90-100 Series Aler t Service Bulletin (ASB) No. GE90-100 S/B 72-A0568, dated July 10, 2013; GE GE90-1 00 Series Service Bulletin (SB) No. GE90-100 S/B 72-0569, Revision 0, dated July 19, 2013; and GE GE90 SB No. GE90 S/B 72-1091, Revision 0, dated June 11, 2013, which provide additional information regarding the affected TGB radi al gearshafts. We also revi ewed GE GE90-100 Series SB No. GE90-100 S/B 72-0563, Revision 0, dated June 21, 2013, and Revision 1, dated July 10, 2013; and GE GE90 SB No. GE90 S/B 72-1066, Revision 0, dated June 21, 2013; which provide information regarding the mandatory terminating action.
FAA’s Determination We are issuing this AD because we eval uated all the relevant information and determined the unsafe condition de scribed previously is likely to exist or develop in other products of the same type design. AD Requirements This AD prohibits operation of an airplane with affected TGB radial gearshafts installed on both engines after the effective date of this AD. This AD also prohibits operation of an airplane with affected TGB ra dial gearshafts installed on any engine 60 days after the effective date of this AD. This AD also adds a mandatory terminating action, namely, to install a TGB radial gear shaft that is eligib le for installation.
FAA’s Justification and Determination of the Effective Date An unsafe condition exists that requires the immediate adoption of this AD. The FAA has found that the risk to the flying public justifie s waiving notice and comment prior to adoption of this ru le because of the before fu rther flight compliance time. Therefore, we find that notice and o pportunity for prior public comment are5 impracticable and that good cause exists for ma king this amendment effective in less than 30 days.
Comments Invited This AD is a final rule that involves re quirements affecting fl ight safety, and we did not provide you with notice and an opportun ity to provide your comments before it becomes effective. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include the docket number FAA-2013- 0447 and directorate identifier 2013-NE-17-AD at the beginning of your comments. We speci fically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD because of those

comments. We will post all comments we receive, without change, to http://www.regulations.gov , including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. Costs of Compliance We estimate that this AD will affect about 16 GE90 engines installed on airplanes of U.S. registry. We also estimate that it will take about eight hours per engine to replace the TGB radial gearshaft. The average labor rate is $85 per hour. The cost of this part is about $16,700. Based on these figures, we estimat e the total cost of this AD to U.S. operators to be $278,080. Authority for this Rulemaking Title 49 of the United States Code specifi es the FAA’s authority to issue rules on aviation safety. Subtitle I, Section 106, descri bes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency’s authority.6 We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, “General requirements.” Under that section, Congress charges the FAA with promo ting safe flight of civil aircraft in air commerce by prescribing regulations for pr actices, methods, and procedur es the Administrator finds necessary for safety in air commerce. This regu lation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect 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. For the reasons discussed above , I certify that this AD: (1) Is not a “significant regulator y action” under Executive Order 12866, (2) Is not a “significant rule” under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska to the extent that it justifies making a regulatory distinction, and (4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under th e criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safet y, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegate d to me by the Administrator, the FAA amends part 39 of the Federal Aviation Re gulations (14 CFR part 39) as follows:7 PART 39 - AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by: a. Removing AD 2013-10-52 (78 FR 38195, June 26, 2013); and b. Adding the following new AD: 2013-15-20: Amendment 39-17536; Docket No. FAA-2013-0447; Directorate Identifier 2013-NE-17-AD. (a) Effective Date This AD is effective [INSER T DATE 15 DAYS AFTER DATE OF PUBLICATION IN THE FEDERAL REGISTER]. (b) Affected ADs This AD supersedes Emergency AD 2013-14-51, Directorate ID 2013-NE-17- AD, dated July 12, 2013. This AD also removes AD 2013-10-52 (78 FR 38195, June 26, 2013) from the Code of Federal Regulations. (c) Applicability General Electric Company (GE) GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B, GE90-110B1, GE90-113B and GE90-115B turbofan engines with a transfer gearbox assembly (TGB) radial gearshaf t, part number (P/N) 1995M24P02, serial number (S/N) listed in Figure 1 to pa ragraph (c) of this AD, installed. Figure 1 to Paragraph (c) – TGB Ra dial Gearshaft P/N 1995M24P02 S/N’s
FIA0KCYG FIA0JETA FIA0H0VJ FIA0HL0C FIA0K63F FIA0J7V2 FIA0K62R FIA0HLY9 FIA0K3A3 FIA0KCYM FIA0K63C FIA0HL0E FIA0JVRE FIA0JJ6E FIA0K89H FIA0HL0F FIA0H0VM FIA0JNJH FIA0KCYK FIA0HL0G FIA0K3A4 FIA0K62W FIA0K3A5 FIA0HLY7 FIA0K62T FIA0K89P FIA0HWKA FIA0HJTE8 FIA0JJ53 FIA0JJ57 FIA0KCYR FIA0HJTJ FIA0K89W FIA0JJ56 FIA0HWKE FIA0HJTG FIA0KCW8 FIA0KH9Y FIA0J7WH FIA0HJTC FIA0K3A6 FIA0KCYP FIA0JER9 FIA0HJTF FIA0HY8C FIA0JJ55 FIA0JNJJ FIA0HJTH FIA0K3AP FIA0KH9G FIA0JVRR FIA0HJTA FIA0J7WG FIA0KH9H FIA0JNJM FIA0HJR9 FIA0JVRL FIA0KH9K FIA0KH9R FIA0HWJ7 FIA0J7V1 FIA0KH9C FIA0KH9P FIA0HY76 FIA0JVRM FIA0K63H FIA0K89C FIA0HY8F FIA0K3AV FIA0K63M FIA0JVRH FIA0H0VK FIA0J7V8 FIA0K62Y FIA0K89L FIA0J7VR FIA0J7WE FIA0JVP9 FIA0JER6 FIA0JJ58 FIA0K3A2 FIA0K63E FIA0JETH FIA0JJ6C FIA0K3A1 FIA0K3AY FIA0H0VC FIA0JNJF FIA0K3AN FIA0JVRT FIA0K3AL FIA0JNJK FIA0JVRP FIA0HY8E FIA0J7VV FIA0JVRC FIA0JJ6F FIA0HY8N FIA0J7VP FIA0J7V4 FIA0JJ6J FIA0J7V0 FIA0J7V9 FIA0JETF FIA0JVRV FIA0J7V3 FIA0HWJ8 FIA0HEG4 FIA0H0VL FIA0J7V5 FIA0H0VA FIA0HWJ9 FIA0K89T FIA0HY8H FIA0KCYL FIA0HWJ5 FIA0K89Y FIA0HEG2 FIA0HY79 FIA0HWJ6 FIA0JETL FIA0K62V FIA0KH9J FIA0J7VW FIA0JER8 FIA0HEGY FIA0HY8G FIA0J7VY FIA0J7WC FIA0HWKC FIA0HY8M FIA0J7VT FIA0JETE FIA0K3A0 FIA0HY8A FIA0J7WF FIA0K3AT FIA0JVRJ FIA0H0VG FIA0J7V6 FIA0JJ59 FIA0K8AA FIA0K3AR FIA0K89G FIA0K3AW FIA0KCYT FIA0JETC FIA0K89K FIA0JVRN FIA0KH9T FIA0KH9W FIA0K89R FIA0JNH8 FIA0HEG1 FIA0JNJC FIA0KCYJ FIA0JETN FIA0HEG3 FIA0K63L FIA0JJ6G FIA0HY78 FIA0J7WJ FIA0KCYN FIA0JJ6A FIA0HY75 FIA0JER7 FIA0JVRG FIA0HY8K FIA0HEG0 FIA0JVRF FIA0HY8L FIA0HLY6 FIA0KH9E FIA0K63K FIA0HY8J FIA0HLY0 FIA0KH9F FIA0J7WK FIA0H0VH FIA0HLY1 FIA0H0T9 FIA0JER5 FIA0H0VF FIA0HLY4 FIA0HLY3 FIA0JETM9 (d) Unsafe Condition This AD was prompted by reports of thr ee failures of TGB radial gearshafts which resulted in in-flight shutdowns (IFSDs). We are issuing this AD to prevent failure of the TGB radial gearshaft, which could result in IFSD of one or more engines, loss of thrust control, and damage to the airplane. (e) Compliance (1) Comply with this AD within the compliance times specified, unless already done. (2) Before further flight after the effec tive date of this AD, do not operate the airplane if more than one in stalled engine has a TGB radial gearshaft P/N and S/N listed in Figure 1 to paragraph (c) of this AD. (f) Mandatory Terminating Action No later than 60 days after the effective da te of this AD, as terminating action to the requirements of paragraph (e) of this AD, replace all TGB radial gearshafts identified in Figure 1 to paragraph (c) of this AD that are installed on an airp lane with TGB radial gearshafts that are elig ible for installation. (g) Prohibition on Operation Sixty days after the effective date of this AD, do not operate any airplane that has an engine installed that ha s a TGB radial gearshaft P/N and S/N listed in Figure 1 to paragraph (c) of this AD. (h) Definition For the purposes of this AD, a TGB radial gearshaft eligible for installation is: (1) A TGB radial gearshaft P/N a nd S/N, not listed in this AD or (2) A TGB radial gearshaft with an S/N listed in paragraph (c) of this AD with part number 1995M24P04, 2205M61P01 or 2205M61P02.10 (i ) Alternative Methods of Compliance (AMOCs) The Manager, Engine Certification Offi ce, FAA, may approve AMOCs for this AD. Use the procedures in 14 CFR 39.19 to make your request. ( j ) Related Information (1) For more information about this AD, contact Carlos Fernandes, Aerospace Engineer, Engine Certification Office, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7189; fax: 781-238-7199; email: carlos.fernandes@faa.gov

. (2) GE GE90-100 Series Alert Serv ice Bulletin No. GE90-100 S/B 72-A0568, Revision 0, dated July 10, 2013; GE GE90-100 Series Service Bulletin (SB) No. GE90- 100 S/B 72-0569, Revision 0, dated July 19, 2013; GE GE90-100 Series SB No. GE90- 100 S/B 72-0563, Revision 0, dated June 21, 2013, and Revision 1, dated July 10, 2013; GE GE90 SB No. GE90 S/B 72-1066, Revision 0, dated June 21, 2013; and GE GE90 SB No. GE90 S/B 72-1091, Revision 0, dated June 11, 2013, can be obtained from GE using the contact information in para graph (j)(3) of this AD. (3) For service information identified in this AD, contact General Electric Company, One Neumann Way, Room 285, Cincinnati, OH; phone: 513-552-3272; email: geae.aoc@ge.com. (4) You may view this service inform ation at the FAA, Engine & Propeller Directorate, 12 New England Executive Par k, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125. (k) Material Incorporated by Reference
None.11 Issued in Burlington, Ma ssachusetts, on July 25, 2013.

Frank P. Paskiewicz, Acting Director, Aircraft Certification Service.