CFM56-72010 Component Repair Directory 01 Jan 2010 © Snecma | All rights reserved Standard terms & conditions of sale 1.0 Introduction These Standard Terms and Conditions of Sale of Engine Part/Component Repair Services of SNECMA SA (hereinafter called "SNECMA"), together with any terms and conditions, set forth in SNECMA' signed proposal ("Proposal") submitted to the customer identified in the Proposal ("Customer") and with the approved workscope shall be the only terms and conditions applicable to the provision by SNECMA of Services (as hereafter defined) for the repair (performed in accordance with OEM Engine Shop Manual or SNECMA Maintenance Manual), overhaul or servicing of the Engine part or component of Customer's aircraft engines, engine modules, engine module units, assemblies, subassemblies, controls and accessories, and the parts incorporated in any of those items thereof described in such Proposal (individually or collectively, as the case may be, the "Equipment"). The term "Service(s)" means the services which SNECMA agrees to perform as described in the Proposal and in the approved workscope (whether or not contained in the Proposal), including all labor and materials used by SNECMA in the performance thereof. These terms and conditions (“STCS”), together with the signed and accepted Proposal and with the approved workscope, shall be considered as the agreement between the parties and shall be in lieu of any and all terms and conditions of any purchase order or other document submitted by Customer except as specifically stated hereinafter. Pricing contained in these STCS are the prices available on the SNECMA Website, www.snecma.com, update regularly. SNECMA reserves the right to adjust pricing throughout the year for any business need including but not limited to correcting any pricing error that is identified following issuance of this these STCS. 2.0 Definitions Accessories: Fixed price including labour and material with exceptions (FOD, misused, fuel contamination, mishandling, major part bodies) AD or Airworthiness Directive shall mean a document issued by the Competent Aviation Authority having jurisdiction over the Equipment, identifying an unsafe condition relating to such Equipment and, as appropriate, prescribing inspections and the conditions and limitations, if any, under which the Equipment may continue to operate. Cleaning and Inspection costs and TAT are not included for the CRD dedicated to customer with Snecma Engine Overaul Contract but shall be added for CRD dedicated for isolated parts and accessories Business, packages or repairs. If part fails inspection, clean and serviceability fees apply. Any additional factory testing, inspection and packaging requirements of Customer shall be paid for by Customer. CLP or Catalog list Price shall mean the OEM’s current catalog or the OEM’s current list price pertaining to a new part or new item of Equipment. The term “current” as used in this definition means as of the time of providing such part or item during the applicable Service. Designated Repair Facility shall mean one or more of the repair facilities owned by SNECMA or its affiliates, which are certified by the Competent Aviation Authority to perform the applicable Service hereunder. A list of repair facilities currently owned or operated by SNECMA or its affiliates is set forth in Article 15 hereunder. The Services on the Equipment shall be performed at the repair facility designated in Customer’s Purchase Order as agreed by SNECMA. However, SNECMA has the right to change the Designated Repair Facility and to subcontract any Services to any other SNECMA repair facility, SNECMA-affiliated facility, or to any subcontractor selected by SNECMA, as long as such repair facility, SNECMA affiliated facility or subcontractor is certified and rated by the Competent Aviation Authority to perform the required Services on the Equipment. Material listed at CLP is sometimes requested by the ESM repair. This cost shall be added excepted if specified otherwise at CRD repair description. SB or Service Bulletin shall mean the document issued by an OEM to notify the engine’s operator of modifications, substitution of parts, special inspections, special checks, amendment of existing life limits or establishment of first-time life limits, or conversion of Equipment from one model to another. Turnaround Time (TAT) means the number of calendar days, between Delivery and Redelivery, required to complete repairs, exclusive of public holidays observed by the Designated Repair Facility, Excusable Delays, and any delays due to acts of Customer or failure to act by Customer. - The Turn Around Time shall begin the day SNECMA acknowledges receipt of the Equipment to be repaired in the Designated Repair Facility as evidenced by the date shown on the shipping documents or; from the date of acceptance by the Customer of SNECMA 's quotation as proven on the purchase order, whichever is the latest. - The Turn Around Time terminates the day of the notice advising the Customer that the component is ready for shipment or; when the component leaves the Designated Repair Facility to be returned to the Customer as evidenced by the date shown on the shipping documents, whichever occurs first, provided the notice of the Customer acceptation of the quotation and all necessary information for SNECMA to perform the repairs have been received by SNECMA on due time. To this effect the Customer shall provide with its purchase order or at SNECMA's request all relevant information to enable SNECMA to perform the Services. In case of disregard of the Customer’s obligations, TAT shall be modified accordingly. When all information is available to SNECMA and if the TAT has been exceeded by more than 50%, SNECMA shall consider providing standard exchange for the Equipment for which the Services was to be performed, which Equipment shall become the property of SNECMA. The price to be paid by the Customer shall be the price of Service of the initial Equipment. 3.0 General Procedure A. Following Delivery (as defined below) of the Equipment to SNECMA´ Designated Repair Facility, together with (1) a repair/purchase order from Customer authorizing such Service, (2) an approved workscope if any, and (3) all applicable Equipment records, SNECMA shall induct the Equipment and proceed with the Service described in the Proposal. SNECMA shall perform a standard receiving inspection of the Equipment and shall submit a workscope to Customer for approval, if not already defined in the Proposal. If Customer decides not to proceed with the Service, Customer shall immediately notify SNECMA in writing of its decision not to proceed and shall pay to SNECMA all costs and labor charges incurred in connection with the inspection of the Equipment, including, without limitation, preparation of inspection report(s), loose assembly and packing of the Equipment for return shipment. B. Following disassembly and/or inspection of the Equipment, SNECMA shall provide Customer with an estimate of the Redelivery (as defined below) date. C. Should SNECMA discover some additional work to be performed after approval of workscope by Customer, SNECMA shall so notify Customer and perform such additional work, which shall be embodied in the Services, at Customer expense unless Customer notifies SNECMA in writing within five (5) days of receiving such notification that Customer does not want such additional work to be performed. D Service shall be in accordance with SNECMA´ standard commercial quality control policies, procedures and practices. SNECMA shall determine which parts are required to repair the Equipment. These parts shall be charged to Customer under the terms and conditions set forth in Article 4 “Price” – “Mark up” below, unless specified in the SNECMA directory that the Services includes the primary parts. E. Serviced Equipment shall be prepared and packed in accordance with SNECMA' normal commercial practice unless otherwise specified in the Proposal. SNECMA agrees to comply with all reasonable written instructions of Customer as to markings to be placed on bills of lading, packing lists, correspondence and shipping containers. F. In connection with the Services provided on the Equipment, SNECMA shall provide Customer with copies of all work records required by the European Aviation Safety Agency ("EASA"), or, if applicable, the Federal Aviation Administration of the United States ("FAA"), or such other foreign equivalent aviation authority as agreed to in writing by SNECMA and Customer (each, a "Competent Aviation Authority"), including any required repair facility component/accessory tags. 4.0 Price All prices are shown in United States Dollars. They are valid until the next update of the prices. The Services described in this directory are only payable in U.S.$. Prices shall be as quoted by SNECMA to Customer in the Proposal or, if not, set forth in the Proposal, as published in SNECMA´ or other original equipment manufacturer's ("OEM") directories in effect at the time the item is allocated to, or incorporated in, Customer´s Equipment. SNECMA´ directories or other OEM directories are published once a year at least and is subject to evolution during a year, including without limitation creation of new repairs; such evolution shall be applicable immediately even if not published in the current SNECMA’ directories. © Snecma | All rights reserved 1/18 MATERIAL MARK UP Mark up on primary parts replacement will be 10 % over Original Engine Manufacturer (“O.E.M.”) directory price. Exchange fee is 7 % of the O.E.M. directory price on the part to be replaced if rotable parts are available. Transfer of title is effective after payment of the corresponding invoices. Serviceable parts will be supplied at 85 % of the directory price unless otherwise agreed by the Parties. CUSTOMER DEROGATION REQUEST (“CDR”) Customer will be charged for any Customer's Derogation Request on a part a management fee equivalent to 2% of the OEM directory price of said part, such fee being not less than $ 200. This management fee does not include labor and part. The referring prices applied in the quotations are the prices available in the SNECMA web site www.snecma.com updated regularly 5.0 Delivery, Redelivery, Title and Governmental Authorization A. Customer's Equipment shall be Delivered Duty Paid ("DDP") to SNECMA' Designated Repair Facility pursuant to International Chamber of Commerce "Incoterms" (2000 Edition) ("Delivery"). SNECMA shall redeliver the Equipment to Customer, Ex Works, in SNECMA' Designated Repair Facility pursuant to "Incoterms" (2000 Edition) ("Redelivery"). Incoterms : - including transport packaging required for the return of the repaired component to the Customer (packaging shall be in accordance with SNECMA normal commercial practice). It excludes specific packaging or shuttle ones that would not insure proper protection during the return shipment. - including SNECMA usual tests and inspections unless otherwise specified in the directory. - not including any transportation and charges related to transportation. - not including the price of the parts, if required for the repair, unless otherwise specified in writing by SNECMA. Parts needed to perform the repairs shall be furnished by SNECMA and deemed to have been sold to the Customer, the replaced primary part to be scrapped by SNECMA. The transfer of title shall take place at the same time as the transfer of risk. These Incoterms are valid insofar no contrary quotation or notice shall have been made by SNECMA after receipt of the Equipment to be repaired. B. Title to SNECMA furnished parts, material and associated labor shall pass to Customer upon the first to occur of incorporation in the Equipment, and simultaneously, title to parts removed from the Equipment shall pass to SNECMA. Without further act or obligation on the part of the Customer, SNECMA shall dispose of all scrapped or condemned parts removed from the Equipment. C. If Equipment cannot be Redelivered when ready due to any cause referred to in Article 8 "Excusable Delay", below, SNECMA may place such Equipment into storage. In such event, SNECMA shall notify Customer of such storage, SNECMA' Redelivery obligations shall be deemed fulfilled and all risk of loss or damage to the Equipment shall pass to Customer on the date of such storage. Any amounts otherwise payable to SNECMA upon Redelivery shall be payable upon presentation of SNECMA' invoice. Promptly upon submission of SNECMA' invoice, Customer shall reimburse SNECMA for all expenses incurred by SNECMA, including, but not limited to, preparation for and placement into storage, handling, inspections, preservation and insurance of the Equipment. Upon payment to SNECMA of all amounts due hereunder, SNECMA shall assist and cooperate with Customer in the removal of any Equipment which has been placed in storage. D. Customer shall be the importer or exporter of record of the Equipment and, unless otherwise specifically agreed to in writing by the parties, Customer shall be responsible for obtaining import licenses, export licenses, exchange permits and any other required governmental authorizations. At Customer's request and expense, SNECMA will assist Customer in obtaining any required approval but shall not be liable if any authorization is delayed, denied, revoked, restricted or not renewed, and Customer shall not be relieved of its obligation to pay SNECMA for Services and any other charges which are the obligation of the Customer hereunder. All items (including technical data) delivered hereunder shall at all times be subject to (i) the U.S. Export Administration Regulations and/ or the International Traffic in Arms Regulations and (ii) the French Export Administration Regulations and applicable customs regulations of France and (iii) any other foreign government export control regulations.. Customer agrees not to dispose of U.S. or French origin items (including technical data) provided by SNECMA under these STCS other than in and to the country of ultimate destination specified in Customer's purchase order, approved government license(s) or authorization(s), except as said laws and regulations may permit. 6.0 Invoices and Payment A. SNECMA shall provide Customer with a budgetary estimate of the costs to perform Services and shall issue a preliminary invoice to be paid by Customer before Redelivery of the Equipment. Any quotation or cost estimate is provided and accepted by Customer only as a budgetary estimate, solely for the purpose of guidance and not for reliance. SNECMA shall issue a final invoice for Services as soon as practicable after completion of the Services. The final invoice shall reflect the total charges owed by Customer and credits due Customer and shall reflect any additional charges or credits to the preliminary invoice incurred (if any), based on actual charges to complete the Services. Such invoice shall be reconciled with any preliminary invoice. Unless otherwise stated in the Proposal, the unpaid balance of any preliminary invoice for Services shall be payable in full prior to Redelivery of the Equipment. Customer shall pay the final invoice at receipt. If any payment date falls on a day that is not a business day, the payment that is otherwise due shall instead be due the next business day. Timely payment by Customer shall be of the essence of these STCS and SNECMA reserves the right to require different terms of payment or other assurances of payment in the event Customer fails to make timely payments such as an advance payment of 100% of the estimated amount of the works and parts. The remainder at receipt of invoice. The invoice will be deemed to be received no later than seven (7) days from date of issue. B. Customer shall make all payments under these STCS in United States Dollars via wire transfer to the bank account designated on the Proposal. Such payment shall be immediately available for use and without any right to withhold or to make any deduction whatsoever unless accepted by SNECMA or affirmed by the competent court as per article 13, Paragraph A. C. SNECMA shall have the right, in addition to all other rights and remedies afforded to it under these STCS or by law, to suspend performance of its obligations under these STCS should Customer default in the performance of its obligations under this article, and to charge Customer for the corresponding costs associated with the work stoppage. D. If Customer is in default of any payment obligation, SNECMA is without reminder and prejudice to any other rights entitled to charge interest at Libor 3 month plus 4% for any outstanding sum, beginning with any due date of payment. E. Customer hereby grants to SNECMA a security interest in any property owned by Customer (including Customer´s beneficial rights to property leased by Customer) in the possession of SNECMA or any of SNECMA´ affiliates, at any time, to secure all amounts owed by Customer to SNECMA under these STCS. F. For each final invoice, Customer will be charged at least a lumpsum of 150$ regardless of the repair price. 7.0 Taxes A. Any taxes of any nature levied exclusively in connection with transactions hereunder, whether levied against Customer or Snecma, shall be borne, and to the extent permitted by law, paid directly by the Customer to the relevant authority. If Snecma is required by law or otherwise to pay any such taxes, including any related penalties and interest, the amount of the payment so made by Snecma shall be reimbursed by Customer to Snecma upon submission of Snecma’s invoices. Customer will use all reasonable effort to obtain a refund thereof. If all or any part of any taxes be refund to Snecma, Snecma will repay Customer such part thereof as Customer will have paid or reimbursed to Snecma. B. Withholding - All payments to be made by Customer to Snecma under this agreement shall be free of all withholding of any nature whatsoever except to the extent otherwise required by law; and if any such withholding is so required, Customer will: - Promptly notify Snecma; and - Forthwith pay to Snecma such additional amount necessary to ensure that, after the making of such deduction or withholding, Snecma receives and retains a net amount equal to the full amount which it would have received had no such deduction or withholding been made or required to be made; and; - Pay the full amount required to be deducted or withheld to the relevant taxation authority within the time allowed for such payment under applicable law; and - Provide Snecma, in the same time of the payment, with a certificate of deduction of tax at source. If the aforesaid mechanism contravenes the law of [COUNTRY], the Parties shall amend this Agreement in order to increase the respective prices and mount envisioned by this Agreement so that the initial prices and amounts are preserved. C. Value Added and similar taxes - Transactions contemplated between Snecma and Customer under this agreement will be governed by European Community regulation in force (to date, Council directive 2006/112/EC). Should value added tax or similar tax be applicable to the contemplated transaction, Snecma will be entitled to invoice Customer such tax in addition to the price hereto, unless Customer provides Snecma with adequate exemption. © Snecma | All rights reserved 2/18 D. Assistance - It is expressively agreed between the Parties that Customer will do its best effort to assist Snecma in the following situations: - Obligation for Snecma to provide any public authorities within the jurisdiction of the Customer with any return of administrative, legal or fiscal nature; - Dispute with any public authorities within the jurisdiction of Customer relative to matters of fiscal or customs nature with respect to this agreement or the performance of this agreement on. 8.0 Excusable Delay SNECMA shall be excused from, and not be liable for, any delay in its performance or failure to perform due to causes beyond SNECMA´ reasonable control, including, without limitation, acts of God, war, warlike conditions, inability to secure parts, material or transportation, insurrection, riot, explosions, fires, government acts or failure to act, government priorities, acts or failure to act of civil or military authorities, labor disputes, strikes or Customer´s acts (or failure to act) as required under the terms of these STCS. In the event of such delay, SNECMA shall have the right to invoice Customer for all completed Service, and Customer shall pay such invoice net thirty (30) days. Should Customer's action or inaction (such as, without limitation, delay in providing Customer owned property, Equipment records, approval or other information), cause a delay, Customer's Equipment may be removed from production, which may result in greater than day-for-day delay. If delay resulting from any of the foregoing extends for more than six (6) months and the parties have not agreed upon a revised basis for continuing the Service, including an adjustment of the price, then upon thirty (30) days written notice to the other, either party may terminate their performance in respect to the Service delayed. In the event of such a termination Customer shall pay SNECMA' termination charges upon receipt of SNECMA' invoice(s) therefore. 9.0 Warranty A. SNECMA warrants to Customer that, at the time of Redelivery, the work performed under these STCS will be free from defects in workmanship for a period of one thousand (1000) running hours after repair or six (6) months after installation or one year from date of end of repair, whichever shall first occur. Customer shall send SNECMA written notice of a defect prior to the expiration of thirty (30) days following discovery thereof. If SNECMA reasonably determines that the work performed does not meet the warranty specified above, SNECMA shall promptly correct the defect by, at SNECMA´ option, (1) repairing the defective work, (2) making available at the Designated Repair Facility a repaired or replacement item, or (3) refunding the repair price allocable to the defective work. The warranty period on any such repaired or replaced item shall be the unexpired portion of the warranty on the initially repaired item. If requested by SNECMA, Customer shall ship such defective item, freight prepaid, to the location specified by SNECMA. If SNECMA determines that a repair is covered by this warranty, SNECMA shall reimburse Customer for its reasonable freight charges in connection with the transportation of such item to SNECMA. B. THE FOREGOING WARRANTY IS EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER WRITTEN, ORAL, EXPRESSED, IMPLIED OR STATUTORY (including, without limitation, any warranty of merchantability and fitness for particular purpose). This warranty is not assignable without the written consent of SNECMA. This warranty is applicable only if: the Equipment, following Redelivery, (1) has been transported, stored, installed, operated, handled, maintained and repaired in accordance with the then-current recommendations of the Equipment manufacturer as stated in its manuals, Airworthiness Directives, Service Bulletins or other written instructions; (2) has not been altered, modified or repaired by anyone other than SNECMA; and (3) has not been subjected to accident, misuse, abuse or neglect. C. The liability of SNECMA connected with or resulting from the foregoing warranty shall not exceed in any case the cost of correcting the defect as provided in paragraph A above. Upon the expiration of the shortest period described in paragraph A above, all such liability shall terminate. The foregoing shall constitute the sole remedy of Customer and the sole liability of SNECMA for breach of warranty. 10.0 Limitation of Liability A. The total liability of SNECMA for any and all claims, whether in contract, warranty, tort (including negligence but excluding wilful misconduct or recklessness), product liability, patent infringement, or otherwise, for any damage arising out of, connected with, or resulting from the performance or non-performance of any Service provided hereunder or from the manufacture, sale, Redelivery, resale, repair, overhaul, replacement or use of the Equipment or any item or part thereof, shall not exceed the price allocable to the repaired or overhauled item, part or Service which gives rise to the claim. Consequently, Customer and its insurers waive any recourse against SNECMA for any loss or damage beyond that limit. B. Customer shall defend, indemnify and hold harmless SNECMA for and against any and all losses, claims, suits, judgements, costs and expenses, including but not limited to reasonable attorney fees and all associated costs therewith, which may be incurred by, charge to, recoverable from or which may accrue against SNECMA by virtue of a claim by a third party for injury or death to person or damage to property as a result of the negligent performance or non performance by SNECMA of its obligations under these STCS, except to the extent that that such injury, death or damage is determined to be due solely and directly to SNECMA´ recklessness or willful misconduct. C. In no event, whether as a result of breach of contract, warranty, tort (including negligence but excluding willful misconduct or recklessness), product liability, patent infringement, or otherwise, shall SNECMA be liable for any indirect damages (for avoidance of doubts indirect damages shall cover any similar types of damages such as but not limited to, special, consequential, incidental, resultant, punitive or exemplary damages, including, without limitation, loss of use, revenue, image, profit or goodwill). D. For the purpose of this Article 10, the term "SNECMA" is deemed to include SNECMA and its affiliated companies, the subcontractors and suppliers of the Services furnished hereunder, and the directors, officers, employees, servants and representatives of each. 11.0 Information A. Unless otherwise specifically agreed upon in a proprietary information agreement signed by the parties, any knowledge or information which Customer has disclosed or may hereafter disclose to SNECMA, incident to the Service or Equipment, shall not be deemed to be confidential or proprietary information, and, accordingly, shall be acquired free from any restriction on use or disclosure. B. The existence of these STCS and their general purpose may be stated to others by either of the parties without approval from the other except that the terms of these STCS and any knowledge or information which SNECMA may disclose to Customer with respect to pricing, design, manufacture, sale, use, repair, overhaul or Service of Equipment shall be deemed to be proprietary information and shall be held in confidence by Customer. Such information shall not be reproduced, used or disclosed to others by Customer without SNECMA' prior written consent, except to the extent required by government agencies or courts for official purposes. Disclosure to such government agencies or courts shall be made only (1) upon thirty (30) days advance written notice to SNECMA of such disclosure so as to provide SNECMA the ability to obtain appropriate protective orders and (2) with a suitable restrictive legend limiting further disclosure. C. The preceding paragraph B shall not apply to information which (1) is or becomes part of the general public knowledge or literature otherwise than as a result of breach of Customer's obligations hereunder, or (2) was, as shown by written records, known to Customer prior to receipt from SNECMA, or (3) is disclosed without restriction to Customer by a third party having the right to do so. D. Nothing contained in these STCS shall convey to either party the right to use the trademarks of the other, or convey or grant to Customer any license under any patent owned or licensed by SNECMA. 12.0 Termination Either party may terminate these STCS upon thirty (30) days written notice to the other for failure to comply with any material provision of these STCS unless the failure shall have been cured, or the party in breach has substantially affected all acts required to cure the failure, prior to such thirty (30) days. SNECMA may immediately terminate these STCS if Customer (1) fails to make any of the required payments when due, unless cured within ten (10) days of such payment due date, (2) makes any agreement with creditors due to its inability to make timely payments of its debts, (3) enters into liquidation whether compulsory or voluntary, (4) becomes insolvent, or (5) becomes subject to the appointment of a receiver of all or a material part of its assets. If such termination should occur, Customer shall not be relieved of its payment obligation for Services rendered hereunder. 13.0 Dispute Resolution A. Arbitration Procedure. All disputes arising out of or in connection with these STCS, may be exclusively referred by any party that is involved in the dispute, and to the exclusion of any competent court, to binding arbitration and, if so referred, shall be fully and finally resolved under the Rules of Conciliation and Arbitration of the International Chamber of Commerce (the "Rules") by one or more arbitrators appointed in accordance with said rules. The place of arbitration shall be Paris, France. The arbitration shall be in English and the opinion shall be rendered in French. The arbitration award may be presented and enforced by any party in any court of competent jurisdiction. Notwithstanding the foregoing, SNECMA may at any time seek from a court of competent jurisdiction any relief to avoid irreparable damage occurring in the event obligation set forth in article 6 here above was not performed in accordance with the terms hereof. © Snecma | All rights reserved 3/18 B. Exclusivity, Confidentiality. Each of the parties intends that the dispute resolution process set forth in this Article shall be the parties´ exclusive remedy for any dispute. All statements made in connection with the dispute resolution process set forth in this Article shall not be disclosed to any third party except as required by law or subpoena. C. Exception. Any party may at any time, without inconsistency with this Article, seek from a court of competent jurisdiction any equitable, interim, or provisional relief to avoid irreparable harm or injury. D. Applicable Law. These STCS are construed and governed in all aspects by the laws of France. 14.0 General Provisions A. Right to Subcontract. SNECMA shall have the right to have any of the Services performed at any SNECMA facility or any facility of SNECMA' affiliates, or any subcontractor selected by SNECMA or such affiliates, provided such facility, affiliate or subcontractor is properly certified and rated by the Competent Airworthiness Authority to perform such work. SNECMA´ use of affiliates or subcontractors shall not relieve SNECMA from the responsibility for the proper performance of its obligations set forth in these STCS. B. Assignment. Except as described in paragraph A above, the assignment of all or any portion of these STCS, or any purchase order or any right or obligation hereunder, by either party, without the prior written consent of the other party shall be void. Notwithstanding the foregoing, the Customer's consent shall not be required for the substitution of a SNECMA affiliate in place of SNECMA as the contracting party or the recipient of payments pertaining to all or any portion of these STCS or any purchase order or any right or obligation in connection with these STCS. In the event of any such substitution, Customer shall be so advised in writing, although failure to so advise shall not be cause for termination hereunder. C. Waiver of Immunity. To the extent that Customer or any of its property becomes entitled at any time to any immunity on the grounds of sovereignty or otherwise from any legal action, Customer hereby irrevocably waives the application of such immunity insofar as such immunity relates to Customer's rights and obligations in connection with these STCS. D. Partial Invalidity : If any provision of these STCS shall be held to be invalid, illegal or unenforceable, the validity, legality and enforceability of the remaining provisions shall not in any way be affected or impaired thereby. E. Beneficiaries. Except as herein expressly provided to the contrary, the provisions of these STCS are for the benefit of the parties hereto and not for the benefit of any third party. F. Language, Notices. All correspondence and documentation arising out of or connected with these STCS and any related purchase order(s), including but not limited to Equipment records and logs, shall be in the English language. Any notices furnished under these STCS: (1) shall be in writing, (2) shall become effective upon receipt, and (3) shall be delivered or sent by mail or electronic transmission to the address set forth on the Proposal, which may be change by written notice to the other party. G. Non-Waiver. Any failure by either party to enforce any of the provisions of these STCS or to require at any time performance by the other party of any of the provisions hereof shall in no way affect the validity of these STCS or any part hereof, or in the right of the parties thereafter to enforce each and every such provision; nor shall the parties actual performance, whether or not under these STCS, be deemed in any way indicative of the scope of the obligations of the parties under these STCS. H. Titles/Subtitles. The titles and subtitles given to the sections of these STCS are for convenience only and shall not be deemed to limit or restrict the context of the article or section to which they relate. I. Entire Agreement. These STCS contain and constitute the entire and only agreement between the Parties hereto respecting the subject matter hereof, and supersedes and cancels all previous negotiations, agreements, proposals, statements, course of dealing or usage of trade, commitments and writings in connection therewith. These STCS may not be released, discharged, abandoned, supplemented, changed or modified in any manner, orally or otherwise, except by an instrument in writing of concurrent or subsequent date signed by a duly authorized representative of each of the parties hereto. J. Counterparts: These STCS may be executed by the parties in separate counterparts, each of which shall be deemed to be an original and all of which, when taken together, shall constitute one and the same document. Delivery of an executed counterpart of a signature page to these STCS by fax shall be as effective as delivery of a manually executed counterpart. 16.0 Repair centers Snecma Villaroche Rond Point René Ravaud REAU 77550 MOISSY-CRAMAYEL France Customer Support Manager : François Degras Tel : 33 (0) 1 64 14 85 83 Fax 33 (0) 1 64 14 89 60
[email protected] Snecma Saint Quentin 1, Rue des frères Farman 78771 Magny-les-Hameaux Cedex France Customer Support Manager : Laurent Picot Tel. : 33 (0) 1 30 96 28 00 / 57 52 Fax. : 33 (0) 1 30 96 27 23
[email protected] Snecma Chatellerault Z.I. Nord - Rue maryse Bastié BP 129 86101 Châtellerault Cedex France Customer Support Manager : Bruno Roy Tel. : 33 (0) 5 49 20 45 00 / 45 29 Fax. : 33 (0) 5 49 20 22 43
[email protected] Snecma Sevices Bruxelles Bâtiment 24B - Local 305 Aéroport Bruxelles National BP 1930 Zaventem Belgium Customer Support Manager : Tel. : 32 2 790 45 00 Fax. : 32 2 790 47 99 Propulsion Technologies International 15301 SW 29th Street Miramar, Fl 33027 USA Director of Sales : Gregory Ryan Customer Service : Evelyn Valenciano Tel. : +1 (786)-999-0600 Fax. : +1 (954)-874-0301
[email protected] Aircelle Europe Services Zone industrielle de Saint Ulfrant 27500 Pont Audemer France Tel : 02.32.20.40.00 Fax : 02.32.20.40.50 17.0 Sales Interfaces Philippe DUMAY SALES DIRECTOR Phone : +33 (0)1 60 59 88 16 Fax : +33 (0)1 60 59 55 01
[email protected] Pascal RONDOUIN SALES DIRECTOR Phone : +33.(0)1 60 59 41 37 Fax : +33 (0)1 60 59 55 01
[email protected] © Snecma | All rights reserved 4/18 HARNESS MW0301>0304 & MW0312>0313 Villaroche 325-015-001-0 MW0301/0302/0303/0304/0312/0313 18224 325-026-401-0 Inspection test 21 1150 325-026-501-0 MW0301/0302/0303/0304/0313 18222 325-026-701-0 Minor repair 21 2000 325-026-801-0 MW0312 20513 325-026-901-0 Minor repair 21 3400 325-026-902-0 MW0301/MW0304 20509 325-035-201-0 Major repair 21 3400 325-035-501-0 MW0312 20515 325-035-502-0 Major repair 21 8200 325-045-301-0 MW0302/MW0303 20510 Major repair 21 2700 MW0313 20514 Major repair 21 4100 HARNESS FOR NACELLE - MW0311 Villaroche 325-029-901-0 12886 325-029-902-0 TEST INSPECTION 21 1150 325-029-903-0 20511 325-029-904-0 Minor repair 21 2600 325-029-905-0 20512 Major repair 21 5500 23922 NEW MW0311 ELECTRICAL HARNESS 21 1800 FAN ROTOR BLADE Saint Quentin - PTI 340-001-022-0 11663 340-001-026-0 CLEANING / INSPECTION 7 70 340-001-027-0 BASIC OVERHAUL 11664 BLEND REPAIR OF THE BLADE AIRFOIL +21 +377 SHOTPEENING OF THE FAN ROTOR BLADE REPAIR OF CU-NI-IN THERMAL SPRAY COATING AND DRY FILM LUBRICANT VARNISH ON THE ROOT 11665 STRAIGHTENING OF THE AIRFOIL +7 +850 23514 Reconditioning face mating with booster +7 +452 11731 REWORK ROOT PRESSURE FACE UNDERCUT (CFM special program) +7 +377 23532 Static Moment weight +151 22747 REPAIR OF THE FAN BLADE PER CDR. (CFM technical data) +162 23901 MAPPING ENGINE SET. PRICE PER BLADE +7 FAN DISK PTI 340-000-410-0 11983 340-000-415-0 Cleaning / Incoming inspection 7 1356 340-000-420-0 STANDARD REPAIR 18334 340-000-471-0 REPLACEMENT OF THE CRIMPED SELF- LOCKING NUTS ON THE SPINNER REAR CONE ASSY +30 +20 744 340-000-472-0 340-000-473-0 REPLACEMENT OF THE CRIMPED SPACERS REPAIR OF DOVETAIL SLOT PRESSURE FACES ON THE FAN DISK SB 72-0324 OR 72-0585 22125 REPLACEMENT OF THE CRIMPED SELF- LOCKING NUTS ON THE SPINNER REAR CONE ASSY +30 +22 319 REWORK OF THE FAN DISK REPLACEMENT OF THE CRIMPED SPACERS BLENDING OF THE FAN DISK REPAIR OF DOVETAIL SLOT PRESSURE FACES ON THE FAN DISK 11984 REPLACEMENT OF THE CRIMPED SELF- LOCKING NUTS ON THE SPINNER REAR CONE ASSY +1 137 20230 BLENDING OF THE FAN DISK +1 675 21818 REPAIR OF THE FACE THAT MATES WITH THE SEALING FLANGE OF THE BOOSTER SPOOL +2 999 11985 REPLACEMENT OF THE CRIMPED SPACERS +1 137 19125 REPAIR OF PAINT MARKING +1 304 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price TESTA MIR MIR MAR MAR MAR MAR INSP 002 004 007 MIR MAR SB 72-0062 CINSP CINSP 002 011 016 002 011 012 016 SB 72-0324 002 012 013 016 017 715101 715102 722101 722103 SP MP 014 SB 72-0253 SP MW CDR 001 © Snecma | All rights reserved 5/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price 21819 REPAIR OF LOCKS BY PLASMA SPRAYING +2 822 22719 REPAIR OF THE FAN DISK PER CDR +14 +2 191 11434 FPI + ECI +2 217 SPINNER FRONT CONE PTI 337-005-118-0 13064 340-000-205-0 Cleaning / Incoming inspection 21 209 20597 REMOVAL OF SURFACE DEFECTS AND SPOT TOUCH-UP OF OXIDE FILM COATING OR RESTORATION OF AERODYNAMIC PROFILE AND FULL RECONDITIONING OF HARD ANODIZING +783 22267 REMOVAL OF SURFACE DEFECTS AND REPAIR OF THE SULFURIC ANODIZING, ANTI-EROSION PAINT, AND WHITE SPIRAL MARK ON THE SPINNER FRONT CONE +1 043 19243 REPAIR OF THE SPINNER FRONT CONE DIAMETER THAT LOCATES THE SPINNER REAR CONE +1 518 13065 REPLACEMENT OF THE DEFECTIVE SWAGED SELF-LOCKING INSERTS ON THE SPINNER FRONT CONE ASSEMBLY +418 SPINNER REAR CONE PTI 337-005-118-0 11328 Cleaning / Incoming inspection 14 209 13021 SPOT TOUCH-UP OF THE HARD ANODIZING ON THE SPINNER REAR CONE +586 20781 REPLACEMENT OF CRIMPED SELF LOCKING NUTS ON SPINNER REAR CONE +7 +1 252 21854 REPAIR OF THE SPINNER REAR CONE DIAMETERS +7 +2 514 22798 Repair of the Spinner Rear Cone Mating Faces with the Retaining Flange and/or the Spinner Front Cone +7 +2 723 BOOSTER VANE STG 1 PTI 340-001-307-0 22780 340-001-308-0 Cleaning and serviceability inspection 21 418 340-001-309-0 STANDARD REPAIR 22202 340-001-310-0 Blending of vane airfoil +3 724 Reconditioning of abradable coating on outer shroud 21163 Blending of vane airfoil +897 22203 Reconditioning of abradable coating on inner shroud +2 457 21164 Reconditioning of abradable coating on outer shroud +3 129 22781 Reconditioning of the front flange rabbet diameter +1 669 22782 Reconditioning of front flange rabbet outer diameter +1 669 24001 Replacement of inner shroud +3 360 22692 Improvement of the Fan and Booster Vane Assy to Prevent the Corrosion in Field Only +1 899 BOOSTER VANE STG 2 PTI 335-192-202-0 22795 335-192-203-0 Cleaning and serviceability inspection 21 418 STANDARD REPAIR 22204 Blending of vane airfoil +3 755 Reconditioning outer shroud 21165 Blending of vane airfoil +897 22796 Reconditioning of abradable coating on inner shroud +2 457 22787 Reconditioning of front flange rabbet diameter +1 669 22788 Reconditioning of aft flange rabbet diameter +1 669 22789 Reconditioning of front flange mating face +1 669 22790 Reconditioning of aft flange mating face +1 669 23016 Replacement of vane one by one all stages +9 +10 165 018 CDR AD 2002-13-03 CINSP 001 014 016 026 CINSP 001 002 002 003 017 025 CINSP 001 CINSP 001 003 001 002 010 011 012 013 036 722105 722105 722109 722109 006 007 028 SB 72-0454 003 001 © Snecma | All rights reserved 6/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price BOOSTER VANE STG 3 PTI 340-058-302-0 22797 340-058-303-0 Cleaning and serviceability inspection 21 418 STANDARD REPAIR 22205 Reconditioning of abradable coating on outer shroud +3 724 Blending of vane airfoil 21166 Blending of vane airfoil +897 22206 Reconditioning of abradable coating on inner shroud +2 457 21167 Reconditioning of abradable coating on outer shroud +3 129 21168 Replacement of riveted self locking nuts +705 22792 Reconditioning of aft flange rabbet diameter +1 669 22791 Reconditioning of front flange rabbet diameter +1 669 22793 Reconditioning of front flange mating face +1 669 22794 Reconditioning of aft flange rabbet diameter +1 669 23017 Replacement of vane one by one all stages +9 +10 165 BOOSTER VANE STG 4 PTI 340-058-402-0 21169 340-058-404-0 Cleaning and serviceability inspection 21 418 340-058-405-0 STANDARD REPAIR 22207 340-058-406-0 Blending of vane airfoil +3 724 Reconditioning of abradable coating on outer shroud 21171 Blending of vane airfoil +897 21170 Reconditioning of abradable coating on inner shroud +2 457 21172 Reconditioning of abradable coating on outer shroud +3 129 21173 Replacement of riveted self locking nuts +705 23018 Replacement of vane one by one all stages +9 QUOTE FAN BLADE PLATFORM PTI 23487 340-001-814-0 CLEANING / INSPECTION 21 340-001-816-0 STANDARD REPAIR 22283 REPLACEMENT AND BONDING OF ELASTOMER SEALS (15- 93557) +21 +501 Repair of corrosion damage (P/N340-001-816-0 only) Repair the forward end concave side WEIGHT ADJUSTEMENT OF PLATEFORM FULL OR PARTIAL RECONDITIONNING OF PROTECTIVE COATING (15-93555) 21807 APPLICATION OF SB 72-0586 FOLLOWING ESM 722120 +14 +131 VARIABLE BLEED VALVE GUIDE PADS PTI 340-079-603-0 Price for one part 22772 340-079-604-0 Replacement of PTFE friction pad +21 +1 612 Cleaning, FPI, dimensional incoming inspection Replacement of crimped self locking nuts or swaged self locking insert From 2 to 4 parts (price for each) 22773 Replacement of PTFE friction pad +21 +1 043 Cleaning, FPI, dimensional incoming inspection Replacement of crimped self locking nuts or swaged self locking insert FAN SHAFT PTI 1767M49G05 22824 1767M49G06 Cleaning / Incoming inspection 21 720 1767M49G07 Standard repair 22287 335-006-414-0 REPLACEMENT OF THE ALUMINUM PAINT +3 129 CINSP 003 722109 001 001 002 003 004 015 014 016 017 036 CINSP 001 722109 003 001 002 003 004 036 CINSP 002 722120 003 006 007 008 SB 72-0586 001 002 CINSP 722123 001 002 CINSP CINSP 722201 001 © Snecma | All rights reserved 7/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price REPLACEMENT OF ALL CRIMPED SELF-LOCKING SHANK NUTS 21716 TOUCHUP PAINTING PER INSPECTION +522 22774 Reconditioning of the air/oil separator locating diameter +3 041 22775 Reconditioning of locating diameter with N°1 bearin g sleeve +3 145 22776 Reconditioning of aft locationg diameter with LPT shaft +3 025 22777 Reconditioning of mating face with LPT coupling nut +2 264 22778 Reconditioning of tungsten carbide coating of N°2 B earing locating diameter +5 737 22779 Reconditioning of locating diameter with the fan disk +3 578 23738 Repair of the LPT shaft midspan inner locating diameter +3 025 23737 Repair the locating diameter with fan disk assembly with plasma spray +2 608 21717 INTRODUCTION OF A NEW PROBE HOUSING WITH INCREASED LENGTH INSERTS OR REWORK OF THE OLD ONE +1 268 21790 CLEANING + MPI +1 466 NO. 1 BEARING SLEEVE PTI 301-297-812-0 22558 CLEANING / INSPECTION 21 319 22564 RECONDITIONING OF FWD LOCATING INNER DIAMETER +1 758 22565 RECONDITIONING OF FDW LOCATING OUTER DIAMETER +1 758 FAN OUTLET GUIDE VANE PTI 340-002-305-0 22825 Cleaning / Incoming inspection 37 STANDARD REPAIR 11471 AIRFOIL AND PLATEFORM BLEND REPAIR +21 +183 RECONDITIONING OF THE PROTECTIVE COATING 21726 REMOVAL OF CORROSION AND REPAIR OF PROTECTIVE COATING +7 +53 COMPRESSOR ROTOR SPOOL STAGE 1-2 Châtellerault 72-31-04 17895 CLEANING / INCOMING INSPECTION / AD 2002-13-03 / FPI 28 2140 17896 REPAIR OF ILLEGIBLE PART MARKINGS +420 23530 REPAIR OF FRETTED DOVETAILS +1 828 17897 REPAIR OF DIAMETER B +4 698 17898 REPAIR OF THE SEAL TEETH COATING +3 440 17899 APPLICATION OF THE MOLYDAG 254 COATING ON STAGES 1 AND 2 DOVETAILS +3 091 17900 REPAIR OF FRETTED SURFACE G +1 634 22183 DOVETAIL REPAIR +742 22720 Blending per SP704111 +1 129 COMPRESSOR ROTOR DISK STAGE 3 Châtellerault 72-31-05 21736 Cleaning / Incoming inspection 21 1613 12552 FPI +1 183 22721 Blending per SP704111 +1 054 22426 REPAIR OF THE RABBET DIAMETERS +4 714 COMPRESSOR ROTOR SPOOL STAGE 4-9 Châtellerault 72-31-06 12575 CLEANING + FPI +28 +1 962 22293 REPAIR OF THE SEAL TEETH COATINGS +4 816 002 INSP01 004 005 006 008 010 014 011 016 SB 72-0298 AD 2002-13-03 CINSP 001 002 722212 002 003 004 CINSP 001 002 008 AD 2002-13-03 001 SP704111 CINSP AD 2002-13-03 SP704111 722303 723104 723105 723106 002 005 006 007 008 CINSP © Snecma | All rights reserved 8/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price 22307 REPAIR OF THE FORWARD AND AFT RABBET DIAMETERS +2 140 22228 BLEND REPAIR OF BLADE PLATFORM RAILS +1 505 23140 REPAIR OF THE SEAL TEETH COATINGS QUOTE REPAIR OF THE FORWARD AND AFT RABBET DIAMETERS COMPRESSOR ROTOR SHAFT Châtellerault 1386M56P02 19918 1386M56P03 INSPECTION / TOUCH-UP THREADED END +28 +1 056 1590M28G01 12585 1590M28G02 FPI +1 223 1590M28G03 19794 1590M28G04 Blending per SP704111 +659 1590M28G05 19928 1590M28G06 REPAIR OF COATINGS ON THE SHAFT +4 363 1590M28G07 12311 1590M28G08 REPAIR OF THE LOCKING LUG SLOTS +28 +1 970 21414 REPAIR OF THE AFT FLANGE RABBET DIAMETERS +4 912 21417 REPAIR OF 4.6875-12 THREADS +925 19919 REPLACE THE THREADED END +12 708 19797 REPAIR OF AREA P +1 322 23141 REPLACE THE THREADED END QUOTE REPAIR OF AREA P CPR ROTOR REAR ROTATING AIR SEAL (CDP) Châtellerault 1523M35P01 12325 Cleaning / Incoming inspection 21 1355 22534 AD +1 183 12326 REPAIR OF THE SEAL TEETH COATING +2 204 21606 REPAIR OF THE FORWARD AND AFT RABBETS +3 209 23142 REPAIR OF THE SEAL TEETH COATING QUOTE REPAIR OF THE FORWARD AND AFT RABBETS COMPRESSOR ROTOR AIR DUCT PTI 9514M54 17880 Cleaning / Incoming inspection 418 Standard Repair 23096 REPAIR OF THE FORWARD MATING SURFACE +21 +4 442 REPAIR OF THE FORWARD MATING SURFACE OF THE AIR DUCT DIAMETER BB REPAIR OF THE AFT SUPPORT LUGS REPAIR OF ILLEGIBLE PART MARKINGS 23740 REPLACEMENT OF COMPRESSOR ROTOR AIR DUCT SLEEVE QUOTE 23741 SUPPORT LUG REPAIR QUOTE HPT INNER STATIONARY SEAL (CDP) Châtellerault 1808M56G01 12220 Cleaning / Incoming inspection 7 525 Standard Repair 21159 REPLACEMENT OF THE SEAL CLINCH NUTS +21 +14 280 REPLACEMENT OF HONEYCOMB 17826 HEAT SHIELD REPLACEMENT +10 +13 934 COMBUSTION CHAMBER SSB 724200 STANDARD REPAIR 22932 REASSEMBLY OF THE COMBUSTION CHAMBER + FINAL INSPECTION +28 +27 400 PRELIMINARY + INSPECTION (VISUAL) DISASSEMBLY Standard repair EXTENDED REPAIR 22933 REASSEMBLY OF THE COMBUSTION CHAMBER + FINAL INSPECTION +28 +33 726 003 004 001 003 INSP 723107 AD 2002-13-03 SP704111 002 004 005 006 007 008 007 008 CINSP AD 2002-13-03 723108 001 003 001 003 002 CINSP 001 002 004 005 003 004 B STDR A 723111 724103 724200 B 006 007 CINSP © Snecma | All rights reserved 9/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price EXTENDED REPAIR PRELIMINARY + INSPECTION (VISUAL) DISASSEMBLY COMBUSTION CHAMBER INNER AND OUTER COWLS SSB 1968M59G01 13109 CLEANING / INSPECTION +28 +678 22918 Weld repair and resize outer cowl +888 22941 Weld repair and resize inner cowl +888 23834 Labour Packages (complete units, only SAC) COMBUSTION CHAMBER DOME SSB 1275M27P04 STANDARD REPAIR 22919 1561M26G05 Cleaning / Incoming inspection 28 9267 SPECIAL SIZING TECHNIQUE - VENTURI DIAMETER SIZING AND WELD REPAIR WELD REPAIR AND BORING SCREW BOLT REPLACEMENT OF THE PRIMARY SWIRL NOZZLE RETAINER APPLICATION OF THE THERMAL BARRIER COATING REMOVAL OF THE THERMAL BARRIER COATING PRIMARY SWIRL NOZZLE ANTI ROTATION TANG REPAIR WELD REPAIR AND RESIZE OF BOLTED COMBUSTOR DOME EXTENDED REPAIR 22920 Cleaning / Incoming inspection 28 10285 SPECIAL SIZING TECHNIQUE - VENTURI DIAMETER SIZING AND WELD REPAIR SLEEVE - DEFLECTOR AND SWIRLER REPLACEMENT ON DOME PER ONE SET INSERT Primary swirl nozzle bore plasma spray wear repair Sleeve and deflector replacement WELD REPAIR AND BORING SCREW BOLT REPLACEMENT OF THE PRIMARY SWIRL NOZZLE RETAINER FLANGE REPLACEMENT APPLICATION OF THE THERMAL BARRIER COATING REMOVAL OF THE THERMAL BARRIER COATING PRIMARY SWIRL NOZZLE REPAIR/REPLACEMENT PRIMARY SWIRL NOZZLE ANTI ROTATION TANG REPAIR WELD REPAIR AND RESIZE OF BOLTED COMBUSTOR DOME 22924 DEFLECTOR OF PLATE SPD REPLACEMENT +3 549 22925 DOME THICKBELLMOUTH SPD REPLACEMENT REPAIR +5 597 23827 SWIRLERS - THICK FLANGE QUOTE 23835 Labour Packages (complete units, only SAC) COMBUSTION CHAMBER INNER LINER SSB 1317M57G02 STANDARD REPAIR 22921 1317M57G03 Cleaning / Incoming inspection 28 8028 1968M64G01 1968M64G02 APPLY OF THE THICKNESS THERMAL BARRIER COATING DRILL LINER BOLT HOLES APPLY THE THERMAL BARRIER COATING REMOVAL OF THE THERMAL BARRIER COATING 00C 001 002 COM CINSP 724202 008 009 013 CINSP 001 002 005 006 001 002 003 005 006 007 008 009 010 011 012 013 004 014 SB 72-0455 COM CINSP 005 006 007 012 724201 A EXTR 724203 © Snecma | All rights reserved 10/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price INSTALLATION OF THE NUT PLATES REMOVAL OF THE NUT PLATES IN THE LINER WELD REPAIR AND RESIZING AND STRESS RELIEF EXTENDED REPAIR 22922 Cleaning / Incoming inspection 28 9041 Nugget wall thickness inspection Brazed cooling hole inspection APPLY OF THE THICKNESS THERMAL BARRIER COATING AFT SUPPORT LEG WELD REPAIR Repair inner liner bolt holes DRILL LINER BOLT HOLES APPLY THE THERMAL BARRIER COATING REMOVAL OF THE THERMAL BARRIER COATING INSTALLATION OF THE NUT PLATES REMOVAL OF THE NUT PLATES IN THE LINER WELD REPAIR AND RESIZING AND STRESS RELIEF 22926 INNER LINER SEAL PULSE TIG WELD REPAIR +1 491 Price per patch 22927 WELDED PATCH REPAIR +1 488 22928 WELD REPAIR OF NUT SUPPORT +615 23828 INNER LINER AFT FLANGE AND DATUM REPLACEMENT SPARE PART REPAIR QUOTE 23836 Labour Packages (complete units, only SAC) COMBUSTION CHAMBER OUTER LINER SSB 1317M56G0X STANDARD REPAIR 22929 1968M43G0X Cleaning / Incoming inspection 28 9429 1968M44G0X 1968M63G0X lug ring braze modification APPLY OF THICKNESS THERMAL BARRIER COATING IGNITOR FERRULE REPAIR / REPLACEMENT IGNITER SLEEVE, FERRULE, RETAINER WELD REPAIR AND RESIZING WITHOUT THE LUG RING REPLACEMENT BOLT HOLE DRILLING REPAIR INSTALLATION OF THE LUG RING REMOVAL OF THE COMBUSTION CHAMBER OUTER LINER LUG RING APPLY OF THE THERMAL BARRIER COATING REMOVAL OF THE THERMAL BARRIER COATING REPAIR OF THE PLASMA SPRAY WEAR COATING EXTENDED REPAIR 22923 Cleaning / Incoming inspection 28 12784 brazed cooling hole inspection lug ring braze modification Nugget wall thickness inspection Alf seal flange weld repair Igniter port localized sizing repair and inspection APPLY OF THICKNESS THERMAL BARRIER COATING IGNITOR FERRULE REPAIR / REPLACEMENT IGNITER SLEEVE, FERRULE, RETAINER 001 003 004 CINSP 001 003 004 005 006 007 010 011 012 SB 72-547 SB 72-521 002 008 004 005 009 013 COM CINSP 014 016 SB 72-647 CINSP 006 007 008 009 002 003 009 SB 72-521 SB 72-647 SB 72-547 014 016 017 021 724204 © Snecma | All rights reserved 11/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price WELD REPAIR AND RESIZING WITHOUT THE LUG RING REPLACEMENT BOLT HOLE DRILLING REPAIR INSTALLATION OF THE LUG RING REMOVAL OF THE COMBUSTION CHAMBER OUTER LINER LUG RING APPLY OF THE THERMAL BARRIER COATING REMOVAL OF THE THERMAL BARRIER COATING REPAIR OF THE PLASMA SPRAY WEAR COATING 22934 WELDED PATCH REPAIR +1 491 22935 INCO 718 PLASMA SPRAY REPAIR OF THE LUG RING AFT SURFACE +1 570 22936 WELD REPAIR OF THE OUTER LINER SEAL +1 570 23829 AFT SUPPORT RING REPLACEMENT QUOTE 21155 SALVAGE REPAIR +18 732 23837 Labour Packages (complete units, only SAC) HPT NOZZLE SEGMENTS Châtellerault 2002M20G 19229 2080M35G Cleaning / Incoming inspection 7 158 FULL REPAIR 18768 FULL REPAIR INCLUDING PACH, SVPA AND TBC +21 +3 198 22463 Rework of HPT Nozzles to Double Vertical Seal Slot Configuration +42 +13 824 SPLIT VANE REPAIR (3D-AERO) 19228 COOLING MODIFICATION +7 +134 HPT OUTER STATIONARY SEAL Châtellerault 1808M58Gxx 12287 Cleaning / Incoming inspection 21 578 12288 HONEYCOMB REPLACEMENT ON HPT AFT OUTER STATIONARY SEAL +6 400 22274 DIAMETER B DIMENSIONAL RESTORATION BY PLASMA +2 888 HPT ROTOR BLADES Châtellerault 2002M52P04 21735 2002M52P05 CLEANING / INSPECTION 5 78 2002M52P09 23470 2002M52P11 ECI edge of contact 30 11910 SWET WELD REPAIR ON TIP, AND DEEP TIP CRACKS,RECONTOUR,EDM PLUGGED HOLES +35 +804 FULL REPAIR 13708 THROUGH FIELD REWORK (PN 2002M52P09/11) +56 +1 308 FULL REPAIR with TBC (MONO RENE N5 MATERIAL) REJUVENATION REPAIR 18390 HIGH PRESSURE TURBINE BLADE COATING REJUVENATION +56 +1 308 HPT FRONT ROTATING AIR SEAL (FOS) Châtellerault 1795M36P02 22525 CLEANINIG / INCOMING INSPECTION 28 1006 11428 FPI +1 414 21402 REPAIR OF THE SEAL TOOTH COATING +2 204 21403 REPAIR OF DIAMETER R +1 667 HPT ROTOR FRONT SHAFT Châtellerault 1873M73P01 12694 Cleaning / Incoming inspection 7 952 13934 THERMAL SPRAY RABBET REPAIR +21 +4 343 HPT ROTOR REAR SHAFT Châtellerault 1498M45P06 008 002 003 004 005 012 006 007 CINSP 003 COM CINSP 015 SB 72-0683 004 CINSP CINSP 019 725201 SB 72-0389 020 021 CINSP 725203 AD 2002-13-03 001 002 CINSP 725204 001 725205 725101 725105 017 SB 72-0466 013 015 018 SAL © Snecma | All rights reserved 12/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price 19995 1864M9P04 Cleaning / Incoming inspection 1608 70-21-11 STANDARD REPAIR 20469 70-21-12 REPLACEMENT OF THE SEAL TEETH +28 +7 251 70-21-31 70-21-32 REAR SHAFT BEARING JOURNAL THERMAL SPRAY REPAIR 70-21-33 18298 70-32-14 REPAIR OF AREA M +2 613 70-32-24 23118 70-41-11 REPLACEMENT OF THE SEAL TEETH +12 336 70-53-11 72-00-52 REPAIR OF AREA M REAR SHAFT BEARING JOURNAL THERMAL SPRAY REPAIR 22685 SP 0704111(BLENDING OF ROTATING SEAL) +362 HPT REAR ROTATING SEAL Châtellerault 1319M17P01 13128 1319M17P02 Cleaning / Incoming inspection 7 814 STANDARD REPAIR 19324 REPLACEMENT OF SEAL THEETH COATING +21 +5 786 THERMAL SPRAY REPAIR OF DIAMETER "E" 22166 MOUNTING FLANGE HOLE DAMAGE REPAIR +987 HPT SHROUD Châtellerault 1522M25P02 20468 1795M50P01 Cleaning / Incoming inspection 7 68 1795M50P02 24008 1957M75P01 Standard repair of N5 material +35 +760 1957M91P02 24009 2081M28P01 Enhanced Durability Puck Repair +35 +760 2081M28P02 STANDARD REPAIR + SB C CLIP 11567 STANDARD REPAIR OF N5 MATERIAL +21 +746 C-CLIP COOLING MODIFICATION STANDARD REPAIR ( post C CLIP) 22667 STANDARD REPAIR OF N5 MATERIAL SHROUD WITH C-CLIP MODIFICATION +21 +641 23475 Wear track & forward pad weld restoration +214 HPT SHROUD NOZZLE SUPPORT ASSEMBLY Châtellerault 1784M36G01 22174 2002M69G02 Cleaning / Incoming inspection 28 1224 13628 FORWARD FLANGE WEAR REPAIR +8 474 13629 REPLACEMENT OF SUPPORT BUSHINGS +2 846 22089 REPLACEMENT OF THE BORESCOPE BOSS +2 027 21611 SELF RETAINING SLABBED HEAD BOLT REPLACEMENT +12 768 22335 SUPPORT AFT FLANGE HEADLESS STRAIGHT PIN RELACEMENT +767 23020 Dimensional heat-treat repair with mandels +3 140 13630 REPAIR OF WEAR ON VANES MOUNT AFT FACE +2 552 20559 FORWARD FLANGE DIMENSIONAL REPAIR +3 481 13631 PLASMA SPRAY OF SURFACE AM AND DIAMETER FM +4 095 21636 FORWARD FLANGE WEAR REPAIR +8 474 23119 REPLACEMENT OF SUPPORT BUSHINGS QUOTE FORWARD FLANGE WEAR REPAIR FORWARD FLANGE DIMENSIONAL REPAIR SELF RETAINING SLABBED HEAD BOLT REPLACEMENT HPT SHROUD SUPPORT HANGER Châtellerault 1808M61 20200 1957M74 Cleaning / Incoming inspection 7 100 FULL REPAIR 13848 REPAIR USING RBD +21 +1 266 FULL REPAIR + SB 13983 REPAIR USING RBD +21 +1 591 CINSP 001 005 006 001 005 006 SP SP704111 CINSP 001 003 725210 002 CINSP 013 SB 72-0735 725301 011 SB 72-0079 003 R03,R11 CINSP 004 012 013 014 015 016 018 019 021 SB 72-0156 012 014 019 SB 72-0156 CINSP 014 014 725302 725304 © Snecma | All rights reserved 13/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price C-CLIP COOLING MODIFICATION 23359 Form repair +294 LPT NOZZLE SEGMENTS STG 1 Châtellerault 338-108-606-0 11945 338-108-607-0 Cleaning / Incoming inspection 7 105 338-108-608-0 MINOR REPAIR 1 22514 338-108-609-0 BLEND REPAIR OF THE BLADE AIRFOIL +21 +263 338-108-706-0 338-108-707-0 VPA Overcoating 338-108-708-0 MINOR REPAIR 2 19029 338-108-709-0 BLEND REPAIR OF THE BLADE AIRFOIL +21 +483 RECONDITIONING OF VAPOR PHASE ALUMINIZATION FULL REPAIR 20879 RECONDITIONING OF VAPOR PHASE ALUMINIZATION +28 +2 888 DIFFUSION BRAZING REPAIR HEAVY REPAIR 19031 RECONDITIONING OF VAPOR PHASE ALUMINIZATION +28 +3 429 GAS PATH AREA RECONDITIONNING BY RBD DIFFUSION BRAZING REPAIR 11948 COOLING MODIFICATION +226 LPT NOZZLE REAR FLANGE STAGE 1 Saint Quentin 338-111-303-0 23529 Cleaning / Inspection 840 20374 REPLACEMENT OF THE PLASMA THERMAL COATING ON THE FACE MATING WITH THE STAGE 1 LPT NOZZLE SEGMENT +21 +4 515 INTERMEDIATE FLANGE Châtellerault 23591 CLEANING / INSPECTION 7 420 21715 REPAIR OF THE THERMAL COATING ON MATING FACE AND RABBET DIAMETER WITH STAGE 1 LPT NOZZLE INNER AIR SEAL +21 +3 366 LPT BLADES STAGE 1 Châtellerault 338-108-206-0 23615 Cleaning / Incoming inspection 7 16 STANDARD REPAIR 23616 TOUCH UP OF ALUMINIZATION ON STAGE 1 TURBINE BLADES +20 +100 Repair of Hard Facing and if necessary, the Mating Faces of Tip Shroud on the Stage 1 Blades with Coast Metal 64 Repair of the Seal Teeth on the Blade Tip Shroud, by Weld Buildup with Coast Metal 64 Repair of the Seal Teeth by Plasma Spraying Resetting of Pretwist Angle AIRFOIL BLEND REPAIR 23617 Repair of the Vapor-Phase Aluminization +21 LPT BLADES STAGES 2-4 Châtellerault 338 116-303-0 11578 338-108-304-0 Clean and serviceability inspection 7 16 338-108-403-0 STAGE 2 - STANDARD REPAIR 23654 338-108-503-0 REPAIR OF THE SEAL TEETH BY PLASMA SPRAYING +20 +100 338-108-504-0 338-108-553-0 Repair of the Vapor-Phase Aluminization on the Stage 2 Blades 338-108-5540 338-115-902-0 TOUCH-UP OF ALUMINIZATION ON STAGE 2 338-116-102-0 338-116-103-0 REPAIR OF HARD FACING AND MATING FACES ON TIP SHROUD WITH CM 64 STAGE 2 338-116-152-0 338-116-153-0 AIRFOIL BLEND REPAIR RESETTING OF PRETWIST ANGLE STAGE 2 23657 Repair the seal teeth on the blade tip shroud by weld build up with coast metal 64 +21 STAGE 3 - STANDARD REPAIR 001 SB 72-0079 016 CINSP 005 005 017 005 002 CINSP 001 CINSP 725311 725401 001 002 003 004 005 007 008 CINSP 002 003 004 006 010 018 725402 020 725306 725308 017 018 SB 72-0089 CINSP 001 055 © Snecma | All rights reserved 14/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price 23655 REPAIR OF THE SEAL TEETH BY PLASMA SPRAYING +20 +100 Repair of the stage 3 and stage 4 turbine blades seal teeth by weld build-up with coast metal 64 REPAIR OF HARD FACING ON NOTCHES/MATING FACES ON TIP SRHOUD AIRFOIL BLEND REPAIR RESETTING OF PRETWIST ANGLE STAGE 4 - STANDARD REPAIR 23656 REPAIR OF THE SEAL TEETH BY PLASMA SPRAYING +20 +100 Repair of the stage 3 and stage 4 turbine blades seal teeth by weld build-up with coast metal 64 REPAIR OF HARD FACING ON NOTCHES & MATING FACES ON TIP SHROUD REPAIR OF HARD FACING ON NOTCHES & MATING FACES ON TIP SHROUD AIRFOIL BLEND REPAIR RESETTING OF PRETWIST ANGLE STAGE 3 AND 4 23658 Removal of Oxides and Oxysulfides by Chemical Cleaning +21 LPT DISKS STAGE 1-4 Châtellerault - PTI 336-001-804-0 22526 Cleaning / Incoming inspection 21 1183 22785 Machining foward flange of stage 1 and 2 +4 300 12579 AD 2002-13-03 +645 13760 Blending according SPM 70-41-11 +2 150 LPT ROTOR SUPPORT Châtellerault 725405 13157 CLEANING / INSPECTION 21 1022 CLEANING + FPI STANDARD REPAIR 23571 REPAIR SURFACE MATING WITH LPT FWD ROT. OIL SEAL +4 515 RECOND REAR SURFACE MATING WITH FWD ROT. AIR SEAL LPT ROTATING AIR SEALS STAGE 1-4 Châtellerault 338-111-502-0 12449 338-111-603-0 Cleaning / Incoming inspection 21 504 338-111-701-0 12450 REPAIR OF THE TITANIUM/ALUMINIUM OXIDE COATING ON THE SEAL TEETH +2 673 STAGE 1 TO 4 18772 RECONDITIONING OF RETAINING RING MATING FACE +3 035 22179 TOUCH-UP OF SEAL TEETH QUOTE REPAIR OF SEAL TEETH BY WELD BUILD-UP LPT CASE PTI 338-117-404-0 21850 REPLACEMENT OF RIVETED PARTS AND RIVETS +2 187 21777 REIDENTIFICATION PER SB72-0552 +825 23869 Repair of wear marks on rail 0 support ring by plasma spaying QUOTE Rework of the LPT Case Rail 0 Support Ring and Reidentification of the LPT Case. PACKAGE 1 18920 REPLACEMENT OF RIVETED PARTS AND RIVETS +80 QUOTE REPAIR OF WEAR MARKS ON RAIL 0 BY PUSLED WELDING BUILD-UP RECONDITIONING OF THE DIA A BY PLASMA LPT NOZZLE SEGMENTS STAGE 2 Châtellerault 338-109-106-0 13627 338-109-107-0 Cleaning / Incoming inspection 7 105 338-109-206-0 MINOR REPAIR 002 003 005 007 017 002 003 005 008 009 017 028 CINSP 001 AD . 725403 SP 704111 CINSP AD 2002-13-03 001 725405 003 CINSP 001 002 725406 003 004 001 SB 72-0552 725407 021 SB 72-0718 001 002 012 CINSP 725408 © Snecma | All rights reserved 15/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price 22510 338-109-207-0 BLEND REPAIR OF THE BLADE AIRFOIL +14 +210 338-109-306-0 338-109-307-0 TOUCH-UP THE ALUMINIZATION MEDIUM REPAIR 19214 BLEND REPAIR OF THE BLADE AIRFOIL +14 +630 REPLACEMENT OF THE ABRADABLE HONEYCOMB LINER REPAIR OF THE VAPOR PHASE ALUMINIZATION FULL REPAIR 20366 BLEND REPAIR OF THE BLADE AIRFOIL +21 +1 680 DIFFUSION BRAZING FULL REPAIR REPLACEMENT OF THE ABRADABLE HONEYCOMB LINER REPAIR OF THE VAPOR PHASE ALUMINIZATION 19216 REPAIR OF THE ANTI-ROTATION SLOTS AND HARD FACE MATING SURFACES BY WELDING +7 +447 11552 INNER PLATEFORM REWORK +7 +630 LPT OUTER STATIONARY AIR SEALS STAGE 1 Châtellerault 338-112-603-0 13985 338-112-605-0 Cleaning / Incoming inspection 7 91 338-122-604-0 STAGE 1 - STANDARD REPAIR 22471 REPLACEMENT OF THE ABRADABLE HONEYCOMB LINER +21 +1 040 REPAIR OF WEAR ON LOCATING DOWEL APPLICATION OF VAPOR PHASE ALUMINIZATION (S.V.P.A) ON THE HONEYCOMB LINER ON THE STAGE 1 SEAL SEGMENT STAGE 1 - MAJOR REPAIR 22247 REPLACEMENT OF THE ABRADABLE HONEYCOMB LINER +24 +1 491 REWORK OF STAGE 1 SEAL SEGMENT REPAIR OF WEAR ON LOCATING DOWEL APPLICATION OF VAPOR PHASE ALUMINIZATION (S.V.P.A) ON THE HONEYCOMB LINER ON THE STAGE 1 SEAL SEGMENT LPT OUTER STATIONARY AIR SEALS STAGE 2-4 Saint Quentin 338-112-602-0 STAGE 2-4 23949 338-112-7XX Serviceability inspection only 45 338-112-8XX STAGE 2 - STANDARD REPAIR 23950 Replace honeycomb +21 +435 STAGE 2 23951 Replace FWD braze strip QUOTE STAGE 2 23952 Anti-rotation lock replacement QUOTE STAGE3 - STANDARD REPAIR 23953 Clean and Serviceability inspection 28 435 Replace honeycomb STAGE 3 23954 Replace FWD braze strip QUOTE STAGE 4 - STANDARD REPAIR 23955 Replace honeycomb +28 +435 STAGE 4 23956 Anti-rotation Lock replacement QUOTE LPT NOZZLE SEGMENTS STAGE 3 Châtellerault 338-109-702-0 11573 338-109-704-0 Cleaning / Incoming inspection 7 105 338-109-705-0 MINOR REPAIR 22536 338-109-802-0 VANE AIRFOIL BLEND REPAIR +14 +289 338-109-804-0 338-109-805-0 TOUCH-UP THE ALUMINIZATION MEDIUM REPAIR 22537 VANE AIRFOIL BLEND REPAIR +21 +861 REPLACEMENT OF THE HONEYCOMB LINER APVS - RECONDITIONING OF THE VAPOR PHASE ALUMINIZATION MAJOR REPAIR 20201 VANE AIRFOIL BLEND REPAIR +21 +1 728 REPLACEMENT OF THE HONEYCOMB LINER APVS - RECONDITIONING OF THE VAPOR PHASE ALUMINIZATION 001 005 001 004 018 001 004 018 020 019 SB 72-0241 CINSP 001 006 007 001 006 007 SB 72-0567 CINSP 001 004 008 CINSP 001 004 001 004_STG4 CINSP 001 002 001 005 009 001 005 009 725412 725412 725413 © Snecma | All rights reserved 16/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price REPAIR OF CRACKS BY DIFFUSION BRAZING 21392 REPAIR OF THE ANTI-ROTATION SLOT AND HARD-FACE MATING SURFACES BY WELDING +7 +447 11575 INNER PLATEFORM REWORK +7 +363 LPT NOZZLE SEGMENTS STAGE 4 Châtellerault 338-110-102-0 21393 338-110-103-0 Cleaning / Incoming inspection 7 158 338-110-202-0 MINOR REPAIR 19137 338-110-203-0 Vane airfoil blend repair +14 +473 Replacement of the honeycomb liner FULL REPAIR 19138 Vane airfoil blend repair +28 +1 166 Replacement of the honeycomb liner Repair of cracks by diffusion brazing 19136 Repair of the anti-rotation slot and hard-face mating surfaces by welding +7 +420 SEAL SUPPORT Châtellerault 336-026-302-0 21693 Cleaning / Incoming inspection 7 620 21694 REPLACEMENT OF THE ABRADABLE HONEYCOMB +21 +5 271 21793 REPAIR OF THE ABRADABLE COATING +3 019 21794 REPAIR OF THE OUTER DIAMETER MATING THE LPT ROTOR SUPPORT, BY PLASMA SPRAYING +2 946 21795 REPAIR OF THE INNER DIAMETER MATING THE LPT ROTOR SUPPORT, BY PLASMA SPRAYING +3 035 LPT SHAFT PTI 340-074-703-0 19962 Cleaning / Incoming inspection 28 592 19964 FULL REPAIR OF THE ALUMINIUM PAINT +2 833 22345 REPAIR OF THE AFT DIAMETER, LOCATES THE FAN SHAFT BY PLASMA SPRAYING +3 817 22799 Reconditioning of the N°4 bearing mating face +3 505 22800 Reconditioning of the rear rotating air/oil seal locating diameter +2 226 22801 Reconditioning of LPT stub shaft mating face +2 226 22802 REPAIR OF THE TUNGSTEN CARBIDE COATING ON DIAMETER THAT LOCATES THE N°4 BEARING +4 730 22804 Reconditioning of forward locating diameter with fan shaft by metal coating +3 505 22803 REPAIR OF THE TUNGSTEN CARBIDE COATING ON DIAMETER THAT LOCATES THE N°5 BEARING +3 951 22805 Reconditioning of center vent tube aft locating diameter +2 258 22806 Reconditioning of LPT stub shaft locating diameter on LPT shaft +2 226 22807 REPAIR OF CENTER VENT TUBE FORWARD LOCATING DIAMETER +2 580 22808 Reconditioning of rear rotating air seal locating diameter +2 365 22809 Replacement of bonded ribs +2 226 19963 IT76/96 - R01 - TOUCH UP OF THE ALUMINIUM PAINT +1 301 13164 CLEANING + MPI +1 962 REAR ROTATING AIR/OIL SEAL Châtellerault 336-095-401-0 13738 Cleaning / Incoming inspection 28 648 11976 RECONDITIONING OF THE DIAMETER THAT LOCATES THE LPT ROTOR SUPPORT BY PLASMA SPRAYING +1 908 11977 REPAIR OF THE REAR ROTATING AIR /OIL SEAL TEETH +5 419 003 012 SB 72-0241 CINSP 001 009 725413 001 003 009 012 CINSP 001 002 003 004 CINSP 001 002 003 004 005 006 007 008 009 010 011 012 013 IT76/96 725504 AD 2002-13-03 CINSP 001 003 725416 725501 © Snecma | All rights reserved 17/18 Effective : 01 Janv 2010 CFM56-7 Package Component / Parts ATA/Repair Number Workscope Repair Site TAT in days Price CENTER VENT TUBE PTI 301-319-724-0 23495 334-007-196-0 Cleaning / Inspection 21 471 Standard repair 17740 RECONDITIONING OF FRONT AND/OR MID JOURNALS +5 748 REPLACEMENT OF CENTER SECTION RECONDITIONING OF AFT JOURNAL 21087 RECONDITIONING OF FRONT AND/OR MID JOURNALS +1 777 21086 RECONDITIONING OF AFT JOURNAL +1 568 21083 REPLACEMENT OF CENTER SECTION +2 822 17071 REPLACEMENT OF MID JOURNAL SECTION +2 508 17073 REPLACEMENT OF FORWARD SECTION (IN CONJUCTION WITH REP 003 ) +1 902 21088 REPAIR OF THE LOCATING HOLES +1 401 18068 Recond. of aft. locating diameter +2 195 23493 Repair of the Anti-rotation Tang by Weld Build-Up +2 258 22470 CLEANING AND CONDITIONING +418 23161 REIDENTIFICATION SUIVANT SB 72-0124 +2 822 21707 REWORK OF ANTI-ROTATING TANG +2 090 22966 Any combination of repairs do not exceed 28 days REAR VENT TUBE PTI 23531 Cleaning / Inspection 7 366 23542 REPLACEMENT OF ONE OR SEVERAL LOCATING PINS +14 +784 NO. 4 BEARING FORWARD ROTATING OIL SEAL Châtellerault 336-009-801-0 21599 Cleaning / Incoming inspection 21 523 22278 PLASMA SPRAY REPAIR DIAMETER C +1 542 22279 PLASMA SPRAY REPAIR DIAMETER X +1 239 12413 RECONDITIONING OF THE ABRADABLE COATING +2 242 21600 REPAIR OF RABBET DIAMETER (DIA A) +2 185 LPT SHAFT PLUG ASSEMBLY PTI 23537 Cleaning / Inspection 7 314 CINSP 001 002 003 001 002 003 004 005 006 007 008 009 SB 72-0124 15-93902 COM CINSP 001 CINSP PLASM PLASM2 001 002 CINSP 725506 725510 725514 725516 © Snecma | All rights reserved 18/18